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Aviation OLF helideckmanual_010911_en

1. 01 09 2011 Page 23 4 1 4 1 3 OLJEINDUSTRIENS LANDSFORENING Operations This section of the manual describes operational limitations and the routine tasks of the helideck crew during helicopter operations The step by step duty of each individual member of the helideck crew during take off and landing is described in enclosure G and for stop start of rotors engines in enclosure H Operations related to the fuel plant and refuelling are described in Chapter 5 Fuel Control and Operations Reference is also made to Chapter 6 4 Refuelling in strong winds Operating on the helicopter deck The use of anti collision lights as a signal to the helideck crew After the helicopter has landed and is ready for unloading the helicopters anti collision lights will be switched off This indicates that the helideck crew have permission to approach the helicopter in order to carry out their tasks See enclosure B Danger Zones Immediately before takeoff or when the situation so requires the pilot will switch on the anti collision lights This indicates that the helideck crew must immediately vacate the helideck The HLO will give the thumbs up signal when all personnel have left the helideck and all objects have been removed there from Use of wheel chocks This procedure applies to all helicopters with a wheeled undercarriage during operations on fixed installations mobile rigs and vessel
2. 01 09 2011 Page 47 OLJEINDUSTRIENS LANDSFORENING 6 3 2 Risk reducing measures 6 4 6 5 6 5 1 When a report has been received forecasting winds of more than 50 knots each installation shall attempt to reduce the passengers exposure to the wind Such appropriate methods may include e A careful evaluation when selecting the exit access to the helideck that is least exposed to the wind e The heliguard and fireguard assisting passengers to from the helicopter e Passengers carrying only one piece of luggage so as to have one hand free e The heliguard and the fireguard handling all luggages on the helicopter deck In such cases it may be necessary to strengthen the manning of the helicopter deck The HLO must continuously evaluate the conditions on the helicopter deck and after conferring with the pilot decide how best to ensure the safety of the passengers If the HLO decides that the safety of the passengers can no longer be upheld in a sound and proper manner he must stop helicopter operations on the installation The Installation Manager or similar must be duly informed Refuelling in strong winds In special situations emergencies it may be required to refuel the helicopter with wind forces in excess of 60 knots In such cases special precautions must be taken The pilot will brief the helideck crew regarding any special procedures to be followed or precautions to be taken The HLO should ca
3. SUPER PUMA AS 332 L Li Exhaust Anti collision light MR Anti collision light k S oos d NOR version E Prossure rofuoling N point aft rh sponson bs 3s v E N M Grounding point Gravity fuel points rh side Max length 187m Enclosure F1 to OLF Helideckmanual rev 01 09 2011 SuperPuma L L1 a m DE z i OG E Enclosure F1 to OLF Helideckmanual rev 01 09 2011 SuperPuma L L1 COMPARTMENT 1 MAX LOAD 115 kg MAX SHELF LOAD 290 kg m2 COMPARTMENT 3 MAX LOAD 55 kg A MAX FLOORLOAD 73 kg m2 N conserve NT 2 MAX LOAD 250 kg MAX FLOOR LOAD 390 kg m2 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 General information Eurocopter SuperPuma L2 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 SuperPuma L2 T t ina i Enclosure F1 to OLF Helideckmanual rev 01 09 2011 SuperPuma L2 Total 1 2 350 Kg Total 1 2 3 400 Kg 200 kg COM sjel Enclosure F1 to OLF Helideckmanual rev 01 09 2011 General information Eurocopter EC225 Maximum Take off weight 11 000 kg 4 250 Ibs Empty Weight Standard Aircraft 5 256 kg 11 587 Ibs seful load 5 744 kg 12 663 Ibs MTOW with external load 1 200 kg 4 690 Ibs eating capacity E i CABIN INTERNAL DIMENS
4. DO NOT LOAD OVER THIS LEVEL Two Bags of Equipment for securing the helicopter during parking etc are located on the upper shelf These are not to be removed from the helicopter UPPER COMPARTMENT EQUIPMEN IRCRAFT EQUIPMENT DO NOT REMOVE Adi enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Nor W ay IV CLOSING THE BAGGAGE COMPARTMENT After loading of baggage please observe the following 1 Attach all straps and tighten as shown in the pictures on page one Insure that all baggage is within the limits given above and that there are no foreign objects or persons in the area that could become trapped during operation of the ramp 3i Move the ramp to the fully up position NOTE Observe entrapment danger on each side of the ramp 4 Switch off any lights at the Control Panel 5 Release and turn the handle on the upper hatch clockwise see page 2 and pull the hatch down into the fully down position Turn the handle back into horizontal position and push handle into the recess and locked position 6 Ensure that the area behind the helicopter is clear and give a sign to the crew Please observe that the S 92 helicopter creates a significant higher rotor wind downwash than other helicopters that have been operated previously For safety reasons it is of utmost importance that any loose objects on or close to the helideck are properly secured during landing and take off All baggage and other cargo located
5. DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 38 OLJEINDUSTRIENS LANDSFORENING tank depth is allowed Thereafter all the specified tests must be repeated The process shall be repeated until a satisfactory result is achieved but should a satisfactory result not have been achieved after the fourth settling period the fuel will not be approved The final test results the results from the last settling periods should be noted and the receiver s copy of the transport certificate signed Both a receipt for the fuel and the results of the tests should be noted on the transport certificate for aviation fuel Helicopter fuel should not be used until the fore mentioned procedures have been completed and satisfactory test results have been achieved 5 11 2 Non approved fuel Before fuel that does not meet the requirements regarding purity specific weight or water detection is returned it should be given a new settling time before draining and testing the fuel at least three more times The equipment instruments should be checked a new set should be tried if available and it should be ensured that the tests are conducted according to the procedures Should the test results still be uncertain another person should conduct the tests by themselves Should this test confirm the unsatisfactory or uncertain results a Superior must be informed If the fuel and or the tank cradle do not meet
6. 6 7 Traffic light on display The traffic light on the display indicates when one of the parameters above has reached a threshold As long as all the measured parameters are within limits it should show a green light and when a limit is passed it should show a red light This function may be coupled to a light enclosure L to OLF Helideckmanual rev 01 09 2011 system on the helideck that shifts between green and red parallell to the traffic light This is to enable the flight crew to see the status of the helideck movements from the cockpit on landing and when parked on the helideck 7 Heading of Helideck Vessel The heading of the helideck and the vessel shall be stated in degrees relative to magnetic North 8 Weather data Data for this section may be assessed by the use of other equipment than the HMS system but must be of a standard that has a possibility to deliver data to the HMS system Ref Chap 6 Norsok standards N 002 and C 004 8 1 Wind Direction Wind direction shall be stated in degrees relative to magnetic North Displayed wind direction shall have the options to show real time wind direction 2 minute mean wind direction and 10 minute mean wind direction 8 2 Wind Speed Wind speed shall be stated in knots Displayed wind shall be configurable to show real time wind 2 minute mean wind with gusts exceeding ten knots of the mean wind and 10 minute mean wind with gusts exceeding 10 knots for 3 sec or more of the mean 10
7. The following subsections are guidelines regarding the visual checking of fuel samples e Colour Jet fuel may vary in colour from completely clear water colour to a straw yellow colour e Water Free water will normally show as drops on the sides or at the bottom of the sample jar free floating It may also occur as a misty cloud in the fuel Emulsification e Particles Consists mainly of small specks of rust sand dust or scale from hoses and equipment settle at the bottom of the sample Jar e Clear and bright This expression is independent of the natural colour of the fuel Clear means that there is no presence of sediments or emulsion Shiny refers to the shiny appearance of the fuel when it is completely clean If water or particles are discovered new samples must be taken until the test is clear and bright e Control Check This check consists of a Visual Check and the specific weight density of the fuel This check is made to ensure that the fuel has the proper quality and has not degraded or been polluted during storage The results of this test are compared to the values listed on the certificate When the actual weight has been corrected to standard 15 C the difference must be no more than 0 003 kg l If the difference is greater the product must be quarantined and not supplied until the reason for the deviation has been clarified and new approval given If the discovered deviation is in the form of a technical problem
8. The helicopter also have a rotor brake which can be used to stop rotation of the main and tail rotor AFTER the engines have been shut down Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Emergency Exits Upper cabin door 1 ROTATE HANDLE 2 PULL DOOR UP Figure 2 Upper cabin door Emergency exit The cabin door consists of one upper and one lower part The door opens upwards and gas cylinders will help raising the door To open the door e Rotate handle from locked to open position and pull door open Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Lower cabin door Figure 3 Lower cabin door The upper door MUST be open prior to opening the lower door The door opens downwards and dampers will help restricting the door movement To open the door e Open UPPER door e Rotate handle from locked to open position and lower door Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Cabin emergency exits EXIT 1 ROTATE HANDLE 2 PULL HANDLE TO REMOVE HATCH OPEN _ A Figure 4 Cabin emergency exit The three cabin emergency exits are not hinged to the aircraft When operating the handle the emergency exit will be forced out on the bottom and then slide out of the frame on the top WARNING SUPPORT HATCH DURING PROCEDURE IF YOU DO NOT DO THIS HATCH CAN FALL AND CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT To open
9. f zo wz zs ie Yee 20 au zo wa EL q O md O Page 1 li m Elo zo oo C FE Eo 3 z z o o 2 LU tc DOCUMENT NO O OLJEINDUSTRIENS LANDSFORENING Changes in this edition 2 13 helideck Report max period of validity extended text 3 1 12 Marking of closed helideck new 5 6 Specific weight measuring New second last sentence If an electronic 6 5 Flights to installations that are normally unmanned reworked Enclosure B New layout adjusted zone at cargo bays Enclosure F5 removed S 76 new AW139 Enclosure I change cloudbase from helideck to sea level Enclosure F1 new info cargobay EC225 Enclosure M Helideck Report Renamed to Helideck Report OLF ver1 and attached as separate writable PDF form Updated content DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 2 C OLJEINDUSTRIENS P LANDSFORENING TABLE OF CONTENTS 1 GP Mer C M 5 1 1 Purpose and SCOPE RU 5 1 2 lacer cer T 5 1 3 iren EE NE EE 5 1 4 Distribution and Amendments uamedsmmeneuiddauuveu kdtnmesagdaaeikni 5 1 5 SE ne EE NER 5 1 6 41 EEE EE NE EE EE ER 6 2 Responsibilities requirements and operational regulations 8 2 1 HESDOBSIDIIID REE NE re awe I credo Cmn So eene Uti n 8 2 2 Approval of mobile and fixed installa
10. 30 5 2 PUMOS eua bentes siete EE EE teenies ence ce 30 5 3 Personnel duties ve 30 5 4 Sampling and COMMO S xia rense ennie R EE ES 30 5 5 Testing and COMUO S vasset a ia s oaia 31 5 6 Specific weight measuring density measuring ssene 35 5 7 Basic requirements for laboratory samples eernnnnnnnnnnnvvvnnnnnnnnnnnnnnvnnnnnnnnnnnnnnnnnnnnennennnnn 36 5 8 Hoses for aviation fuel approval and control seseeee 37 5 9 Presse erre 38 50 Fillhgnazzesvavvcqvesaogessssmedeue anaadusnemb naumsaeasumigdun 38 5 11 Receiving fuel and checking the delivery ssssssssssen en 38 5 12 Fuel SVS ry GRC gjopee rmm 41 5 13 Review over required documentation nnnnnvnnnnnnnnnnnnnnnnvnnvnnnnnnnnnnnnnnnnnnnnenerennnnnnnnennnnnnnn 42 6 Special procedures and operatiOnS rrsrrrnnrnvvnnnnnnnnvvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnenn 44 6 1 Emergency situations M E Eiaa 44 6 2 Helicopter deck Safedeck rrnnnnnnnnnnrnnnnnnrnrrnnnnnnnnnnnnanannnnnnrnnnnennnnnnnnnnnnnrnnrnnnensrnrrnnnenennn 47 6 3 Embarking disembarking from the helicopter in strong wind esses 47 6 4 Refuelling in strong WINGS P ee nenna 48 6 5 Flights to installations that are normally unmanned eee 48 DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 3 OLJEINDUSTRIENS L
11. Material and equipment Available communications equipment 7 Follow up Carry out an evaluation of the exercise where all elements of importance are noted for use in the transfer of experience and any required documentation Note who has taken part in the exercise file the information for use as documentation in the event of an audit 8 Estimation duration Approximately 1 hour enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 3 Subject Training with the rest of the Emergency Organisation 1 Purpose To maintain and develop the helideck crew s proficiency in dealing with emergencies involving the whole of the installation 2 Training objectives At the end of the lesson exercise the participants will have learnt about understand and be able to deal with emergency situations involving other areas on the installation For example Fire gas and oil leaks evacuation of the installation or other scenarios based on local conditions 3 Contents With available means and knowledge take part in and assist the other units of the emergency organisation in dealing with situations described in paragraph 1 4 Preparations Ensure that the HLO and the rest of the helideck crew are involved in developing the exercise scenario 5 Implementation Participate and take an active part in the installation s emergency exercises 6 Materials and equipment All the available emergency equipment that the situat
12. includes documented knowledge in the use of smoke diving apparatus Special responsibilities and duties for the leader of the helicopter deck HLO It is the duty of the HLO to supervise and run day to day operations on the helideck during helicopter visits including updating the installation manager in writing at regular intervals regarding the status of the helideck equipment and services He shall i a ensure that e necessary steps are taken to deny unauthorised persons access to the helicopter deck prior to take off and landing e the deck is cleared of loose objects snow and ice inflammable substances etc necessary personnel are present and at a state of readiness the helideck crew has been briefed on any special conditions prior to the arrival of the helicopter specially on the arrival of unfamiliar types of helicopter or in the event of special operations DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 9 2 11 OLJEINDUSTRIENS LANDSFORENING all equipment and instruments are in place and in full working order e all crane operations in the vicinity of the landing area have been stopped and the cranes are correctly positioned in relationship to the free approach and departure sectors e passengers are held in the safe zone during landing take off and that they are given guidance during disembarkation and embarkation passengers are wearing on their survival suits in a proper
13. land on the helicopter deck preparations must be made to deal with the situation Ensure that the radio operator control room is informed and that the proper alarm signals have been activated The emergency teams are mustered in accordance with the installation s internal procedures All of the crew who man the helideck must don fire protection gear Put on smoke diving apparatus Dry powder equipment Prepare the fixed powder extinguishing hose for immediate use See Chapter 3 Stand in a sheltered area with this equipment at the ready 6 2 Helicopter deck Safedeck 6 2 1 General description Helicopter decks of the Safedeck type have been specially designed to quickly lay a complete layer of foam over the whole surface of the helicopter deck in the event of a fire in the helicopter or a crash on the helicopter deck The deck may also have a pop spray system 6 3 Embarking disembarking from the helicopter in strong wind 6 3 1 General information The upper limit for ordinary passenger transport is 60 knots wind including gusts The wind on the helicopter deck may deviate from the given wind measurements Due to the surroundings around the helideck upwind or downwind and or funnel effects may occur together with turbulence This changes the wind fields radically Such local conditions will differ from installation to installation and may also vary with the wind direction DOCUMENT NO REVISION NO REVISION DATE
14. 73545500 Mob 47 91316103 E mail magnus leirvik kongsberg seatex no MIROS Att Sturla Maehre Solbr veien 32 P O Box 364 N 1372 ASKER Norway Tlf 47 66987500 Mob 47 99039379 E mail office miros no Blom Maritime AS Gauselveien 90 N 4032 STAVANGER Phone 47 51 70 85 13 Fax 47 51 70 85 01 E mail pms blom no FUGRO OCEANOR Att Jon A Silgjerd Luramyrvn 29 N 4313 Sandnes Norway Tlf 47 51 63 43 30 Mob 47 90 19 53 29 E mail j silgjerd oceanor com Shore Connection International AS Att Jonny Rabben N 5397 Bekkjarvik tlf 47 41 53 60 60 E mail mail shoreconnection no www shoreconnection no MARINTECH AUTOMATION AS Att Oddbj rn Morlandst Hollundsdalen 5430 Bremnes Norway Tlf 47 56 90 92 00 Fax 47 56 90 92 01 E mail mail marintech automation no suppliers 1 1 enclosure M to OLF Helideckmanual rev 01 09 2011 j CHC J t Bristow Reporting form ground occurences Place Date Time Occurrence categories Operations of the aircraft Tick off category Collision between aircraft and other object on the helideck L Security Attack on aircraft such as bomb threat or hijacking Difficulties in handling intoxicated violent or unmanageable passengers Discovery of a nonregistered passenger OOO L Incorrect procedures on the helideck unintentional persons passengers on the helideck Systems Leakage of hydraulic fluids
15. Direct passengers from the fire heliguard standing at the entrance door towards the baggage and or the fire heliguard standing at the edge of the helideck See enclosure B safe access HELIGUARD AND FIREGUARD 1 Open cargo doors and unload baggage and cargo placing the baggage 90 to the helicopter on the opposite side of the entrance door or on the baggage trolley 2 One fire heliguard opens the cabin door and direct passengers towards the HLO standing in front of the nose 3 The other fire heliguard takes position by the baggage at the edge of the helideck to direct the passengers to the closest exit Operation Embarking around the nose of S 92A EC225 SuperPuma 1 Take position in front of the nose inside the rotor tip approx 1m from the nose Keeping eye contact with the pilots and both sides of the helicopter 2 Check that one fire heliguard is in position by the entrance door ready to receive the passengers and then signal to the fire heliguard that he may now let the passengers enter the helideck 3 Direct signal to the passengers what is the safe route between him and the nose of the helicopter and direct them towards the heliguard by the entrance door 4 Move back to normal position on the helideck outside the rotordisk keeping eye contact with the pilots and full view of the helideck HELIGUARD AND FIREGUARD 1 One fire heliguard takes position by the entrance door of
16. Evaluate whether the equipment is suitable and correctly placed Note who has taken part in the exercise 8 Estimated duration Approximately 1 hour enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 7 Subject Governing documentation 1 Purpose To maintain the knowledge of the documentation that governs helicopter operations To ensure that changes and updates in the governing documents are made known to relevant personnel in a systematic and proper manner 2 Training objectives At the end of the lesson the participants will have learnt about the at all times available applicable governing documentation 3 Content Study the available documents 4 Preparation Provide updated documents where these are available 5 Implementation Ensure a thorough review of the governing documentation Group work followed by a presentation of the results 6 Materials and equipment Governing documentation 7 Follow up Carry out an evaluation of the lesson Note who has taken part in the lesson 8 Estimated duration Approximately 1 5 hours enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 8 Subject Life support and First Aid 1 Purpose To maintain the helideck crew s knowledge of life Support and first aid 2 Training objectives At the end of the lesson the participants should be able to carry out life Support and first aid 3 Content To be developed by the instal
17. Installation Helideck Report Date Flight number gt Example DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 11 OLJEINDUSTRIENS LANDSFORENING Troll A Helideck Report 13 08 10 or Aasgard B Helideck Report 13 08 10 HKS477 Send the completed form via E mail to the relevant helicopter operator e Bristow Norway helideck norway bristowgroup com e CHC Helikopter Service helideck chc ca NB These e mail addresses are for receiving helideck reports only and will not be monitored for other requests 2 13 1 Filling in the form The form is self explanatory but rolling the pointer above a writable field then additional information will show up Items that need further explanations are detailed in the below paragraphs Dynamic positioning Cross YES or NO to indicate if the vessel is positioned dynamically DP If DP system is active YES If inactive moored anchored free floating with or without steering speed or fixed installation NO Accurate monitoring equipment HMS system If a moving helideck ie not a fixed platform and HMS system operative Cross YES If no operational HMS system or fixed platform Cross NO Log info Logistics data have to filled in if this information are not reported separately in accordance with local arrangement Return load may not be available when this form is forwarded to the helicopter operator How
18. Traffic light on display ssssssssessseeenenen nennen nnne nnne nnns 5 7 Heading of Helideck Vessel eese eese esee eren nnn ennt annie nnn annt innen 8 Weather anirua Da TAEAE BS tae Ss sn a en or on aD 8 1 Wind Direction iota eene tee nh ne eee cee ele eds 6 8 2 Wind Speed uci get d qu EH ee ee acu 6 8 3 Visibility uui dee Hn ae e qu e Hi de d i D ut ett 6 8 4 Temperature Dewpoint sssssssssseeeenenenneeenen nennen nnne entrent 6 8 5 Air Pressure vain uice deu ode gere de educ a ee e pede dede 6 8 6 C IDEE PPM 6 8 7 Logging system eie eene tdeo det doe d raa de pe da ape La ede io 6 Attatchment 1 Helideck Movement and Weather data display 9 Attatchment 2 Logistics Information display eere 10 List of known motion measurement equipment producers eere enclosure L to OLF Helideckmanual rev 01 09 2011 1 Purpose and intentions The purpose of this document is to ensure uniformity of readings registration of helideck movement and weather conditions This standard is an agreement between Norsk Helikopter AS an CHC Helikopter Service AS and shall apply to all Moving Helidecks operating on the Norwegian Continental Shelf Further intentions are to establish National and International standards based on contents of th
19. cm length 2 4 m e llluminated during night flying Identification The helicopter deck shall be marked with the name of the installation clearly visible from all approach directions above the level of the helicopter deck Lighting Helicopter decks that are to be used for night flying and or in conditions with reduced visibility must Have a satisfactory shielded floodlighting arrangement so that the pilots cannot be dazzled during the approach and landing phase The floodlights are to be used at the request of the pilot Be marked with perimeter lighting consisting of green lamps equally spaced at a interval of not more than 3 metres The perimeter lighting must not reach more than 25 cm above the level of the helideck The floodlighting and the perimeter lighting must be connected to the installations plants emergency power supply and switchover time must in the event of a failure of the main power supply be no more than 10 seconds The highest point of the derrick crane booms and cabins or any other obstacle that represents a hazard to flying must be marked with red warning lights and be visible from all positions The derrick and crane booms must also be fitted with red lights at levels for every third of the overall length calculated from the highest point of the derrick crane boom DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 17 3 1 8 OLJEINDUSTRIENS LANDSFORENING A
20. copper alloys cadmium plating galvanised steel or plastic materials is permitted The use of copper containing materials for other components in contact with the fuel shall be minimised and no zinc or alloy materials containing more than 596 zinc or cadmium shall be used No flow in the process line shall exceed maximum 7 m s Grade marking All units must be marked in accordance with API requirements Design Criteria Norwegian Maritime Directorate NMD Norwegian Petroleum Directorate NPD Class requirements shall be followed all vessels except fixed installations Norsok standards CAP 437 Transportable tanks DnV 2 7 1 amp IMO IMDG requirements They shall also conform to the dangerous goods Code Type 1 or 2 Storage and recycle tanks TBK ASME VIII and BS5500 Categories I II III e Filter water separators according to API IP 1581 Specification and qualification procedures for aviation jet fuel separators latest edition e Aviation fuel filter monitors according to API IP 1583 Specification and qualification procedures for aviation fuel filter monitors with absorbent type elements latest edition e Refuelling hose type C grade 2 semi conducting meeting the latest edition of API 1529 or BS EN 1361 e Vessel movements wind and explosion loads must be taken into consideration during construction of the system enclosure J to OLF Helideckmanual rev 01 09 2011 Helicopter refuelling system The following subsecti
21. displacement vane pump or centrifugal pump with a head and flowrate suited to the particular installation For larger helicopter types it might be advisable to use larger capacity units The pump unit should be constructed to meet EX zone 1 The pumps shall be equipped with internal relief valves or alternatively with a common external relief valve The relief valve outlet should be routed to the pump suction side The pump unit shall be connected to only one tank Check valves must be installed on the discharge side of each pump An emergency stop valve for pneumatic driven systems or emergency stop panel electric driven shall be installed enclosure J to OLF Helideckmanual rev 01 09 2011 Block ball valves should as a minimum be installed on the pump unit inlet and outlet flange A pressure gauge must be installed on the pump discharge side A device for automatic pump stop at a pre set time after start and during emptying the tank shall be installed on the system Filter Water Separator A filter water separator according to the API IP 1581 specification latest edition sized to suit the pump capacity should be installed either in the pump unit or in the dispensing unit The Filter Water separator shall also be fitted with e Adifferential pressure gauge for monitoring the conditions of the elements e Anair eliminator which automatically vents any air entering the vessel e A pressure relief valve e A closed circuit samp
22. e Wind direction and velocity e Any other information of importance to flight safety Where two frequencies are in operation all other communication shall take place on the Logistics frequency on another radio DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 29 5 5 1 5 2 5 3 5 4 5 4 1 OLJEINDUSTRIENS LANDSFORENING Aviation fuel Introduction General The contents of these guidelines cover the minimum requirements regarding the use of equipment for supplying fuel to the helicopter It is important that the helideck crew is familiar with these guidelines and the relevant safety requirements Purpose This document contains operational guidelines and includes the control and handling of the product aviation fuel Jet A 1 Personnel duties It is the responsibility of each individual installation to establish a preventative maintenance programme relating to the unit with regard to safety and environment and ensuring that such measures are in accordance with current regulations The most important duties for personnel involved in operating the units are to always ensure that the correct fuel quality is delivered that the product is free from water and pollutant solids and that refuelling is carried out in a safe secure and efficient manner The HLO has the day to day supervision of the refuelling operations He shall ensure that all work is conducted in a
23. even though the test has been concluded so as to get a DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 32 5 5 3 5 5 4 OLJEINDUSTRIENS LANDSFORENING confirmation of the change of colour A detector must be used only once and thereafter discarded Drainage Sampling and Checking Drainage and product sampling routines at the plant In order to check that the storage tanks and delivery equipment are particle and water free drainage samples must be taken on a regular basis The equipment must be drained for water and particles at the following intervals e Daily from storage tank filter separator and filter monitor before the day s first delivery e Before and after each delivery After heavy rain and storms Drainage must be carried out with a full flow of liquid from the tank sump the filter water separator and from the inlet side of the filter monitor The liquid must be drained into clean clear glass jars of at least 3 5 litres for Visual Check If the sample does not give a satisfactory result by Visual Check the plant must be drained and new samples taken until a satisfactory Visual Check is achieved If unusually large amounts of free water or particles are found or if it is not possible to achieve a satisfactory Visual Check then the system must be taken out of service Investigations must be carried out immediately to find the cause of the pollution Visual Check
24. four partitions is located above the Control Panel IBAGGAGE COMPARTMENT OPERATION BAGGAGE COMPARTMENT ACCESS NA AMP HEIGHT FROM GROUND Use the Ramp Control switch on the left hand side to move the Ramp down to approx 8 inch 20 cm above the ground NOTE The Ramp shall not be moved fully down to the surface as this may cause severe resonance in the helicopter enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway II LOADING Loading of baggage is done by unfastening the hooks for the nets as shown below LOWER COMPARTMENT LOADING UPPER COMPARTMENT ACCESS DO NOT REMOVE EIO EN NET HERE y Please observe that only parts of the nets on upper shelf need to be unfastened depending on the amount of baggage UPPER COMPARTMENT LOADING UPPER COMPARTMENT UNLOADING FULL ACCES FULL ACCESS paw ems XN SS III BAGGAGE COMPARTMENT LIMITATIONS The following limitations apply and should not under any circumstances be exceeded Max 150 Ibs 68 kg in each partition on the upper shelf and max 580 Ibs 264 kg in total on the lower shelf ramp see placard above the Control Panel The baggage volume shall not exceed the height of the fence on the ramp to avoid crushing when the ramp is moved to upper position see dotted line below right enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway LOADING LIMITATIONS WEIGH LOADING LIMITATIONS HEIGH
25. in degrees relative to magnetic North and Wind velocity speed in knots Other relevant weather info Fill in additional relevant weather information that is not presented elsewhere in this section l e fog banks variable winds resent rain snow showers thunderstorm activity lightning variable visibility in different directions etc Sea spray observed over the helideck Check Yes or No if there has been has not been observed reported sea spray over the helideck This can be difficult to determine but in regard to incidents of sea spray causing engine flame out The helicopter operator does require observed reported sea spray to be reported HELIDECK MOVEMENT Max pitch UP DOWN with reference to horizon The largest pitch movement up down over the last 20 minutes measured in degrees with reference to the horizon Max roll Starboard Port with reference to horizon The largest roll movement starboard port over the last 20 minutes measured in degrees with reference to the horizon Max Helideck Inclination The largest measured helideck inclination over the last 20 minutes measured in degrees with reference to the horizon Max heave top to bottom The maximum heave total vertical movement of the helideck is the maximum top to bottom value in one cycle one movement curve over the past 20 minutes Heave period The time in seconds between tops of two waves If measurement equipment is not available the pilots will use a s
26. is much stronger than other helicopters operating today During take off and landing it is very important that loose items located on or in close proximity to the helicopter deck is secured in a proper way Luggage and cargo stored in trolleys must be secured with cargo nets Personnel should also be aware of this strong downwash not only during take off and landings but also when embarking and disembarking the helicopter A pair of glasses and other loose items might come loose in these conditions if not secured properly Please contact the crew if additional information is required 17 enclosure F4 to OLF helideckmanual rev 01 09 2011 enclosure F4 to OLF helideckmanual rev 01 09 2011 DanCopter EC 155 B1 DanCopter DanCopter EC 155 B1 The EC 155 helicopter can be handled from either side as there are luggage compartment doors on both sides Therefore handling of passengers and cargo on the platforms should be performed from the side most convenient to the helideck crew unless something else has been agreed If the helideck crew has never received any instructions of how to operate the doors please inform the pilots and ask for assistance One of the pilots will show you how to operate the doors When opening the luggage compartment door the light switches automatically on and vice versa First thing is to unload all luggage on the helideck Close the luggage compartment door before the cabin door is opened The
27. manner e passengers have fastened their safety belts Before landing the HLO shall maintain contact with the helicopter pilot and inform whether the deck is clear for landing The HLO shall immediately report any form of deviation on the helicopter deck to his immediate superior installation manager so that the helicopter operator may be informed of the situation The HLO shall be positioned to be able to observe as best as possible and closely monitor landing and take off The HLO shall immediately inform the pilot via radio or visually if any abnormal situation occurs The threshold using the radio should be low and with no demands regarding phraseology or language Warning should though preferably be given in English if this can be achieved without time loss Clothing and protective equipment for the helideck crew All persons who are part of the helideck crew during take off and landing shall each have immediate access to one set of equipment consisting of Norwegian Standard European Norm NS EN 469 Protective clothing for fire fighting NS EN 659 Protective gloves for fire fighting NS EN 443 Helmets for fire fighting EN 15090 Boots for firemen alternative old standard NS EN 345 2 Safety shoes for occupational use EN 533 Balaclava helmet EN 137 Smoke diving equipment a minimum of two 2 sets for distribution When the equipment is not in use it shall be stored in a separate locker ready for rapid donning in the immedi
28. minute wind 8 3 Visibility Horizontal visibility shall be stated in metres 8 4 Temperature Dewpoint Temperature dewpoint temperature shall be stated in degrees Centigrade 8 5 Air Pressure Air pressure shall be stated in hPa as QNH meaning altitude adjusted for for height and temperature relative to sea level 8 6 Cloud Cloud is stated as few scattered broken overcast few sct bkn ovc in feet above the ground 8 7 Logging system The system should be able to log all data for at least 48 hours The historic data should be available by configuring the date and time to the period of interest enclosure L to OLF Helideckmanual rev 01 09 2011 Attatchment 1 Helideck Movement and Weather data display Data Display layouts shall be approved by the Helicopter Operators Typical layouts are attached Kongsberg Seatex HMS 100 Norwegian Sector Petrojarl I File Option Help Motion Summary Compass Configure Category A Limititation Day October 1 0 1 o 3 49 N maznetic N 63 26 31 356 Max Roll Pitch 3 1 7 E 10 24 12 196 Max Avg Heave rate 1 3 m s Vessel heading Helideck heading Position o Time C 230 Roll 2 0 deg Por and 2 0 deg Stbd Wind direction Pitch 1 4 deg Down and 1 4 deg Up Max heave 5 4 meter s 05 1 2 60 kts Heave periode 36 sec Max Avg heave rate 0 3 m s UTC Print report i Logistic info Info last submitted at 17 0ct 2003 08 01 33 GMT Ww VScale Roll and Pitch Vessel moti
29. negative refuel Installation We copied negative refuel Changes in weather conditions If the weather changes visibility ceiling the movements of the helideck or other details of interest to the Helicopter Crew this must be forwarded over the radio with no delay enclosure J to OLF Helideckmanual rev 01 09 2011 Specification for offshore refueling systems This specification is applicable for all fixed and floating installations operating on the Norwegian shelf Specific class requirements from the Norwegian Civil Aviation Administration NCAA BSL D 5 1 the Norwegian Maritime Directorate NMD Norwegian Petroleum Directorate NPD Class BV ABS DnV amp Lloyds and UK regulations CAP 437 latest revision must be complied with This specification is based on the requirements made by the Norwegian Offshore Helicopter Operators for offshore helicopter refuelling systems and the approval of the refuelling systems will be done by them General information No threaded connections are accepted in all wetted parts Exceptions are the connection to the 30m fuel hose nozzles dry break coupling gauges air eliminators sample valves instruments amp instrument fittings A complete system description and specific operation procedure shall be available to the operator Materials All pipework Norsok AS20 and accessories shall be of stainless steel or mild steel protected internally by lining with approved epoxy material No
30. on the helideck As is the case with manned installations control forms and maintenance routines must be available If a floating installation movement data roll pitch heave must be available at the mother installation according to standard HMS system specifications Landing and departure shall be observed from the mother installation or stby vessel either visually or by video monitoring of the helideck Helideck crew and helicopter shall have radio contact with the mother installation or stby vessel during the complete helicopteroperation If there is any danger of gas on the installation gas detectors with warning lights shall be in operation A light should be positioned in the limited obstacle secor 150 sector and have good visibility at approach and at helideck During night flying the perimeter lights red obstacle lights and the approach lights must be switched on DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 49 7 CUT Erz zroq332dgzmoow o I OLJEINDUSTRIENS LANDSFORENING Company Specific Procedures N A Enclosures hand signals helicopter danger zones helifuel forms phraseology emergency training SuperPuma AS332 amp EC225 CHC HS Sikorsky S 92 NOR Sikorsky S 92 Eurocopter EC155 AgustaWestland AB139 Westland SeaKing Agusta A109E take off and landing helicopter shut down guidance to radio communications offshore refuelling sy
31. or on the helicopter deck 3 2 3 Alarm systems Fire Alarm Boxes FAB s Boxes for activating the fire pumps are located near the helicopter deck Throwing the switches in these boxes will start the fire pump s and indicate in the control room which fire alarm box has been activated DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 20 OLJEINDUSTRIENS LANDSFORENING 3 3 Fire fighting equipment The authorities requirements relating to fire protection on the helicopter deck are to be found in the Civil Aviation Authority s the Maritime Directorate s and the Petroleum Directorate s regulations See Chapter 1 5 The Helicopter Landing Officer HLO shall ensure that the fire fighting equipment is always in good working order and ready for use Any deviation shall be reported to his her immediate superior NOTE The fire extinguishers system of the helideck must not be activated prior to helicopter landing Activation before completed landing could lead to loss of deck references for the pilots 3 3 1 Fire water system A fire water system is compulsory 3 3 1 1 Purpose and effect By using water a fire may be controlled or extinguished in the following manner Water can act as a dilutor when converted to steam in the fire zone Steam reduces the oxygen content in the air current mixture by 1 3 Water absorbs heat when being converted to steam Water may be used for cooling surrounding areas so as
32. pitch in degrees up and down from zero with zero being the absolute horisontal level It shall be possible to read the historic maximum angles over the past 20 minutes direct and if possible graphically The graphical presentation shall cover 20 minutes of data and alternatively 3 hours for trend determination The graph and the associated max value last 20 minutes shall be updated at least at 1 minute intervals In maritime terms maximum pitch consists of trim pitch 6 2 Maximum Roll The equipment shall be capable of measuring helideck roll in degrees right starboard and left port with zero being the absolute horisontal level It shall be possible to read the historic maximum angles over the past 20 minutes direct and if possible graphically In maritime terms maximum roll consists of list roll 6 3 Maximum Helideck Inclination The equipment shall be capable of measuring the maximum helideck inclination in degrees to the absolute horizon over the past 20 minutes direct and if possible graphically 6 4 Vertical Movement Maximum Heave The equipment shall be capable of measuring vertical helideck movement from top to bottom with readings in metres The maximum heave total vertical movement of the helideck is the maximum top to bottom value in one cycle one movement curve over the past 20 minutes It shall be possible to read the historic maximum value over the past 20 minutes direct and graphically The graphical presentation s
33. relating to the unit competent personnel must be summoned DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 33 OLJEINDUSTRIENS LANDSFORENING 5 5 5 Sampling and inspection Daily every morning to be carried out by the HLO Take a 3 5litre sample from the filter separator and monitor with the system pressurised Take a 3 5litre sample from the tank currently in use All samples to be checked with the Shell Water Detector The accepted sample from the storage tank must be kept for 24 hours The sample must not be exposed to sunlight If two tanks are being used during the course of one day then the samples from both tanks must be kept for 24 hours The samples must be labelled Carry out a visual inspection of the equipment to check for leaks and damage When transferring fuel read off and note in the helicopter tank log the monitor s pressure difference Earth cables Daily inspection for good mechanical contact with the unit and for possible damage All tests and inspections must be logged Weekly checks and inspections to be carried out by the HLO If the system has been out of operation for more than a week in addition to the other samples a 3 5litre sample must be taken from the filling nozzle In order to distribute wear and tear on pumps A and B a weekly alternation of the pump in use is recommended Take a 3 5litre sample or until the sample is acceptable from portable tanks th
34. safe manner and in accordance with the relevant procedures and instructions All inspections relating to operations shall be logged Sampling and controls General Jet A 1 shall be subject to quality assurance controls from the refinery to consumption All quality assurance shall be controllable This must be conducted in accordance with the relevant guidelines All samples must be taken by competent personnel using proper procedures and equipment It is important that persons suffering from colour blindness do not carry out water detector tests This is to ensure that that samples that are taken give a correct picture of the product being controlled All sampling must be logged 5 4 2 Water Water in the fuel may be found in two forms e As dispersed water i a fine small droplets that have separated from the fuel The dispersed water may be removed separated from the fuel in the filter separator Any remaining water will be absorbed in the filter monitor e As water molecules i a loosely attached to the fuel molecules Water attached to the molecules in this manner cannot be removed by these methods Even though it occurs in only minute quantities it is nevertheless of no little DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 30 OLJEINDUSTRIENS LANDSFORENING importance for the fuel Such fine dispersion may be generated during the water and the fuel s path through a pum
35. standards eg ASME VIII and BS5500 Categories I II IIl The tank shall slope 1 on 30 The sump shall be fitted with a 3 4 minimum sample line which has both a ball valve and a self closing ball valve at the sample point The outlet should either be by floating suction or from a stack pipe which extends at least 150mm above the lowest point of the tank If a floating suction stainless is embodied a bonded wire pull assembly should be fitted to the top of the tank The suction floating is strongly recommended and shall be used when possible Make sure the drain point on the stationary tanks on mobile units e g rigs FPSO s are able to drain the tank sump varying on the vessels movements position Automatic closure valves to the delivery and suction inlet should be capable of operation from both helideck dispenser unit and from another point which is at a safe distance from the tank The tank shell must be properly bonded Each chamber to be equipped with 500mm quick release hinged manhole to allow physical access Dipstick or a sight glass content gauge to determine the tank content A closed circuit sampler connected to the sample point is recommended A combined pressure vacuum relief valve must be installed on each closed chamber of the tank Pumping module A 60 mesh Y strainer shall be installed in front of the fuel pumps The twin pump unit shall be air driven alternatively electrically equipped with a positive
36. that samples that are taken from the portable tanks are given a powerful rotation in order to achieve such a cyclone Satisfactory result When none of the above mentioned are visible and the sample is clear and sediment free Unsatisfactory result The sample is not clear and transparent water or pollution is present If a sample contains sediment and or free water e Further samples must be taken until the fuel is clear and free from water clear and bright e If the sample contains finely dispersed water a settling time of 1 hour per meter tank depth shall be allowed After which a new purity test must be carried out This process must continue until the samples are completely free from water and or sediment clear and bright satisfactory test results 5 5 Testing and controls Shell s water detector should be used to check the samples taken from the helicopter fuel Jet A 1 Should a detector change colour it is most important that the procedures described in the following are used to remove the pollution from the fuel The detector is comprised of the following components e Anunbreakable injection syringe of 5 ml e A plastic detector capsule containing water sensitive paper DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 31 5 5 1 5 5 2 OLJEINDUSTRIENS LANDSFORENING Storing Shell s Water Detectors The capsule lid should be screwed on as soon as possible after the detecto
37. the helicopter Fire protective clothing clothing used to protect response crews from heat and other stresses during fire smoke diving situations Exempted from this definition is the protection of head hands and feet that is regulated through separate NS EN standards DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 7 OLJEINDUSTRIENS LANDSFORENING 2 Responsibilities requirements and operational regulations The authorities place minimum requirements regarding helicopter decks equipment and personnel These may be found in BSL D 5 1 Some extracts from the BSL are quoted here 2 1 Responsibility The operator of an installation is responsible for ensuring that the installation s helideck refuelling plant and competence meet current requirements 22 Approval of mobile and fixed installations Prior to initial use on the Norwegian Continental Shelf an installation s helideck and refuelling plant must be approved by relevant authorities and the helicopter company s operating on the installation For permanent installations the relevant authorities are The Petroleum Safety Authority Norway and the Norwegian Civil Aviation Authority For mobile installations the relevant authorities are the flag state alternatively the Norwegian Maritime Directorate assisted by the Norwegian Civil Aviation Authority Reference is made to chapter 3 23 Inspection The operator of an installation is respons
38. the helicopter 2 The other fire heliguard takes position by the stairway 3 When signaled by the HLO the person by the stairway collects the boarding cards shows where to drop the baggage and directs passengers towards the HLO 4 The fire heliguard positioned by the entrance door guides the passengers into the helicopter enclosure H to OLF Helideckmanual rev 01 09 2011 Helicopter shut down start up From The helicopter is on the deck the passengers have left both the helicopter and the helideck and the anti collision lights have been switched on again To The rotor has stopped and the anti collision lights have been switched off again Operation Preparation HELIGUARD Stand in the safe zone with a full view of the Stand in the safe zone by Maintain firewatch helideck and with the wind at his back the access stairs Operation Shut down 1 When the rotor has stopped and the anti When requested by the When requested by the HLO collision lights have been switched off the HLO assist in tying down lassist in tying down the rotor helideck may be entered the rotor blades and blades and securing the 2 The HLO will get help to tie down the securing the helicopter helicopter rotor blades and secure the helicopter as required Helicopter start up From The helicopter is on the deck with the pilots onboard and the anti collision lights on To The helicopter has both engines running the roto
39. the specified standards the following should be noted at the bottom of the aviation fuel transport certificate Details regarding the fuel and or deficiencies with the tank cradle The name of the installation The date The signature of the reporter The completed original of the certificate should then be returned to the cartridge on the tank cradle The label should be placed on the transport tank as is shown below and the following completed on the cargo manifest e Non approved fuel e From the name of the installation e To to be completed 5 11 3 Using fuel directly from a transport or storage tank Depending on how the plants are designed on the different installations fuel deliveries may either be transferred from the transport tank to fixed stationary tanks or remain stored in the transport tank by being coupled to the refuelling system 5 11 4 Fuel in the transport tank DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 39 OLJEINDUSTRIENS LANDSFORENING If the transport tank is used for storage an earth cable must be attached to the tank cradle This must also be attached during the transfer of the contents of the tank to permanent stationary storage tanks The tank is coupled to the pump s manifold system with the aid of a pliable flexible hose corrugated steel pipe that is connected to the coupling on the transport tank Only one tank at a time shall be conn
40. to prevent the fire from spreading or to improve access to the area of the fire 3 3 1 2 Application Water is the best extinguishing agent for fires in woodwork paper garbage and is good for damping down fires following the use of hand held extinguishers 3 3 1 3 Equipment 1 5 hoses are standard equipment for fire water hosing down Foam equipment may alternatively be used with water only 3 3 1 4 Use Water used on an oil fire should be in the form of a fine spray Water must never be used on fires in electrical equipment before the power supply has been shut off Water must be used in the form of a fine spray for cooling For most fires the water jet must be directed at the root of the flames 3 3 2 Foam systems 3 3 2 1 Purpose and effect DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 21 OLJEINDUSTRIENS LANDSFORENING By using foam a fire may be controlled and or extinguished in one or more of the following manners Foam acts as a smothering agent If used in sufficient amounts it reduces the oxygen supply by preventing the influx of air Foam acts as a dilutor When forced into a fire zone foam is converted to steam and will under certain conditions reduce the air current mixture by 1 3 The process of converting foam to steam will absorb heat A sufficiently thick layer of foam will protect explosive materials that are exposed to the fire by insulating and ab
41. 0 1 GENERAL The overall installation consists of two forward external luggage cases installed on the attachment fittings for heavy load on the RH and LH sides of the Helicopter The door of luggage cases is equipped with a fail safe locking device This device consists of three plugging locks one of which is secured by key The luggage must be secured by a net and straps As an option the RH luggage case can be equipped with a protection allowing the hoist if fitted operation Lasterom EC 225 Upper shelf Compartment 1 200 kg Lower shelf Compartment 2 250 kg Aft shelf tail compartment 3 50 kg Forward luggage pods each 200 kg 14 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 EC225 Bristow Norway Cargo Loads Cabin Floor A placard indicates the maximum load carrying capacity per unit area CABIN FLOOR LOADING 800 daN m 1 16 Ib in Placards indicating the maximum load carrying capacities and safety instructions Cabin A DOORS MUST BE LOCKED DURING TAKE OFF LANDING AND IN FLIGHT WHEN NO LUGGAGE HANDLING IS IN COURSE Luggage compartment 1 B LUGGAGE MAX LOAD 150 kg MAXIMUM FLOOR LOAD 125 kg m2 D LUGGAGE MAX LOAD 50 daN MAXIMUM FLOOR LOAD 75 daN m2 Additional luggage compartment 2 C LUGGAGE MAX LOAD 160 kg MAXIMUM FLOOR LOAD 210 kg m2 MV EC225KNA1 0020 00 15 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Use of cargo sponsons on t
42. 01 09 2011 Page 36 5 8 OLJEINDUSTRIENS LANDSFORENING Hoses for aviation fuel approval and control Each hose must have a permanent identification and a log for inspection and controls This must contain the date and year of manufacture the date and year of when the hose was taken into use and information relating to the results of maintenance and inspection The maximum storage time is two years The maximum lifetime for hoses is 8 years subject to annual pressure testing and inspection in accordance with API 1529 BS EN 1361 Both periods are to be calculated from the date of production If the hose is not pressure tested annually the maximum lifetime is set to 2 years Prior to use new hoses shall be flushed in accordance with API 1529 BS EN 1361 and then pressure tested Products that have been used for flushing are to be returned to a slop tank that is either being filled or settling All hoses used for supplying fuel shall be subject to routine inspections and checks Hoses are to be kept under observation during refuelling If any weaknesses or faults are discovered delivery through the hose must be stopped and the hose replaced Inspection of the hoses may take place in the following manner Pull the hose out all the way and apply full pumping or operational pressure with the delivery connector shut When the hose is under pressure check for exterior damage leaks or other signs of weaknesses It is recommend
43. 2A is located in the aft part of the cabin with access through a two piece hatch under the Tail Boom The Compartment consists of two shelves which again are divided into two partitions The lower shelf is attached to the Cargo Ramp lower hatch and may be moved up and down by a Control Panel located on the inside of the compartment S92A BAGGAGE COMPARTMENT CHC HS BAGGAGE COMPARTMENT ACCESS Ae enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway I OPENING AND LOADING OF THE BAGGAGE COMPARTMENT To get access to the Baggage Compartment the handle located in the upper hatch right under the Tail Boom must be operated see pictures below Press the button on the handle to release turn handle clockwise and push the hatch to full upper position Please observe that the handle is spring loaded and will automatically move to full open position once turned over center This to avoid damage when the hatch is moved BAGGAGE COMPARTMENT OPENING BAGGAGE COMPARTMENT ENTR Turn the handle back to horizontal position to secure the hatch in full upper position and push handle into the recess again by gently pressing on each side of the handle This to avoid injury during loading The Control Panel for moving the ramp up and down plus switches for internal and external lights is located on the Baggage Compartment right hand sidewall A placard with information on load limitation and numbering of the
44. ANDSFORENING Company Specific ProcedUt s cuiii inen ca ita enr ken ine eru ra S c ceu pep re Dc a Dann hates 50 EN CIOSUBGS e 50 A handsignals B helicopter danger zones C helifuel forms D phraseology E emergency training F1 SuperPuma AS332 amp EC225 F2 CHC HS Sikorsky S 92 F3 NOR Sikorsky S 92 F4 Eurocopter EC155 F5 AgustaWestland AW139 F6 Westland SeaKing F7 Agusta A109E G take off and landing H helicopter shut down l guidance to radio communications J offshore refuelling systems K hot refuelling L standard helideck monitoring systems M reporting form ground occurrences Helideck report form See separate PDF attachment DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 4 1 1 1 2 1 3 1 4 1 5 OLJEINDUSTRIENS LANDSFORENING General This manual describes procedures and guidelines for personnel working on helicopter decks helideck crew on petroleum installations on the continental shelf The manual is the document to which the helideck crew shall relate unless the situation requires an exemption for safety reasons The manual has been developed as a joint project between OLF and the helicopter operating companies CHC Helikopterservice A S and Bristow Norway A S Chapters 1 6 describe common procedures and guidelines based on requirements from the authorities and accepted industrial standards C
45. Bristow Norway Cargo compartment The cargo area of the Sikorsky S 92A is located in the aft section of the helicopter fuselage Access to the area is made through an upper cargo door and a cargo ramp The upper door has to be opened closed manually while the ramp lowering raising is controlled by a toggle switch on the Ramp control panel located on the right hand side wall of the cargo compartment The control panel also holds switches for interior and exterior lighting and a receptacle to connect to the helicopters intercom system The cargo area consists of two shelves one upper and one lower Each shelf is divided into two compartments by a cargo net These compartments are named 1 2 3 and 4 In addition to the shelves a cargo storage box is installed on the ramp This box is divided into two compartments One is for the aircraft parking and mooring equipment and the other for cargo related equipment such as cargo attachment rings and jack straps Each of these compartments is labeled with a decal describing the compartment contents Decals are also installed on the shelves and above the ramp control panel These decals describe the cargo compartment areas and weight limitations I ACCESS THE CARGO AREA To get access to the cargo area a two step process has to be performed First the upper cargo door has to be opened and then the ramp has to be lowered Upper cargo door is opened in the following steps Push the door hand
46. DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 6 VV Vv OLJEINDUSTRIENS LANDSFORENING cabin cargo as a general rule when transporting passengers cargo shall not be transported in the helicopter s cabin Exemptions may be made for priority cargo manifest an official document stating the names of the passengers their employers the weight of the passengers and their luggage the weight of the cargo and the destination night conditions when the sun is more than 6 degrees below the horizon Jet A 1 jet turbine fuel used by aircraft clear and bright Jet A 1 the expression is independent of the fuel s natural colouring Clear states that no sediments or emulsions are present Shiny refers to the clear shiny look of completely clean fuel earthing point point on the helicopter for attaching the anti static wire The helicopter the supply cabinet refuelling and pressure refuelling connectors must all be wired to electrical conductors during refuelling to eliminate any differences in current between the units particles in fuel consist mainly of small pieces of rust sand dust or deposits from hoses and equipment rotor disc the area covered by the main rotor Shell water detector test the Shell Water Detector has been developed for those borderline cases where the human eye cannot be trusted The test is a positive indication of finely divided water at concentration
47. E 01 09 2011 Page 43 6 1 OLJEINDUSTRIENS LANDSFORENING Special procedures and operations This chapter covers the special procedures operations that are used on certain installations types of helicopter under special conditions etc For this reason these are not covered elsewhere in the manual Emergency situations Actions that are taken must be in compliance with the installation s emergency procedures Basic principles Teamwork The crew of the helideck must work together as a team when dealing with emergency situations Discuss how to deal with the different emergency situations on the helideck and conduct exercises on the helideck in handling emergency situations This is to develop quick counter measures forms of cooperation and efficient actions Otherwise refer to Enclosure E Emergency Training Reactions in emergency situations Common sense shall be used when reacting to emergency situations Normal train of action e Evaluation of the extent of the emergency situation securing own escape route e Calling for assistance sounding the alarm Dealing with the situation by e Localising the source e Extinguishing eliminating e Rescuing personnel reducing risk e Preventing spreading Monitoring to prevent re ignition repetition Fire in the helicopter on the helicopter deck First actions e Immediately stop any refueling that is taking place e Activate the fixed fire fig
48. ERIFY WILCO Avbryt landing eller avgang Gjentas 3 ganger dersom en farlig situasjon oppdages Bekreft at min melding er mottatt og forst tt Ja eller tillatt Godkjent Indikerer skille mellom meldinger Annuller siste utsendte klarering Bekreft Rettelse jeg har sagt noe feil Dekket er klart for landing Glem se bort fra Begynn Hvordan h rer du meg Jeg gjentar Lytt p frekvensen Nei ikke tillatt feil Kom med din melding Repeter alt eller deler av sendingen Jeg har mottatt meldingen ikke som svar Gjenta alt eller deler av sendingen Snakk langsommere Vent Unders k og bekreft Jeg har forst tt og vil handle deretter enclosure D to OLF Helideckmanual rev 01 09 2011 enclosure E to OLF Helideckmanual rev 01 09 2011 Emergency training Lesson Exercise No 1 Subject Crash on helideck 1 Purpose To maintain the helideck crew s proficiency in meeting the challenges covered by this subject 2 Training objectives At the end of the exercise the participants will have learnt about the use of fire fighting equipment of equipment for gaining access to the helicopter and of treating injured persons and evacuating these and others from the helideck 3 Content Using equipment to gain access to the helicopter Cutting using jacks slicing Cutting seat belts Treating injured persons Crush wounds fractures and burns The use of available fire fighting equipment 4 Preparation Revi
49. Helideckmanual rev 01 09 2011 E NORSK ac J L Standard Measuring Equipment for Helideck Monitoring System HMS and Weather Data rev 5 14 06 2007 CHC Helikopter Service amp Norsk Helikopter ANTEN LULE E i D SN fani ES EE e Er DR pn I rr ee v Eb eee ie ae ai Saez d ED rd E isnt fsa P PR p EXE P a Z5 eee enclosure L to OLF Helideckmanual rev 01 09 2011 Contents 1 Purpose and intentions eemmsdesnenennennnrnnnndnnnennednannrknnnnnenvednnknnnnannnenvednnnesknnnnnsennmannnennennnnnsnannnne PAE iaiT a AP E de seu E Meek E EA 3 Classification of helidecks nennen aaarnas reana aaepe aane misere n aaa aana daea iaa ieme aiaa 4 Operational Limitations serrnnvvnnnnvnnnnnvnnnnvnnnnvnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennn 5 PANCI S ei LRL NN 6 Accuracy of measurments srunnnnnnvnnnnnnnvnnnnnnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnennnnnnnennnnnnnnennnnnnnnennnnnner 6 1 Maximum PItchzcc osse totlseediuisatonddtdisentu AR 6 2 Maximum Roll o orci eeu Sene ditatus ta anten 6 3 Maximum Helideck Inclination ssessseenmm m 5 6 4 Vertical Movement Maximum Heave sssssssssseseneeeeerenen eren 5 6 5 Heave Perlod one nente alie nien atte eii tiis eet is 5 6 6 Max Average Heave Rate sss ener entente snnt innen enne 5 6 7
50. IONS Width At Seat Level Overall Length including aft seat Minimum Height 1 47 metres itted Maximum Cabin Floor Loading 800 kg m CABIN DOOR DIMENSIONS Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Eurocopter EC 225 Main dimensions 18 50 m Rotor Roning ME g 620m 5314T da amp 14m X waka be C son 3 TED EXTERNAL DIMENSIONS See Figure 0 1 J Ground Clearance Under Tail Rotor Skid Wheel Track Wheelbase Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Eurocopter EC 225 ane o t m ster Ai P9409 54 Deu 8 Standard seat configuration EC225 11 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Eurocopter EC 225 A 4x type 4 emergency exits B 8xnormal windows Window jettison 12 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Eurocopter EC 225 Cargo compartment The cargo compartment is in the tail section and consists of 3 separate sections To open Cargo door Turn handle as indicated by arrow and pull The door is hinged and should be lowered carefully To close the cargo door Push door and turn handle as indicated by arrow Do NOT use excessive force on the locking mechanism 13 Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Load baggage bay CHC Helikopter Service EC225 MAX LOAD IN BAGGAGE BAY M 200 kg max Mi Me max par kg 350 kg MV EC225HLO2 0102 0
51. In order to avoid confusion regarding which tank is in use signs shall be posted showing the status of the tank s The following text shall be used e This tank was received on and has been stored since date e The tank is in use e The tank is settling e The tank is empty NB Also applies to tanks used for storage delivery 5 11 7 Old fuel stores As far as possible super numerous stocks of fuel should not be stored offshore Stocks should be depleted if longer periods without replenishment are expected If fuel has been stored for more than six months after the stated filling date a four litre drainage sample should be taken in a special container This should be sent to an approved laboratory for quality control Should the test show that the fuel meets the required specifications for use it may then be used in the normal manner Old fuel may not be used until the test results are available and approval has been received from the fuel supplier laboratory DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 40 OLJEINDUSTRIENS LANDSFORENING On the condition that the results are satisfactory the stored fuel may be used but it must be re tested every third month Fuel that fails to gain approval during these tests shall be returned to shore as Non approved fuel see Item 5 11 2 5 11 8 Returning transport tanks Outlets must be sealed before transport tanks are returned to shore Th
52. L D 5 1 ch V obstructions are obtained 2 To give the Helicopter Crew better situational awareness under marginal weather conditions Need for refuelling while on deck This information is exchanged in this phase to give the HLO adequate time to prepare the helideck for refuelling if the Helicopter Crew requires so upon landing Example of communication Helicopter Seaway Falcon this is Helibus Norsk 123 Installation Helibus Norsk 123 this is Seaway Falcon Helicopter We are on our way and have an ETA Estimated Time of Arrival of 23 23 minutes past the hour Installation You will be here at 23 Are you ready to receive the details Helicopter We are ready Go ahead Installation Our position is N 59 31 35 E 006 46 55 comma pronounced decimal We have a heading of 300 degrees Our speed is 5 knots The weather in the area Wind from 270 degrees 25 knots gusting 35 knots Visibility 3 km We have Broken BKN at 800 feet Temperature 8 degrees Dew Point 5 degrees QNH 989 Hectopascal A shower has just passed through the area The HMS is showing GREEN deck Return load We have 19 passengers Total weight 1945 kg This is including 185 luggage and cargo We have one fishing vessel 500 meters south of us heading South There are no other vessels in the area Do you require fuel upon arrival Enclosure I to OLF Helideckmanual rev 01 09 2011 Helicopter We received all your details We copied a QNH of 989 And
53. LO regarding boarding the 2 When the Heliguard is ready the HLO passengers will give the signal to the fireguard that boarding can start Enclosure I to OLF Helideckmanual rev 01 09 2011 Guidance communications for Radio operator Exchange of Logistic information Approximately 20 minutes prior to estimated time of arrival ETA the helicopter crew will establish contact with Radio or Bridge for update exchange of Position Also heading and speed if relevant Weather update Movements of the Helideck if relevant Return load Obstructions in the vicinity within 500 meter in the approach and departure missed approach sectors Need for refuelling The installation should have dispatched a Helideck Report to the Helicopter base one hour prior to estimated time of departure ETD from shore This report is carried on board by the helicopter crew It is only necessary to update any changes Position The position shall always be given in Latitude and Longitude in the following format N dd mm mm E ddd mm mm d degrees m minutes and decimals of minutes Heading of the installation is given in degrees magnetic north Speed is given in knots Weather conditions If the weather is better than 10 km visibility and ceiling above 1000 ft one can refer to the earlier shipped Helideck Report The wind direction wind speed and QNH shall always be given to the helicopter crew If the visibility and or ceiling are le
54. Loading 1 Check that the heliguard is ready to receive the passengers and then signal to the fireguard that the passengers may now enter the helideck 2 Direct signal to the passengers what is the safe outside the rotor disk embarking route up to the heliguard 3 Remain in the best position for eye contact with the pilot and a full view of the helideck HELIGUARD AND FIREGUARD 1 When signalled by the HLO collect the boarding cards and show the way to the helicopter Signal to the HLO that the numbers tally 2 Lead the passengers safely in to the helicopter and direct the placing of baggage NOTE In high winds be aware of light baggage cargo 3 Stow baggage and shut cargo compartment hatches 4 Ensure that all passengers have fastened their seat belts 5 Close the cabindoor 6 NB Cabin cargo should be loaded and secured before the passengers are taken onboard When loading Super Puma inform the pilot of the total load in cargo compartment 3 enclosure G to OLF Helideckmanual rev 01 09 2011 Helicopter departure From The HLO clears the helicopter deck To Until 2 minutes after departure Operation Preparing for take off 1 Signal to the heliguard to remove the chocks on the left hand side Remove the chocks on the right hand side 2 When the helideck is clear and the fireguard is in position give a thumbs up signal to the pilots 3 Monitor the take off and radio communicat
55. Page 42 OLJEINDUSTRIENS LANDSFORENING 5 13 2 Documentation Maintenance Logbook in which all work carried out on every unit of the equipment is logged Log for testing of pressure tanks connectors and filling nozzles Log for the inspection and testing of hoses Log for the calibration of volume meter Log for the calibration of pressure manometer Log for tank inspection and cleaning Log for filter equipment inspection and maintenance Log for the filter in the pistol grip nozzle inspection and replacement Documentation relating to the execution of these tasks shall normally be found in the installation s preventive maintenance programme See enclosure C for relevant forms 5 13 3 Signature Filing time The person doing the job must sign all documentation Documents relating to daily inspection shall be kept on file for at least 3 months All documents relating to weekly and monthly inspections shall be kept on file for at least 1 year Documents relating to inspections that have longer intervals or relate to non routine incidents shall be kept for at least 3 years 5 13 4 Change of location The remaining fuel quantity onboard shall be logged when the rig is moving to another helicopterbase and or changing helicopteroperator Registered amounts are to be reported in writing to the owner of the fuel as soon as possible and at least 5 days after arrival new location DOCUMENT NO REVISION NO REVISION DAT
56. and guidelines on helicopter safety and their relationship to rules and regulations The authorities place minimum requirements on helidecks equipment and personnel These are to be found in BSL D 5 1 The following items are mainly extracts of the most important regulations in this BSL The helicopter deck in general Obstacles in the approach and departure sectors In the 210 approach and departure sectors and in the immediate vicinity of the deck there shall be no obstacle that rises above the level of the helideck Exempted are The safety perimeter e Perimeter lights and floodlights no higher than 25 cm above the level of the helideck The outer edges of the safety net e Individual obstacles required for operating the helicopter deck railings stairs foam cannon perimeter lights that do not rise more than 25 cm above the level of the helideck Friction The surface of the helideck shall be treated with a material that prevents the helicopter from sliding non skid With the rope net in place the helicopter deck shall have a friction coefficient of at least 0 40 or higher also when the deck is damp or wet Without the rope net the friction coefficient shall be at least 0 65 see item 3 1 3 below Rope net The helicopter deck shall be fitted with a rope net The size of the net is determined by the size of the largest helicopter that is used Such a net is normally dimensioned for a large helicopter the minimum siz
57. and in a safe position in visual contact with the HLO 1 Make sure that the fire cannon are aimed and adjusted enclosure G to OLF Helideckmanual rev 01 09 2011 Operation Immediately prior to the helicopter landing and during landing HELIGUARD 1 Make sure that cranes have stopped 1 Stand in a safe position 1 Stand at the upwind operating Peripheral crane operations in visual contact with the fire post or alternatively may be permitted but the pilot must be HLO at the remote control informed unit Stand at full 2 Notify the pilot on VHF that the helicopter readiness with the switch deck is cleared for landing and give warning for the alarm systems of seaspray if this has been observed on over within reach the helideck In especially difficult weather conditions ask the pilot to notify the passengers 3 Take up a safe position by the most suitable stairway primarily on the upwind side with a view over the helideck 4 Continuously monitor and immediately report any abnormal situation NB Check that the undercarriage is down Operation After landing HO j HELIGUARD FIREGUARD 1 After the anti collision lights have been 1 On receiving a signal 1 Serve at the fire post until switched off signal to the heliguard that from the HLO take the chocks are in place on entry to the helideck is now allowed wheelchocks and place both sides 2 Can take a set of wheelchocks and thes
58. approved means e Cargo must not be placed in seats adjacent to the main emergency exits of the helicopter Transportation of passengers and cargo Transportation of passengers and cargo in helicopters requires according to JAR OPS 3 1220 c that the personnel involved in the operation has the necessary awareness training in dangerous goods This is to enable the personnel to recognize dangerous goods in passenger luggage and also to identify recognize unmarked cargo that could be Dangerous Goods Training requirements The personnel categories requiring dangerous goods awareness training is e The person checking in the passengers luggage and cargo that also makes the passenger and cargo manifest e The HLO and the helideck personnel involved in loading and unloading of passengers and cargo on the helicopters offshore This training has to be performed every 24 months and requires a separate test Records of this have to be filed and maintained on board the vessel installation for each person DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 26 4 2 7 4 2 8 OLJEINDUSTRIENS LANDSFORENING Dangerous Goods requirements If a capacity of transportation of dangerous goods is required from an offshore installation vessel the IATA regulations require a full IATA Dangerous Goods course for the nominated person accepting the cargo This course has to be repeated every 24 months Records of th
59. at are in storage Drain the air separator collector glass When pumping fuel read off the pressure difference and note the result in the weekly log for pressure difference in the separator and monitor See enclosure If the maximum pressure difference for the filter separator or possibly the monitor is exceeded the filter elements must be replaced for the filter separator only step 1 For the filter separator the maximum pressure difference is 15 psi and for the monitor 22 psi Inspect all earth cables for portable tanks supply unit and the filling nozzles If there is any fault or suspected fault maintenance personnel must be summoned The delivery unit must not be used if there is any fault or suspected fault with the unit s earthing system Once a week the differential pressure for the separator and the monitor must be read whilst pumping at the selected delivery volumes The results shall be logged Monthly checks and inspections to be carried out by the HLO Check the delivery hose for damage and log the result ref item 5 8 and the enclosures Carry out function testing of the piston type differential pressure manometer for correct operation This is done by opening the three way valve connected to the meter It is only necessary to check that the piston has free movement throughout its whole length and ensure visually that it properly returns to its initial adjustment The result shall be logged Check the hose end filte
60. at the weight is within limits To close to the cargo area a two step process has to be performed First the cargo ramp has to be raised and then the upper cargo door has to be closed Cargo ramp is raised in the following steps WARNING Check that no foreign objects or personnel interfere with ramp closing Toggle and hold switch labeled RAMP on the RAMP CONTROL PANEL upwards to RAISE position until the ramp is fully closed then release Cargo area lighting is turned OFF in the following steps Toggle the switch labeled BAGGAGE on the RAMP CONTROL PANEL downwards to OFF position to turn off the internal cargo area light Toggle the switch labeled CARGO on the RAMP CONTROL PANEL downwards to OFF position to turn off the external cargo area light Upper cargo door is closed in the following steps Push the door handle center button to release the handle form its recessed position Support the door and turn the handle clockwise and leave handle in open position NOTE The upper cargo door is equipped with dampers to reduce door closing speed Pull upper door to rest on the ramp and turn handle counter clockwise to closed position Push handle into the recess by pushing the handle ends Check area and notify the crew that loading is complete and that area is clear 16 Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway CAUTION Please note that the Sikorsky S 92A rotor downwash
61. ate vicinity of the helideck The locker must be painted red and marked Brannbeskyttelse and Fire Protection In addition to the required numbers sets of fire protection equipment the locker must also contain e two lifelines with a minimum length of 30 m e fire inhibiting blankets The member of the helideck crew who is stationed at the foam cannon shall wear all the fire protection gear described above apart from the smoke diving equipment During take off and landing when there is reason to believe that a hazardous situation may arise on the helideck all persons who make up the helideck crew must wear fire protection gear DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 10 2 12 2 13 OLJEINDUSTRIENS LANDSFORENING Coverall used for work on the helideck must meet the requirements for fire safety according to EN 531 The HLO shall clearly be marked front and back with the letters HLO or by an armband so as to be easily identifiable by the helicopter crew Manning the helicopter deck The helicopter deck shall be manned by minimum three persons e HLO In charge of the helicopter deck e Heliguard e Fireguard These are nominated as the Helideck Crew They must be able to document that they have completed their familiarization in the use of the helicopter deck s fire fighting equipment including the training stipulated in Chapter 2 7 During take off and landing a
62. atfjord B HLO say again your call sign The call sign of the helicopter The call sign of the helicopter may be the flight number of the helicopter in question e g Helibus 012 or the registration letters of the helicopter usually abbreviated to the first and the last two letters e g LN OMN LMN Radio failure Even though modern radio equipment is reliable radio failure between the helicopter and the helicopter deck crew cannot be excluded In practice a suspected loss of contact will arise when a helicopter fails to respond when called or if the frequency becomes silent In the event of a suspected radio failure contact should be made with another member of the helicopter deck crew or the radio operator so that the helicopter pilot can receive information As an exception hand signals may be used to indicate that the helicopter deck is clear for landing Hand signal OK Phraseology During radio communication between the helicopter and a ground station certain words and expressions known as phraseology are used in order to ease understanding The most possible use of standard phraseology is recommended Enclosure D contains a list of standard English expressions with their Norwegian equivalent DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 28 OLJEINDUSTRIENS LANDSFORENING 4 3 7 Frequencies The information frequency for helicopter services is used for e Deck clearance
63. ckmanual rev 01 09 2011 Enclosure F7 to OLF Helideckmanual rev 01 09 2011 Agusta A109E LUFTINNTAK ANTIKOLLISJONSLYS EKSOS GROUND GRAVITY HERE FUELING FLOATATION D R BAGGASJE HANDTAK ROM begge sider L i Maks totalvekt 2850 kg Maksimum lengde 13 04m Rotor diameter 11 00m Antall seter i kabin offshore 5 Understells bredde 2 15m Maks last i lasterom 150 kg Understells lengde 3 54m H yde under flat rotor 3 10m Enclosure F7 to OLF Helideckmanual rev 01 09 2011 Crash Chart of Agusta A109E Emergency shut off Lift plastic covers and press buttons zz LUFTTRANSPORT To open pilot door either side of To open passenger door either side of helicopter Lift latch and open door helicopter Lift latch and slide rearwards Agusta A109E e D value ee eseseeeeee 13 04 meters e Height under level rotor 3 10 meters e Rotor diameter 11 0 meters Enclosure F7 to OLF Helideckmanual rev 01 09 2011 enclosure G to OLF Helideckmanual rev 01 09 2011 Handling the helicopter during take off and landing This enclosure contains a step by step description of the most general operations on the helideck for a helideck crew consisting of 3 persons e HLO Helicopter Landing Officer In charge of helideck e Heliguard e Fireguard The HLO is the heliguards and fireguards superior Task allocation between Heliguard and Fireguard should be adapted to l
64. do not have direct access to DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 25 4 2 4 4 2 5 4 2 6 OLJEINDUSTRIENS LANDSFORENING alternative escape routes push out windows Passengers must not be placed in seats where the adjacent push out window is blocked or in a seat where cargo hampers free access to the nearest such window e Cargo must not be placed in the centre aisle Exempted are pipes with a diameter of up to 10 cm e Cargo must not hamper access to emergency equipment e Cargo must be secured in accordance with the authorities strictest requirements e Cargo must primarily be placed in front of the passengers in the cabin Luggage free cabin Passengers may not bring hand luggage with them into the helicopter cabin All form of bags briefcases portfolios etc are considered to be hand luggage and consequently prohibited Reading matter magazines newspapers are exempted Transporting cargo in passenger seats If cargo is to be placed in a passenger seat the following restrictions will apply e Max one package per seat with a maximum weight of 80 kg NB Single packages weighing up to 15 kg may be transported accumulatively in a sack with a total weight of no more than 80 kg e The sack s exterior measurements must be less than the height and width of the seat e In addition to the seat belt the cargo must always be secured by a strap cargo net or other
65. e Enclosure E for examples of such a training programme All basic and refresher training must be documented Experience Helicopter deck crew members who have only recently completed their basic training shall participate in a minimum of 20 helicopter landings and take offs under the guidance of an experienced HLO before being fully qualified to stand independent duty and becoming part of the minimum manning of the helicopter deck Such training should be conducted on an installation with heavy helicopter traffic Reference is made to OLF guidelines 074 para 9 Helidekkbemanning og kompetanse Norwegian only Personnel who have completed their training in accordance with item 2 7 but who have not acted in that position during the past two years shall have a thorough introduction to the helideck and refuelling plant in question under the guidance of the HLO Personnel who have not acted in a position on the helideck during the past four years must retake the basic HLO training course Personnel who are to act as HLO should have held a regular position as heliguard and or fireguard for a minimum of one year before being allowed to fill the position as HLO The installation should furthermore facilitate education and training for the new tasks he she will face as HLO Physical fitness Helideck crews must meet the same physical fitness requirements as those applicable to response personnel participating in search and rescue teams This
66. e being 15 x 15 metres The meshes in the net shall be so dimensioned that they do not snag the helicopter s undercarriage The rope net must be fastened every 1 5 metre To ensure that the rope net is kept sufficiently taut at least 50 of the fastening points shall be fitted with tightening mechanisms The net shall be so taut that it cannot be lifted more than maximum 25 cm clear of the surface A rope net is not required on installations where the surface of the helicopter deck consists of single profiles with special friction arrangements safe deck DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 16 OLJEINDUSTRIENS LANDSFORENING The requirement for rope netting on non movable helidecks may be deviated from provided that the deck is suitably constructed and there is a system in place to ensure that the helicopter can not skid and that the friction coefficient is at least 0 65 The requirement for rope netting can not be deviated from if there is snow or ice on the helideck Visual aids The term visual aids means windsock markings and illumination of the helideck Windsock The windsock must be Easily visible e Mounted in an area minimally affected by turbulence from surrounding constructions e Single coloured orange or dual coloured orange white red white or black white conically formed and of sufficient size Standard size inner diam 60 cm outer diam 30
67. e fuel nozzle flip out handle and turn the cap in the direction shown on the cap When closing the fuel cap turn cap in direction shown on the cap and flip in handle Note that the handle can only be flipped in if the cap is properly closed Na PLASTIC SS LANYARD Vh P Y 9 HANDLE NOSA A PN ev FILLER LEE A d me Emergency EMERGENCY EXITS Figure 3 3 Figure 3 4 and Figure 3 5 show the positions of the aircraft entrances and exits EMERGENCY PUSH HERE EMERGENCY EXIT PUSH WINDOW AT ANY CORNER EMERGENCY EXIT PUSH WINDOW AT LOWER CORNER ICN 39 A 153000 A 00003 00343 A 01 1 Figure 3 3 External Markings and Placards Enclosure F5 to OLF Helideckmanual rev 01 09 2011 Red strap to remove window remove cord NOTE Pull red strap to remove cord completely by moving in both directions from the strap When cord becomes free locate red strap attached to rear edge of window and pull inwards to remove window Eject window through opening EMERGENCY EXIT PULL RED STRAP TO REMOVE CORD ICN 39 A 153000 A 00003 00372 A 03 1 Figure 3 4 Internal Markings and Placards A E 1 PULL RED STRAP TO REMOVE CORD EMERGENCY 2 PUSH OUT WINDOW PUSH HERE ICN 39 A 153000 A 00003 00373 A 01 1 Figure 3 5 Internal Markings and Placards Enclosure F6 to OLF Helideckmanual rev 01 09 2011 WESTLAND SEA KING eee eo oer eo Hoe oo Cargo door internal view Enclosure F6 to OLF Helide
68. e in position both sides place these in position and receive deliver shall have chocks the manifest from to the pilot 3 Within the safe zone for the rotor take up a position that ensures eye contact with the pilot and a full view of the helideck enclosure G to OLF Helideckmanual rev 01 09 2011 Helicopter on the helideck From When the helicopter stands on the helideck with rotor engaged and chocks in place To cleared When the helicopter is loaded with passengers and cargo and the helideck is Operation Disembarking and unloading 1 Remain in the best position for eye contact with the pilot and a total overview of the helideck 2 When the helicopter has its rotor engaged all personnel movement shall primarily take place at a 90 angle to the longitudinal axis of the helicopter and thereafter outside the rotor disk See enclosure B HELIGUARD AND FIREGUARD 1 Install any required railings at the exit 2 Open baggage compartment hatches unload baggage and cargo 3 Place any baggage outside the passenger door or together with the cargo on the baggage trolley 4 Open appropriate cabin doors and let out passengers who will carry their baggage to the exit stairway as directed NB Only one cabin door must be opened so that loose objects cannot be blown out of the helicopter Make sure that the passengers keep a tight hold on any light objects Operation Embarking and
69. e protective cover over the hose connector must also be checked to ensure that it is in place 5 12 Fuel delivery refueling 5 12 1 Refueling crew Refueling shall be carried out by competent personnel who are well trained in procedures and operating the refueling system The crew shall be sufficient to ensure a safe operation and to be able to react properly in the event of an emergency The personnel shall be familiar with the location and operation of the emergency stop buttons The requirements relating to personnel competence are to be found in the OLF Guidelines The step by step duty of each individual member of the helideck crew during take off and landing is described in enclosure K 5 12 2 Earthing between the helicopter and the refueling equipment The helicopter the supply unit the filling nozzle pressure connector shall be connected in order to lead electricity during the whole of the refueling operation This is to ensure that electrical potential difference in current does not occur between the units Earthing between the helicopter and the supply unit shall be completed before any hose is connected to the helicopter or any tank cover opened The earthing must remain connected until all hoses have been disconnected and the tank cover replaced 5 12 3 Refueling procedures General e Refueling during local heavy thunderstorms is forbidden e Hoses must be removed in such a manner that they are not damaged Twisting or b
70. ected to the pump s manifold system 5 11 5 Transferring fuel between the transport and the storage tank The following tests must be conducted to verify the quality of the fuel when transferring fuel from the transport tank frame to the storage tank and or during the transfer of fuel between different storage tanks e Visual check e Water detector test on a 3 5litre sample taken from the tank frame tanks drainage point Make sure that the tank that is to receive the fuel has sufficient volume to accept the transferred fuel When transferring from the transport tank e Connect the earth cable to the transfer tank e Connect the transfer hose and open the tank valve e Start to transfer the fuel the fuel must be lead and not allowed to fall freely into the tank e When the transfer is completed disconnect the dry connection hose and the earth cable After the fuel has been transferred Conduct a visual check Allow for a settling time of one hour per meter of fuel in the tank Take a 3 5litre sample from the tank s drainage point and perform a water detector test If the sample contains sediments and or free water new samples must be taken until the sample is free from sediments free water The process must be repeated until satisfactory results are achieved If the test is still not satisfactory after the fourth settling period investigations corrective measures shall be initiated 5 11 6 Labelling and changing tanks
71. ed that when inspecting a long hose under full pressure a vertical loop is formed and that the loop is then rolled along the length of the hose Special attention must be paid to any indication that the hose connections are beginning to loosen With the hose fully extended release the pressure and inspect for soft spots Special attention must be paid to the part of the hose that is about 45 cm from the connectors as this area has a special tendency to weaken This part must be checked for faults by applying pressure around the area in order to discover soft spots bubbles etc DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 37 OLJEINDUSTRIENS LANDSFORENING 5 9 Pressure connectors Whenever refuelling all connectors must be checked for leaks Leaking connectors must be taken out of use Repairs and adjustments shall be logged and carried out by authorised personnel 5 10 Filling nozzles A general inspection of the filling nozzle shall be carried out at each delivery At any sign of a leak the filling nozzle must be taken out of use Repairs and adjustments must be logged 5 11 Receiving fuel and checking the delivery Before the tanks are filled onshore they are inspected and approved and a tank inspection certificate is issued by the fuel distributor The HLO must check that the labelling and traceability between the documents and the tank are in agreement Check that the transport ce
72. en radome Figure 7 Radome The nose compartment is enclosed by the radome The aircraft battery is located inside The radome is secured using two lever latches WARNING PITOT TUBES MIGHT BE VERY HOT AND CAN CAUSE SEVERE BURNS IF TOUCHED To open the radome both latches have to be opened e Push the recessed button on the latch e Pull the latch to open position e Liftthe radome upwards Encl F3 to OLF Helideckmanual rev 01 09 2011 se Bristow No rway Disconnect battery To disconnect battery Rotate connector counter clockwise Remove from battery Figure 8 Aircraft battery The aircraft battery is installed in the nose compartment To disconnect the battery e Open radome e Rotate the battery connector counter clockwise CCW until disconnected from the battery e Move connector away from battery Encl F3 to OLF Helideckmanual rev 01 09 201 1 s92 Bristow Norway Cockpit switches General There are several switches in the cockpit to perform various tasks concerning shutting down the engines APU and disconnecting the battery together with fighting fire Since fighting fire requires electric power the fire fighting must be performed prior to disconnecting all power sources Also applying rotor brake can not be performed with the engines running Engine and APU fire Figure 9 Engine and APU fire indication and arming On the center part of the instrument panel glareshield three combined indica
73. ending the hoses should be avoided Pressure connectors or filling nozzles shall not be dragged along the ground Dust caps must be in place as long as pressure connectors filling nozzles are not in use e During refueling the delivery unit must be checked for leaks the differential pressure of the filter monitors observed and logged and the other instruments read off and otherwise kept under observation e Spilt fuel is both a fire hazard and a danger to the environment Hot helicopter engines may be a source of ignition and extra care must be taken during DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 41 OLJEINDUSTRIENS LANDSFORENING 5 12 4 5 12 5 5 12 6 5 13 5 13 1 refueling Should any spillage occur all refueling must be stopped and the necessary measures implemented according to local requirements routines Refueling with the helicopter s engines running hot refueling Refueling the helicopter with the engines running hot refueling is an operation that demands very strict safety requirements The fuel supply delivery station must be manned in order to operate the unit Defueling Helicopter Defueling shall be done with the same personnel and according to the same safety procedures as for fueling The HLO shall ensure e that all returned fuel is of known quality and type JET A1 e logging of returned amount of fuel and where it is returned from e that retur
74. ever if the information is available or even only partially available i e number of passengers it can be useful to the pilots for fuel planning purposes etc The pilots will confirm information in this section upon arrival In case of multiple landings the ROUTING fields can be used to indicate routing including exchange of passengers i e 1 XXA 8 9 2 XXB 9 11 NOTE An information update of relevant weather movements and log info i e return load for the installation shall be submitted to the arriving helicopter upon initial radio contact See also enclosure Radio communications Helideck nonconformities Any helideck nonconformities shall always be filled into the form Examples ships within the 500 meter zone non conformities of helideck equipment temporary objects close to the obstruction free zones deviation from standard helideck procedures flaring of gas other info which may be useful to the pilots Weather observation All weather information shall be filled into the form but some exceptions as per local procedures If the installation is covered by HFIS services the QNH and the cloudbase field might be DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 12 OLJEINDUSTRIENS LANDSFORENING omitted If the installation is covered by local METAR services the cloudbase field might be omitted writing see metar in the field Wind Wind direction shall be stated
75. ew the exercise scenario with the involved personnel placing it in relationship to the installation s emergency plans with the main emphasis on the procedures applicable to the helideck crew Clear the exercise with management regarding the use of personnel etc Inform and instruct all who are to take part in the exercise simulated injured and any other personnel Make sure that the materials and equipment to be used are ready for use 5 Implementation The HLO will run the exercise and direct the emergency teams based on his evaluation of the accident site and other relevant factors Ensure that personnel are rotated through the various positions so that all may experience the different tasks Pay special attention to exercising the elements mentioned under sections 2 and 3 6 Material and equipment A small container simulated helicopter Jacks cutting equipment Fire fighting equipment Communication equipment 7 Follow up Go through the checklist for the helideck Return all equipment to the proper place and tidy up Carry out an evaluation of the exercise where all elements of importance are noted for use in the transfer of experience and any required documentation Note who has taken part in the exercise file the information for use as documentation in the event of an audit 8 Estimated duration Approximately 2 hours enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 2 Subject Communicat
76. form Date Flight no Helicopter Company Registr Letters Call sign Litres filled Water sample Before After filling filling Pilots signature Daily inspection Water purity test Diff press filters Tank OK Separator OK Monitor OK Monitor daglig Separator weekly Inspection hoses connectors nozzles earthing cables Total sampled volume per day HLO sign enclosure C to OLF Helideckmanual rev 01 09 2011 Hose inspection and test journal Manufacturer Hose identification no Type of hose Length Date of production Diameter Hose with connector Factory installed Locally installed mark Date taken in use Location Date of test Inspection interval Test result Signature Monthly Yearly o y O Use one page for each hose that is in use or in storage enclosure C to OLF Helideckmanual rev 01 09 2011 Inspection and cleaning log fuel tank Jet A 1 Installation Tank no Capacity Non corrosive type of interior surface treatment Date of inspection Point of inspection Signature of inspector State the approximate volume delivered since last inspection cleaning Descr
77. fuel oil or other liquids that can cause a risk of fire or a possibility of dangerous pollution of the aircraft it s systems or equipment or a danger to persons on board L Helideck installation Helideck blocked by aircraft vehicle birds or other objects that could lead to a dangerous or potentially dangerous situation Errors or defects in the markings of infringements or dangers in the helideck safe landing area that leads to a dangerous situation Errors in considerable functional error in or deficiency on the helideck lighting Considerable spill of fuel during fuelling HO L Li Fuelling of wrong amount of fuel which can seriously influence the aircrafts range performance center of gravity or structural strength Handling of passengers luggage and cargo Considerable pollution of the aircraft it s systems and equipment caused by freight luggage or cargo Erroneous loading of passengers luggage or cargo that may cause a considerable impact on the aircrafts weight and or balance Wrong loading of baggage or cargo including carry on baggage that may imply a danger for the aircraft it s equipment or persons on board or that may obstruct emergency evacuation Wrong loading of cargo containers or other major cargo units OO O O LJ Carriage of or attempts to carriage of dangerous goods not in accordance with rules and regulations including wrong markings or package of dangerous
78. gers in this manner 8 Estimated duration Approximately 1 hour enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 5 Subject Response times when alerted notified of an emergency situation 1 Purpose Training the helideck crew in meeting the requirements regarding an acceptable response time in the situations described in the lesson 2 Training objectives At the end of the lesson participants shall be able to meet the required response times and understand the importance of being able to do so 3 Content Training in accordance with the muster plan finding and donning the equipment necessary to tackle the defined situation 4 Preparation Clear the exercise with management regarding the use of resources Agree on the sounding of the muster alarm with the rest of the emergency organisation 5 Implementation May be implemented by specially addressing this field during standard muster exercises on the installation Individual muster exercises for the helideck 6 Materials and equipment All the emergency equipment that is required to meet the described emergency situation in a satisfactory manner 7 Follow up Carry out exercise evaluation emphasising areas for improvement regarding time used on operations that are necessary to meet the requirements given in paragraph 1 Carry out an evaluation as to whether the available equipment is properly positioned and if it is the right equipment wit
79. goods Ground handling and service on the aircraft Filling of wrong type fuel or other important fluids including oxygen and drinking water OLI Discovery of open inspection panels doors missing fuel cap etc Form no NOR F 015 enclosure M to OLF Helideckmanual rev 01 09 2011 History of the event Name Occupation Instructions Fill in form scan or E mail to operations centre of the involved helicopteroperator Report to be forwarded ASAP and within 72 hours Form no NOR F 015
80. h regard to weight user friendliness etc Note who has taken part in the exercise 8 Estimated duration Approximately 1 hour enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 6 Subject Medical evacuation under extreme weather conditions 1 Purpose Training the helideck crew in dealing with a medical evacuation in extreme weather conditions 2 Training objectives At the end of the lesson participants will have learnt about differ ways of carrying out a medical evacuation In cooperation the remainder of the emergency organisation be able to take part in evaluation and implementation if a litter basket must be hoisted from a location other than the helideck 3 Content The use of equipment for medical transportation Coordination and communication with the remainder of the emergency organisation 4 Preparation Clear the exercise with management regarding the use of resources Review the scenario with the involved parties place special emphasis on individual safety during the exercise 5 Implementation The exercise is conducted by training in stretcher transportation from different areas on the installation Mapping the installation in order to chart alternative hoisting zones should the helideck for any reason be inaccessible 6 Materials and equipment Stretcher litter communications equipment cranes 7 Follow up Carry out an evaluation of the exercise with all involved parties
81. hall cover 20 minutes of data and alternatively 3 hours for trend determination The graph and the associated max value last 20 minutes shall be updated at least at 1 minute intervals 6 5 Heave Period The equipment shall be capable of measuring the time between helideck movement summits in seconds i e based on a wave curve the measurement starts and ends in the zero up crossing point The graphical presentation shall cover 20 minutes of data and alternatively 3 hours for trend determination The graph and the associated max value last 20 minutes shall be updated at least at 1 minute intervals 6 6 Max Average Heave Rate The equipment shall be capable of measuring the vertical movement rate of the helideck in metres per second The heave rate measured shall be the mean vertical rate for a movement range from top to bottom within one cycle over the past 20 minutes The Maximum Average Heave Rate value is calculated directly from the Maximum Heave and the associated Heave Period described above in accordance with the following formula Maximum Average Heave rate m sec Maximum Heave divided by 1 2 of the associated Heave Period It shall be possible to read the historic maximum value for the past 20 minutes direct and graphically The graphical presentation shall cover 20 minutes of data and alternatively 3 hours for trend determination The graph and the associated max value last 20 minutes shall be updated at least at 1 minute intervals
82. hapter 7 covers specific requirements relating to installations and companies Purpose and scope The purpose of the manual is to describe the areas of responsibility on the helideck requirements to the helideck crew and their equipment and to determine how activities and tasks are managed and conducted so that operations on the helideck are executed in a safe and proper manner The manual is intended to contribute to the safe conduct of helicopter operations on the Norwegian shelf by ensuring uniform standards and behaviour Responsibilities OLF is the owner of this document and is responsible for either updating or revoking the document should organisational or operational conditions so require OLF s Expert Group on Aviation matters in cooperation with the helicopter operators on the Norwegian shelf are to assume this responsibility Approval The document has been approved by the Committee for Development and Operations and has been verified by CHC Helikopterservice A S and Bristow Norway A S Distribution and Amendments The document is included in OLF s set of regulations and is available via OLF s home page on the Internet http www olf no The latest amendment dates will be published here OLF member companies will be notified in writing of any amendments The operating companies internal distribution lists are shown in Chapter 7 References The following documents are relevant for the contents of this ma
83. he EC225 Please observe the following guidelines and restrictions when using this facility Maximum load in each sponson is restricted to 200 Kgs Flammable material and Dangerous Goods DG is prohibited Only offshore bags and soft coated items are allowed Maximum weight per item is 10 Kgs All other baggage and cargo shall be loaded in 1 amp 2 Left sponson is referred to as cargo room 4 or left sponson Right sponson is referred to as cargo room 5 or right sponson It is favourable to load bags into the cargo sponson as this moves the centre of gravity forward HLO is responsible for the supervision of proper closure and locking of the cargo pods and to provide the A C Commander with confirmation of this before he or she gives the thumb up signal This information should be given at the same time as the information about load in cargo room 3 is given E g 20 Kgs of cargo in compartment 3 Cargo sponsons checked and secure 16 enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway CHC Sikorsky S 92 crash charts are the same as for Bristow S 92 as per enclosure F3 Sem er enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway fr GROUNDING POINT Passenger seating configuration enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway Doors and exits EMERGENCY EMERGENCY exir EXIT enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway BP
84. hting equipment e Sound the alarm e Don fire protection gear The fireguard is already wearing his e Determine the source of the fire s DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 44 OLJEINDUSTRIENS LANDSFORENING Areas of responsibility HLO Alerting Notification Confers with pilot and coordinates actions If the type of fire allows confer with pilot before using fire fighting equipment Heliguard Works with fireguard and HLO in fighting fire and reducing risk Fireguard Operates the fire fighting equipment Fire Teams In extensive fires the fire teams on the installation will be involved in extinguishing the fire and will take over the responsibility from the helideck crew Rescue In some cases it will be possible to save the helicopter crew passengers before the fire becomes too large If rescue appears to be possible then this should be attempted but the fire fighting equipment must be used to cover personnel involved in the rescue operation Should it be necessary to enter the helicopter cabin in order to save personnel one must e Use smoke diving equipment e Keep as low as possible when entering the cabin e Stay below smoke and gasses It is here the largest amounts of oxygen are to be found Fire watch When the fire has been extinguished a fire watch should be maintained at the site so as to avoid re ignition The carpet of foam sho
85. ibe the condition at the last inspection water or pollution the condition of the bottom plates and any surface coating Describe the work carried out during cleaning Describe any work or modifications Any change in inclination or drainage point shall be taken into consideration enclosure C to OLF Helideckmanual rev 01 09 2011 Transport log helicopter fuel JET A 1 Installation vessel Year Receipt of transport tank Return of transport tank Date Transp certificate no Tank no Seals intact Drainage samples Volume received Free of water Visual Detector Particles From certifica te Measur ed Sign Date Returned fuel volume Sealed Sign enclosure D to OLF Helideckmanual rev 01 09 2011 Phraseology In the Air Traffic Services certain words and expressions are used to ease understanding These are known as standard phraseology The highest possible use of standard phraseology is recommended In this enclosure there follows a list of the English standard phraseology and an explanation in Norwegian ABORT Idg to ACKNOWLEDGE AFFIRM APPROVED BREAK CANCEL CONFIRM CORRECTION DECK IS CLEAR DISREGARD GO AHEAD HOW DO YOU READ I SAY AGAIN MONITOR NEGATIVE PASS YOUR MESSAGE READ BACK ROGER SAY AGAIN SPEAK SLOWER STANDBY V
86. ible for routine inspections of the helideck and refuelling plant 24 Supervision The operating company is responsible for supervision relating to helicopter activities on the installation such as the helideck the refuelling plant the helideck crew the radio operator person responsible for communications radio and navigational equipment etc Such supervision is in addition to the installation s routine for maintenance and inspection 25 Maintenance programme A maintenance programme for the helideck its equipment and refuelling plant if installed is to be established and maintained 2 6 Audits The helicopter company and the The Petroleum Safety Authority Norway with professional support from the Civil Aviation Authorities will carry out periodical audits on the operator s systems installation 2 7 Training of helideck crews DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 8 2 8 2 9 2 10 OLJEINDUSTRIENS LANDSFORENING Basic and refresher training for helideck crew is to be carried out in accordance with the OLF curriculum The courses are titled HLO Basic Course and HLO Refresher Course The HLO Refresher Course must be taken within 24 months after the last HLO Basic Refresher course Refresher training on the installation should be carried out at least every 14 days for all helideck crews During this training special emphasis should be placed on fire and damage control Se
87. in baggage trolleys or similar should be secured with cargo nets Also persons located close to the helideck should be aware of the downwash particularly during landing and take off but also during embarkation and disembarkation of the helicopter Eye glasses or other loose items may under certain circumstances be blown off if not secured Please contact the crew if you have any questions 10 Encl F3 to OLF Helideckmanual rev 01 09 2011 se Bristow Norway Sikorsky S 92A Bristow Norway Bristow S 92A overview crash chart cargo compartment Engine Emergency Exit Cabin door Emergency Exit f Cockpit Emergency Exit Battery Compartment f Cabin Emergency exit 1 d vod v Emergency exit Singlepoint Refueling Cockpit Emergency exit Figure 1 S 92A overview Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway General The S 92A is a multi engine helicopter equipped with an Auxiliary Power Unit APU The engines and APU are located on the upper part of the helicopter A battery is located in the nose section The aircraft has four cabin and two cockpit emergency exists All of these exits can be opened from the outside by operating a single handle In order to stop the engines and APU switches in the cockpit must be operated in a correct order Details on how to do this is described in section Cockpit switches
88. ion 1 Purpose To maintain and develop the helideck crew s proficiency in using the existing available communications equipment and meeting the challenges caused by the loss of traditional communications equipment 2 Training objectives At the end of the lesson exercise the participants will have learnt about the use of traditional communications equipment and alternative means of communication based on local conditions 3 Content Training exercising with available communications equipment 4 Preparation Clear the exercise with management regarding the use of resources Go through the installation s emergency plan with main emphasis on the section relating to communication Develop the scenario in cooperation with the person responsible for communication onboard the installation and other relevant agencies control room crane and deck departments helicopter pilots etc Give thorough instructions to the players 5 Implementation The exercise is conducted as a pure Table Top exercise For this reason it is important the equipment is put into physical use when simulating during the exercise that someone really responds to radio calls and that someone answers the telephone when it rings and that these are fully briefed on the intentions of the exercise Make sure that all persons who could be involved in a real incident participate helicopter damage control leader control room radio nurse first aid teams etc 6
89. ion and immediately report any abnormal situation 4 Make sure that nobody leaves their position until 2 minutes after take off Make sure that everyone remains in readiness for another 15 minutes or until the helicopter has landed at another installation HELIGUARD 1 At the signal from the HLO remove the chocks from the left hand side 2 Do not leave position until two minutes after take off Listen on VHF in the event of a possible return of the helicopter to the installation 3 Maintain state of readiness as directed by the HLO 1 Don full fire protective clothing 2 Take up position at upwind fire post alternatively at the remote control unit 3 Do not leave position until two minutes after take off listen on VHF in the event of a possible return of the helicopter to the installation 4 Maintain state of readiness as directed by HLO enclosure G to OLF Helideckmanual rev 01 09 2011 Alternative access Procedures for alternative disembarking and embarking with guidance of the helideck crew This procedure shall be used if the normal procedure with access to the helideck on the same side as the helicopter entrance can not be used Operation Disembarking around the nose S 92A EC225 SuperPuma 1 Move from the side of the helicopter to the front of the nose inside the rotor tip approx 1m from the nose keeping eye contact with the pilots and both sides of the helicopter 2
90. ion may require 7 Follow up Take part in the exercise evaluation Note who has taken part in the exercise 8 Estimated duration 1 2 hours depending on the extent of the scenario enclosure E to OLF Helideckmanual rev 01 09 2011 Lesson Exercise No 4 Subject Behaviour on the helideck 1 Purpose To ensure that all traffic on the helideck is conducted in a safe and proper manner with emphasis both on one s own and the passenger s behaviour 2 Training objectives At the end of the lesson the participants will have learnt about correct traffic movement and behaviour on the helideck 3 Contents Information on and training in correct traffic and movement based on the limitations possibilities as dictated by helicopter gangways exits and other local conditions Special attention shall be paid to limitations caused by wind and weather 4 Preparations Clear the exercise with management regarding the use of resources Agree on a scenario with the helicopter crew and other relevant personnel 5 Implementation Give the participants a theoretical briefing on existing guidelines Test their reactions to irregular behaviour May be run as a live exercise or may be simulated Exercise great caution if run live 6 Materials and equipment 7 Follow up Carry out an evaluation of the exercise and document the result The subject may also be a good input at the installation s safety meetings by targeting the passen
91. is document 2 Definitions Moving helidecks A helideck mounted on floating units like Vessels Floating Production Units Semi Submercible Rigs floating Jack Up Rigs and other helidecks shall be considered to be an unstable moving landing area if the pitch or roll exceeds 1 degree either side of the vertical and if the vertical movement of the helideck exceeds 2 metres Helideck Inclination is the angle between the absolute horizon and the plane of the helideck Average heave rate is the average speed of the helideck between the top and the bottom of a wave movement curve Maximum average heave rate is the average heave rate on the one largest wave peak value within a 20 minute time frame in meters pr Second 3 Classification of helidecks There is no official classification method available for this purpose The classification is based on the actual floating units size and motion characteristics The method is based on experience built over the years in operation between CHC Helikopter Service and Norsk Helikopter The category will be entered on the individual vessel rig information plate in the North Sea Airway Manual and the Company Helideck Limitation List HLL Category A Large ships including productions ships and semi submersible rigs with measuring and monitoring equipment deviating from this standard Category A Cat A with measuring and monitoring equipment installed and functional in accordance with
92. is have to be available on the vessel installation If dangerous goods are to be transported in helicopters from offshore destinations the installation vessel has to have the following available Nominated Person Shipper and Packer Latest version of IATA DGR Goods Regulations available Shippers declaration forms Checklists Radioactive and None Radioactive NOTOC forms UN Specification packages Inner packages matching UN Spec markings Limited Quantity Packages Absorbent and Cushioning material Dangerous Goods Labels Provision of spill kits The transport of fish In order to avoid corrosion and or other damage to baggage the following restrictions will apply to the transport of fish e The fish must be packed in watertight containers or e The fish must be frozen and packed in plastic or a similar material in such a manner as to avoid damage in the event of thawing Personal Locator Beacon PLB Flights where passengers are equipped with personal Locator Beacons PLB to be left behind in the helicopter after the flight the HLO is responsible for departing passengers not taking their PLB s with them If any PLB s are left on the installation information of this incident must be communicated to the heliport which has the daily supervision of the PLB s 4 3 Communications This section of the manual contains procedures and guidelines for communication between the helicopter deck crew and the helicopter pilots See encl
93. k in operation shall be capable of remote closure from the helideck dispenser unit Operation preferably by pneumatic operated tank valve or alternatively by remote closure by wire In order to allow 4L sample jars to be used the sample point should be designed with sufficient access 250mm space and height to accommodate the standard 4 litre sample jar The sample line from tanks shall be minimum 3 4 The outlet fill connection shall be flanged with a 3 internal valve terminating to a 2 5 self sealing coupler with dust cap The tank outlet shall be at least 150mm higher than the lowest point of the tank The drain connection shall be equipped with minimum 1 5 internal valve terminating in a plugged ball valve preferably 1 The plug shall be installed on the end to prevent the ingress of dirt and moisture The stainless 2 5 emergency pressure vacuum relief valve should be fitted with weatherproof anti flash cowl enclosure J to OLF Helideckmanual rev 01 09 2011 Tanks not in use Tank shall only be located in defined safe area during settling and transfer to the static tank The selected tank shall only be connected during the transfer of Jet A 1 Tanks installed on the laydown skid Tanks in use shall have protective deluge system according to class requirements NMD or minimum 10 I m2 min Tank in operation shall be bonded by use of the bonding clip Static storage tanks Stationary tanks shall be constructed to suitable
94. lation nurse 4 Preparation 5 Implementation 6 Materials and equipment 7 Follow up 8 Estimated duration Enclosure F1 to OLF Helideckmanual rev 01 09 2011 Eurocopter Super Puma L L1 L2 and EC 225 Common Crash chart and operation of cabin doors Super Puma amp EC225 Procedure for opening and closing of cabin doors To close push here Open cabin door Pull the handle out and turn down to open position The door shall be fully released from the door frame Move the door forward to be locked in open position Close cabin door Rotate the door handle downwards and the door will release from locked in open position Lead the door to stop in aft position Push the door into the door frame and the door handle automatically moves to mid position Rotate the door handle to closed position Lights in the cockpit indicates if the cabin doors are open Enclosure F1 to OLF Helideckmanual rev 01 09 2011 CRASH CHART die J Super Puma all versions and EC225 NORSK 1 Access to cockpit If door is jammed use emergency release handle when fitted 2 Emergency cut off handles D handles will cut off electrical power and closes fuel valves Release 3 Access cabin for rescue by Releasing cabin doors jettison Opening escape windows pull tab Enclosure F1 to OLF Helideckmanual rev 01 09 2011 General information Eurocopter SuperPuma L L1 Super Puma AS 332 L L1
95. le center button to release the handle form its recessed position Turn the handle clockwise and leave handle in open position Push and hold the door in upper position Turn handle counter clockwise to locked position Push handle into the recess by pushing the handle ends WARNING A protruding handle may cause injuries to personnel during loading and unloading of the cargo area UPPER CARGO DOOR OPEN i Picture 1 Upper cargo door 13 Encl F3 to OLF Helideckmanual rev 01 09 2011 se Bristow Norway Upper cargo net Upper cargo net Snap latches Upper shelf Lower cargo net Snap latches Lower cargo net Lower shelf Storage box Ramp Picture 2 Cargo area Cargo ramp is lowered in the following step WARNING Cargo ramp should not be lowered all the way to the surface as this might cause resonance in the helicopter Toggle and hold the switch marked RAMP on the RAMP CONTROL PANEL from center position and downwards to LOWER position until the ramp is approx 4 8 inches above the surface then release RAMP ioc LTS RAISE BAGA 4 ARGO sig on y ww or Picture 3 Ramp control panel Cargo area lighting is turned ON in the following steps Toggle the switch labeled BAGGAGE on the RAMP CONTROL PANEL upwards to ON position to light up the internal cargo area Toggle the switch labeled CARGO on the RAMP CONTROL PANEL upwards to ON position to light u
96. ler connected to the sample point is recommended e A self closing valve on the 77 minimum drain connection Dispensing module The product flowmeter The product flowmeter must be sized to suit the flow rate and the counter must be resetable Nozzles Fuel delivery to aircraft must be available both by gravity and pressure refuelling Both types of nozzles must be provided with bonding cables and dust caps to prevent the ingress of water and dirt Gravity The gravity nozzle shall be fitted with minimum a stainless 60 mesh strainer and a bonding wire and clip A separate short length of hose 2 3m fitted with an adapter to fit the pressure nozzle and with the gravity nozzle attached is recommended Pressure The pressure nozzle shall be fitted to the hose end pressure control unit The nozzle shall be equipped with a surge controller rated to maximum 35 PSI The nozzle must be equipped with a minimum 60 mesh stainless steel cone strainer bonding wire and clip Hose reel amp fuel hose A fire safe antistatic ball valve shall be installed in front of the hose reel The 30m 1 5 delivery hose should be of an approved semi conducting type to API 1529 or BS EN 1361 BS3158 type C semi conducting Clamp type couplings must be used at hose terminations Fuel filter monitor A fuel filter monitor conforming to the API IP 1583 Specification and qualification procedures for aviation fuel filter monitors with absorbent type elements la
97. ll be absorbed onto the paper fibres releasing and spreading the colouring In this manner a distinct colour change will Occur If this change in colour takes place it means that the fuel is polluted by water and must consequently not be used The part of the paper that is protected by plastic will remain unaffected Any colour change between the inner and outer wet part or measured area is a positive indication of the presence of finely dispersed water A generally light pastel colouring over the whole centre of the detector or no colour at all can be approved A light yellow pastel colouring with darker specks or spots indicates that there are still some drops of water remaining suspended in the fuel which may be above the permitted maximum concentration of 30 parts per million 30 ppm Further precipitation discharging and separation is required to remove this water so that the concentration reaches below the level of 30 parts per million Large and darker specks or a generally darker colour in the centre of the detector will of course indicate the presence of even more water in the fuel This must be removed before it is safe for the helicopter to use the fuel When testing just before and after refuelling the helicopter let the pilot wet the detector after the test has been completed to see that the colour changes to green and to ensure that the detector was not defect On other occasions apart from refuelling e Wet the detector
98. ll upon a qualified person when increasing the manning of the helideck Flights to installations that are normally unmanned General information An unmanned installation is in this context an installation with a helideck operational according to regulations but has no personell onboard when the helicopter lands or takes off from the installation Flights to an unmanned installation should be limited to as few as possible and preferably be executed in daylight Transit passengers are not allowed in the helicopter If there are persons onboard the installation crewing and operations shall be as for a manned installation Exempted is when a helicopter returns empty to collect a group who has previously been offloaded at the same installation When flying to unmanned installations the helideck crew shall consist of at least two qualified heliguards One of these will become the HLO the other the Fireguard DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 48 OLJEINDUSTRIENS LANDSFORENING Both shall have documented knowledge of the installations helideck and equipment Both the HLO and the Fireguard shall be wearing approved survival suits during transit to from the unmanned installation At the latest the Fireguard shall put on firehelmet and gloves just before the helicopter approaches the helideck Both shall disembark the helicopter before any other passengers and take their positions
99. n the product from which the samples are being taken The containers must be properly dried before use The containers must not be filled completely Some 5 of the volume must remain in order to allow the liquid to expand Approved containers must be used these should be labelled and preferably sealed The containers must be sealed and labelled immediately after filling The label shall contain the following information e Date and time e Sample taken by signature e Installation vessel e Tank no e Batch no Documentation for all samples shall be logged A copy of the transport certificate shall be attached for each product 5 7 1 Containers e Containers for laboratory samples Glass metal or approved plastic containers for laboratory or duplicate tests must be either new or approved by the laboratory and absolutely clean Refer to ASTM D 4306 for suitable containers Metal containers must be approved and preferably have epoxy coated linings Even though they may be new all containers must be rinsed at least three times in the product from which the samples are being taken e Containers for visual sampling Clean transparent containers with a capacity of a minimum of 3 5 litres and a wide opening that will accept a threaded lid must be used for sampling If a bucket is used for draining it must be of stainless steel or perhaps white enamel and have approved earthing DOCUMENT NO REVISION NO REVISION DATE
100. ned fuel is settled and drained for free water and particles prior to readying the product for new deliverance Fuel which is defueled through waterseparator or monitor filter can be delivered without any prior settling and drainage Refuelling with Passengers onboard Refuelling with passengers onboard requires that the Helicopter pilot and HLO OIM agree and to follow standard procedures with addition of the following Pilot and HLO shall be present and in full control of the operation at all times All passengers must be briefed on the operation before fuelling commence Passengers must have seatbelts undone during refuelling procedures Doors on the refuelling side closed Doors on non refuelling side open Emergency egress route planned clear and known to all involved in the operation Helicopter Operator procedure in place and known to Helideck crew e Deck procedure known to helicopter crew Review over required documentation The results of all inspections and tests shall be logged on updated documents that are readily available These shall be kept for a minimum of at least one year As a minimum they shall contain Documentation Quality control Helicopter refueling log This form contains the requirements relating to daily sampling inspection Log for filter and differential pressure and transport log for helicopter fuel is also used DOCUMENT NO REVISION NO REVISION DATE 01 09 2011
101. nual DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 5 1 6 OLJEINDUSTRIENS LANDSFORENING The Civil Aviation Authority Regulations for Civil Aviation e BSLD 1 7 Regulations relating to the transport of cargo by civil aircraft http www lovdata no cqi wift Idles doc sf sf sf 20030111 0041 html e BSLD 5 1 Regulations pertaining to aviation on the continental shelf http www lovdata no cqi wift Idles doc sf sf sf 20071026 1181 html e BSLA 1 3 forskrift om varslingsplikt ifm luftfart http www lovdata no cqi wift Idles doc sf st sf 20061208 1393 html The Maritime Directorate e Regulations of 22 December 1993 no 1240 relating to helicopter decks on mobile installations http www lovdata no cgi wift ldles doc sf sf sf 200801 15 0072 html The Petroleum Safety Authority Norway the Facility Regulation 70 including the guidelines to the regulations ICAO TI Restricted Articles List Joint Aviation Authorities JAA Joint Aviation Requirements JAR OPS 3 Commercial Air transportation Helicopters OLF Guideline 074 Recommended guidelines for helideck crew chapter 9 Helideck crew and competence Definitions luggage free cabin passengers are not allowed to carry hand luggage with them onboard the helicopter exemptions are reading matters magazines newspapers anti collision lights powerful rotating lights above and below the helicopter f
102. ny stand by vessel close by is informed of the arrival of the helicopter and that no vessel is located within 1000 meters in the 180 degree zone or if higher than the helideck in the 210 degree zone Gather information on the arriving helicopter This includes estimated time of arrival location and amount of cargo number of passengers and any fuel requirements In difficult weather conditions special cargo evaluate the need for and requisition extra personnel 4 Make sure that the daily inspection of the helideck and refuelling plant has been completed with a satisfactory result 5 Furthermore check that the helicopter landing area is cleared of obstacles 6 Brief and if necessary allocate tasks to the Heliguard and the Fireguard HELIGUARD AND FIREGUARD 1 Meet at least 15 minutes before arrival time 2 Prepare the cargo that is to be sent 3 Check and prepare fire fighting equipment 4 Receive the manifest and information on number of arriving and departing passengers 5 Don the necessary clothing and portable VHF Operation 5 minutes before the estimated time of arrival of the helicopter HELIGUARD 1 Make sure that the crane drivers are informed 2 Monitor radio communication between the helicopter pilot and the installation or HFIS 3 Make sure that the passengers are ready and remain in a safe zone without access to the helideck Physical barriers shall be used 1 St
103. ocal conditions to ensure safe and efficient operations Work tasks in addition to this may be given as required The described operations are based on the assumption that there are exit stairways from the helideck Where this is not the case the installation will use approved alternative departure routes from the helideck The principle behind this procedure is through standardisation and by relieving the HLOs of as many tasks as possible trying to achieve optimal safety levels across the companies on the Norwegian Continental Shelf The helicopter companies emphasize that during helicopter operations the HLO shall have a full overview of the helideck area be in visual contact with the pilot and be able to run control the operations in such a manner that any potential danger is registered and effectively eliminated Apart from what is laid down in this procedure if the HLO has to leave his position the pilot must be informed enclosure G to OLF Helideckmanual rev 01 09 2011 Helicopter arrival From When the Heliguard receives notification from the radio communications officer that a helicopter is expected To Until the helicopter is steady on the deck with rotors moving and chocks in place Operations Well in advance of the arrival of the helicopter 1 Verify the arrival time of the helicopter 30 minutes before the estimated time of arrival 2 Meet at the helideck at least 20 minutes before arrival 3 Verify that a
104. ommunicating with the crew of the helicopter and the installation s radio room 3 1 11 Signs Access routes to the helicopter deck shall be marked with clearly visible signs prohibiting e Presence on the deck during start and landing DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 18 OLJEINDUSTRIENS LANDSFORENING e Movement of personnel on the helicopter deck behind a parked helicopter with the rotor engaged e Exits steps from the helicopter deck shall be clearly marked with EXIT The text shall be visible in the dark 3 1 12 Marking of closed Helideck A helicopter will normally not land before a deck clear message is received from the HLO but in an emergency or by misunderstanding this can still happen A helideck that is not marked as closed is therefore assumed safe to land on without any threat to the helicopter or personnel on the ground To ensure against this the helideck shall be marked as closed if a landing will give unacceptable consequences The Marking shall be used f the helideck is dangerous to land on for example due to work in progress with loose objects weakened structure obstacles like wires stretched above the helideck ao NB Does not normally apply to crane operations because the crane structure will be visible to the pilots If landing will represent a danger to personnel on or near the helideck f another installation with helideck is clo
105. on Configure Po EE EE A 0 4 Up 5 Down Pitch i 1 22Stbd VScale a s 15kts 23 kts 10 min 10 min HScale 4 Omn imt Wind speed Gust Wind speed S Wind measurement Heave Vessel motion Configure Meteorological data Configure 2 mis Weather 5 a Omis Max Avg Heave rate Air temperature OAT Clouds few sct bcn ovc in feet 60s o vass 36 sec 5 C Os Heave periode Dew Point Temperature Se Visibility K vane A AAA 5 4m ee mm 1050 hPa sen Max Heave Sea spray observed over helideck C YES NO Air pressure QNH 10 min HScale 4 Omin limit Dynamic positioning YES C NO Data log 48 hrs Loscontral Sensor status MRU Wind Light Seapath Air Temp 9 AirPress Nav Gyro HMS Norsk Standard rev 4 12 1 2004 enclosure L to OLF Helideckmanual rev 01 09 2011 9 Attatchment 2 Logistics Information display Data Display layouts shall be approved by the Helicopter Operators Typical layouts are attached ABC N 63 26 31 356 E 10 24 12 196 XXA 8 49 O 5 911 XXO S EOD OS ashkjhaskjaksj asdklajsikasjdlak askjdakl ajksj asdj 17 Oct 2003 08 01 33 GMT HMS Norsk Standard rev 4 12 1 2004 enclosure L to OLF Helideckmanual rev 01 09 2011 10 List of known motion measurement equipment producers KONGSBERG SEATEX AS Att J Magnus Leirvik Pirsenteret N 7462 Trondheim Norway Tlf 47
106. ons describe the scope for these rules and regulations Laydown area for transit tanks Laydown skid The drip tray shall be sized to hold 100 of the content of one tank The laydown skid must be equipped with a 2 or preferably 3 drain connection To protect the deluge system pump unit from damage during tank handling a guide buffer frame is recommended welded to the base of the skid Transportable tanks should be properly sea fastened on moving vessels A valve shall be mounted on the Jet A 1 outlet point skid edge A convoluted stainless steel suction hose with a 2 5 dry break coupling shall be used to connect the transit tanks to the pump unit Other end should be sized to fit the pump unit inlet flange ANSI 150lbs The base frame shall be bonded from two different locations Deluge system A Deluge system shall be installed according to design criteria A calculation report hydraulic calculation for the deluge system shall be available upon the surveyor s request Fire detection Acc to class requirements or Oil companies specification Transit tanks Transit tanks shall be constructed to satisfy DnV 2 7 1 amp IMO IMDG requirements They shall also conform to the dangerous goods Code Type 1 or 2 Transit tanks shall have a suitable dipstick preferably of fibreglass material Tanks should preferably be of stainless steel or lined with a suitable fuel resistant epoxy lining The tank outlet valve on the tan
107. opter a passenger cargo manifest must be completed and accompany the helicopter When the passenger cargo manifest has been completed it is considered to be an official document and therefore subject to inspection The standard weight per passenger including survival suit is 211 lbs 96 kg for men and 174 Ibs 79 kg for women The weight of cargo luggage comes in addition The manifest shall contain the following information The full name of the passenger Employer The weight of the passenger The weight of the luggage per person Weight of cargo luggage Description of the content in each package Destination When sending cargo from an installation to shore the HLO is responsible for checking the manifest and ensuring that it accompanies the transmittal The HLO is responsible for checking that the number of passengers onboard complies with the passenger manifest and that the manifest is handed to the helicopter crew In loading the Super Puma the pilot shall be informed of the total load in cargo compartment 3 Cargo and passengers together in the helicopter cabin As arule when transporting passengers cargo must not be placed in the helicopter cabin When exempted the following shall apply e Only prioritized cargo e Cargo shall not be blocking the cabindoors e Cargo must not block the main exits from that part of the helicopter cabin where the passengers are seated e Cargo must not be placed so that passengers
108. ore force to enter the helicopter cutting must only take place at specific points e g emergency exits and windows The rescue equipment listed in Chapter 3 is to be used Should a helicopter be lying on its side those onboard must be supported when the seat belts are released NB The helideck crew must have detailed knowledge of the type of helicopter as described in emergency procedures in Enclosure F Choking stopping the engines shall be carried out when The helicopter is in a normal position and the pilots are put out of action The engines and the rotors are still running Stop the engines with the helicopter s emergency stop handle Be aware that the rotor blades move closer to the deck as rotation speed drops This may constitute a major hazard to personnel on the deck Do not allow personnel to leave the helicopter until the rotors have stopped 6 1 4 Crash into the sea Alerting DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 46 OLJEINDUSTRIENS LANDSFORENING Make sure that the radio operator is notified The radio operator control room will carry out further notification in accordance with the installations internal procedures The helideck crew shall act in accordance with the installation s emergency procedures manual Emergency landing with prior notification Preparations If warning has been given that a helicopter is experiencing problems and wishes to
109. osure I for guidance to radiocommunications 4 3 14 Language Normally all aeronautical communication is in English It may however be more practical to communicate in Norwegian if the English capabilities are limited and both parties speak Norwegian DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 27 4 3 2 4 3 3 4 3 4 4 3 5 4 3 6 OLJEINDUSTRIENS LANDSFORENING Responsibilities The HLO will inform when the helideck is cleared for landing He will also provide safety related information e g that the helideck may not be used due to an alarm that the undercarriage is not lowered loose articles that may have struck the rotor oil or fuel leaks or faults with the helicopter loose covers etc The HLO may not assume control of the air space or exercise air traffic control over the helicopter traffic Establishing radio communications Prior to establishing radio communications one should ensure that e The correct radio frequency is being used e Listen first so as not to interrupt ongoing communications e Be aware of what one wants to say If a radio station hears a call without being able to identify the call sign of the station being called it shall not answer until the call sign has been repeated and understood If a station receives a call without being able to make out the identity of the caller the following terminology shall be used Station calling this is St
110. ot and the airline company must be informed immediately No further fuel must be delivered until the cause has been found and rectified Specific weight measuring density measuring According to the specifications the specific weight density of Jet A 1 lies in the area of 0 775 0 840 kg litre The specific weight density of the product must be checked when received offshore The specific weight is checked by the use of a hydrometer and a thermometer may be built in as part of the hydrometer The test must be conducted in a well lit area protected from rain and wind The hydrometer shall be sunken slowly and carefully into the fuel This is to avoid breakage or it becoming wet above the flotation level Care must be taken to ensure that air bubbles do not attach themselves to the submersed surface The hydrometer must float freely The hydrometer must float for some three to four minutes so that its temperature and movement are stabilised Then carefully push the hydrometer down 2 marks on the scale and release Once the hydrometer has re stabilised read off the specific weight density The fuel will creep slightly up along the thermometer so that the level indicated on the scale will be above the real fuel level Look along the surface of the fuel and read off at the lowest indicated level Read off to the nearest 0 001 kg l and log the products specific weight Shake the hydrometer and take two or three more readings as confi
111. p or a micro filter A visual check will normally disclose dispersed water However experience has shown that with the turbine fuels used by aircraft there may be borderline cases where the human eye cannot be trusted It is against this background that the Shell Water Detector has been developed This will give a positive indication of dispersed water with a concentration of 30 parts per million 30 ppm The capsules may also show a slight change in their appearance in a concentration as low as 5 parts per million 5 ppm 5 4 3 Visual controls In order for the fuel samples to be accepted the fuel must be of the correct colour visibly clear and transparent and free from particles and dispersed water at normal temperatures The colour of Jet A 1 varies from a watery white to a straw yellow Refer also to the chapter on Visual Check Water that has not dispersed will appear as drops on the inner walls of the sampling glass or as water at the bottom of the glass This may also fog the sample make it opaque Particles and other visual pollution will generally consist of rust sand or dust either mixed with the fuel or as sediment at the bottom of the glass When using the permanently installed sampling glasses by discharging the sampled fuel onto the outer rim of the glass an automatic cyclone movement is achieved In this manner particles and larger water droplets are gathered at the bottom of the glass It is therefore important
112. p the external cargo area 14 Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Il LOADING AND CARGO AREA LIMITATIONS Open the cargo net snap latches and load cargo onto the shelves CARGO COMPARTMENTS Picture 4 Cargo compartment decal The following weight limitations applies and must not in any circumstance be exceeded Upper shelf totally Area 1 2 300 Ibs 136 kg Lower shelf totally Area 3 4 700 Ibs 317 kg 1000 Tbs 453 kg Total weight loaded on the ramp upper and lower shelves combined must not to exceed 1000 Ibs 453 kg The storage box must be installed when the lower shelf is installed When cargo is loaded directly onto the ramp the lower shelf and storage box must be removed and the cargo secured to the ramp 15 Encl F3 to OLF Helideckmanual rev 01 09 201 1 se Bristow Norway CARGO LOADS UPPER SHELF COMBINED RAMP FLOOR AND BOTH UPPER MAXIMUM SHELF LOAD AND LOWER SHELF LOAD NOT TO EXCEED NORO142 005 A ES EEN Mun LOWER SHELF CARGO RAMP MAXIMUM SHELF LOAD MAXIMUM RAMP FLOOR LOAD 700 LBS 317 KG NORD152 006 STORAGE BOX WHEN LOWER SHELF IS INSTALLED 1000 LBS 453 KG NORG1 2 007 STORAGE BOX MUST BE INSTALLED ON THE CARGO RAMP NORGE 2 004 Picture 5 Cargo limitation decals Ill CLOSE THE CARGO AREA After loading the cargo perform the following steps Close cargo net snap latches and tighten cargo net Verify th
113. passengers will leave their PLB in the aircraft take their luggage follow the directions from the helideck crew and leave the helideck as directed When embarking passengers the procedure is vice versa When refuelling all passengers will normally have to leave the helicopter and all doors must be closed This gravity refuelling servicing is performed entirely on the left hand side Initially the helicopter must be grounded with a grounding wire at the main wheel as illustrated below Secondly the grounding wire from the pistol handle must be grounded to the grounding point just left of the fuel caps also illustrated Remove fuel cap s and distribute the fuel in the rear or forward tank as agreed with the pilots When refuelling is done close and secure the fuel caps remove the pistol handle grounding and wind up the fuel hose Finally remove the grounding wire from the main wheel and the passengers can board the helicopter again The battery is positioned on the left hand side of the helicopter just forward of the pilot pedals as illustrated yt a Grounding point for the pistol Opening of the fuel caps The battery is positioned on the left hand side of the helicopter just forward of the pilot pedals behind this shield DanCopter A S DanCopter All 2 DK 6705 Esbjerg enclosure F4 to OLF helideckmanual rev 01 09 2011 Crash chart EC 155 B1 DanCopter 1 Access to cockpit 2 Emergency 4 Fo
114. r has been removed from the container This is because of the possible risk of discolouring the paper due to air humidity As a consequence detectors should not be left lying around or left loose in the pockets of overalls clothes etc The maximum storage time for a detection capsule is nine 9 months from the date of production e The expiry date will be stamped on one side of the storage box e The expiry date will also be stamped on each capsule this must be respected Unused capsules should be stored indoors under dry conditions until they are to be used Procedure for using the Water Detector Test Check that the expiry date has not been exceeded to be found on the box container Prepare a sample of at least 3 5 litres in a clean clear glass The sample must be powerfully rotated until a cyclone effect is generated in the glass By using this method particles will accumulate at the bottom of the glass and any water particles will be crushed into the fuel This takes place automatically in the enclosed sampling glasses Mount the detector on the syringe and immediately submerge both into the sample Withdrawn the plunger until the fuel reaches the 5 ml mark Make sure that the plunger is not withdrawn before the syringe is submerged in the liquid If the plunger is withdrawn when in the open air humidity will create an indication in the detector This will result in a faulty reading Any possible water droplets in the fuel wi
115. r turning the anti collision lights off and the helicopter is ready to take onboard both passengers and cargo Operation Preparation HELIGUARD 1 Keep eye contact with the pilot and Takes up position by the The fireguard stands beside maintain full view of the helideck access stairs so as to have the relevant fire post remote 2 During start up there should be no a clear view of the helideck control unit wearing all fire passengers onboard the helicopter apart protection gear from when the pilot so wishes enclosure H to OLF Helideckmanual rev 01 09 2011 Operation Start engines Stand in front of the helicopter in the safe Take up position on the zone Assist fireguard whenever indicated side of the necessary helicopter to observe the engine startup When moving after no 1 engine has started and the rotors are turning the fireguard must stay outside the rotor disk when proceeding to the next engine In the event of a fire in or under the helicopter alert the pilot HLO by the portable VHF radio or by giving the signal Shut down Start to extinguish the fire Operation Final stage of start up embarking passengers and loading take off without passengers 1 On the signal from the pilot anti collision 1 Take up position and give 1 Proceeds to the access lights off commence boarding passengers sign to the HLO that stairs to await signal from and loading cargo remove chocks boarding may start H
116. re floating moving and other helidecks that are moving These are all defined as unstable if pitch and roll movements exceeds 1 degree to either side from the horizontal plane and if the vertical movement of the helideck exceeds 2 meters Measuring equipment for unstable helidecks Helideck Monitoring System The Helicopter Companies have developed a Standard that covers this requirement This standard represents the minimum requirements to measuring equipment for operations to an unstable helideck See enclosure L Standard Helideck Monitoring Systems Reporting of incidents Reporting of ground incidents on the helideck In accordance with CAA N s new reporting requirements all relevant incidents on the helideck shall be reported to the CAA N within 72 hours The form attached to OLF Helideck Manual enclosure M describes types of reportable incidents and shall be used in addition to any internal reporting procedures The report shall be filled out as soon as possible and sent to the Operations Centre of the Helicopter Company involved in the incident They will enter the report into their reporting system and forward the the report to CAA N DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 15 3 1 OLJEINDUSTRIENS LANDSFORENING Helicopter deck and equipment parts The contents of this section are of an informative nature and describe e The helicopter deck in general e Equipment parts
117. re done on an as necessary basis Proposals for revisions must be forwarded to OLF and the Norwegian Offshore Helicopter Operators for comments and advice enclosure K to OLF Helideckmanual rev 01 09 2011 Procedure for refuelling helicopter with rotor running Refuelling with passengers onboard is acceptable provided a mutual agreement between the pilot and the HLO and shall take into account the demands described in para 5 12 6 in addition to standard procedures as described in this enclosure 1 Remains in position with a full view of the helideck When the Fireguard has connected the earthing cable and has taken up his position beside the HLO the Fireguard will assume responsibility for safety on the helideck 2 The HLO and the pilot will then go to the refuelling cabinet and check the fuel sample 3 Verify that the earthing light is lit the counter is set to zero and that the fuel hose is connected to the helicopter 4 On the signal from the Fireguard the HLO will push the button to start refuelling HELIGUARD 1 Waits until all passengers have left the helideck and then pulls out the fuel hose When the Fireguard has connected the earthing cable the heliguard will earth and connect the fuel hose to the helicopter and open the connector valve 2 Stays in position at helicopter refuelling point 1 Pulls out earthing cable and earths helicopter 2 Take up position next to HLO in fron
118. rev 01 09 2011 Helicopter danger zones AgustaWestland AW139 DANGER D Normal route gt Heliguard limited DANGER enclosure B to OLF Helideckmanual rev 01 09 2011 Helicopter danger zones EC155 Approach sector Heliguard limited Keep passenger clear Normal route je iR a a 2 Alternate route Crossing helideck in front of helicopter in safe distance from main rotor only with permission from helicopter crew enclosure C to OLF Helideckmanual rev 01 09 2011 Installation Name and type of filter water separator Elements type 1 Elements type 2 Name and type of filter monitor Elements Max monitor 22 Max separator 15 Filter water separator filter monitor follow up log Year Functional test differential pressure Monitor Separator Number Date installed 1 2 Number Date installed 3 4 5 6 7 8 9 10 Number Date installed 11 12 Psi 24 22 20 18 16 14 12 10 8 6 4 2 112131415161 7 1011 12 11314 15 116117 118192021 22232425 2627 28293031 323334 353637 38 394041424344145464748 4950 5152 enclosure C to OLF Helideckmanual rev 01 09 2011 Rig Installation Helicopter fuelling log Adressee of this
119. rmation that they are correct Thereafter read the temperature Note both temperature and specific weight density as direct readings from the hydrometer DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 35 OLJEINDUSTRIENS LANDSFORENING Use the noted temperature and specific weight density and correct them to 15 C by using the conversion table for density ASTM IP table 53 or by using the conversion unit for fuel density the plastic circular sliding converter Aristo 60 208 Germany Note the specific weight corrected to 15 C NB As sliding converters becomes worn they will show faulty readings If such instruments are used they must be regularly checked for wear The specific weight density corrected to 15 C must be within 0 003 kg litre of the specific weight corrected to 15 C which is to be found on the upper part of the transport certificate for the aviation fuel If an electronic Density Meter are being used the manufacturers user manual must be adhered to If the specific weight is not within the limits then the guidelines for faulty fuel must be followed and the fuel may be sent in return 57 Basic requirements for laboratory samples Samples that are to be certified by a laboratory must be taken from an outlet having direct access to the space where the liquid is stored Before sampling the equipment must be rinsed thoroughly and washed at least three times i
120. ronic data to the helicopter land base operation witch in turn can eliminate the need for a separate Rig Report to be submitted With the Monitoring System functional the category will be upgraded from A to A or from B to B whichever is relevant to the actual vessel rig 6 Accuracy of measurments The monitoring system sensors and data programs shall be checked and verified for correctness on the system field location strictly in accordance with the manufacturer s procedures A verification report showing the correctness of the system shall be provided to both the owner of the installation and to the helicopter operators after first installation The accuracy of the system shall be checked and verified whenever deemed necessary but at least once every 3 years A verification report shall be issued and distributed as described above after each periodic control The accuracy of the data produced by Helideck Monitoring System concerning motion shall be Pitch Roll Inclination x 0 1 RMS Root Mean Square in the range 0 to 3 5 and Heave Rate lt 0 1 m s RMS Root Mean Square in the range 0 to 1 3 m s The accuracy concerning the meteorological data shall be in compliance with NORSOK N 002 Collection of Metocean Data and NORSOK C 004 Helicopter deck on offshore installations enclosure L to OLF Helideckmanual rev 01 09 2011 Measuring helideck motion 6 1 Maximum Pitch The equipment shall be capable of measuring helideck
121. rs in the pressure hose connectors and the filling nozzles DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 34 5 5 5 5 5 6 5 6 OLJEINDUSTRIENS LANDSFORENING During each inspection of the filter strainer monthly the hose in question must be pressurized for at least one minute Checks and inspections with longer intervals than those listed above are part of the installations individual maintenance systems Returning products to the unit Clean products containing no water that are accumulated during draining and sampling may be returned to a slop tank The product in the slop tank shall be allowed to settle and be drained free of water and particles before being transferred to a product tank Sampling when delivering to the helicopter e A3 5litre sample shall be taken from the filter monitor or the filling nozzle before delivery The sample must be checked visually including testing with the water detector Any water must be drained off and new samples taken until a satisfactory water detector test has been achieved e A3 5litre sample shall be taken from the filling nozzle or from the inside of the filter monitor immediately after delivery has been completed This is in order to confirm the quality and to carry out a visual check with a water detector If there are any indications of water or any marked change in colour in the water detector a new sample must be taken The pil
122. rtificate for aviation fuel contains the following elements e Type Amount Batch no Date Tank serial number Specific weight density Verification of being free from solid particles and water the inspector s signature The following must be checked when receiving fuel e Check that the seals on the manhole inspection hatches and outlet are unbroken Also check that all dust covers are in place and intact e Check that the tank cradle tank have their respective approvals This may be read off the tank data plate e Check for damage to hatches and valves Make a special check of protective hatches and their packing rings e Check that the seals are intact and that the type of tank is labelled 5 11 1 Settling time e 600 USG 2300 litre tank 1 5 hour settling time e 1000 USG 3800 litre tank 2 hours settling time e Settling time stationary storage tank 1 hour per meter fuel depth If the sample contains sediments or free water further 4 litre samples must be taken until the samples no longer contain sediments or free water The following tests shall be conducted e Arotation test powerfully rotate the sample before the visual check e Clear and bright test visual check e Shell Water Detection test The criteria for accepting the sample are that it e Passes the clear and bright test e Is free of water e Is free of pollutants If one or more of the criteria are not met a further settling time of one hour per meter
123. rward Pull locking handle cut off P handles will cut off engines and close fuel valves Both handles must be pulled rearwards Overhead panel 3 Access to cabin Pull locking handle DanCopter A S DanCopter All 2 DK 6705 Esbjerg enclosure F4 to OLF helideckmanual rev 01 09 2011 EC 155B1 FIRE ACCESS PANEL SAME ON THE OTHER SIDE I IN CASE OF FIRE i E u FIGHT FIRE HERE Luggage compartment Size of the door in mm Size of the floor 690 1878 1520 4 730 gt 4 2350 gt Enclosure F5 to OLF Helideckmanual rev 01 09 2011 AgustaWestland AW139 AW139 in the offshore configuration Access Operator Blueway Offshore Norge AS Bygd y all 2 Postboks 573 Sentrum 0101 Oslo Norge Tel 47 6712 5400 Fax 47 6712 5401 E mail BLUE WAY info bluewayoffshore no Organisationsnr 994 104 586 Offshore Norge AS Enclosure F5 to OLF Helideckmanual rev 01 09 2011 Cargo 3 15ft 1 32m 0 61m 0 54m 4 33ft 2 00ft 1 771 ICN 39 A 000000 A 00003 00266 A 01 1 Figure 1 3 Cabin and Baggage Door Dimensions The cargo compartment has access via one door on each side of the fuselage Dimensions 4 22m 13 85ft pre me 7 13 77m 45 18ft 16 62m 54 55ft Enclosure F5 to OLF Helideckmanual rev 01 09 2011 Refuelling Refuelling on right hand side of helicopter Gravity refuelling only After grounding the helicopter and th
124. ry fine form The chain reaction of the fire is stopped by introducing into the atmosphere a large number of finely powdered particles Remember When extinguishing a fire by using dry powder any evaporation through the powder will present the possibility of re ignition from hot metal smouldering insulation etc 3 3 3 2 Application Dry powder is effective against most fires especially electrical fires as it is non conductive When used to extinguish a petrochemical fire in most cases re ignition will occur unless the source of ignition is removed Foam must be used to prevent re ignition 3 3 3 3 Equipment The equipment is of the gas cartridge propellant type The powder is propelled by internal overpressure Discharging a CO2 propellant cartridge located inside the extinguisher creates this overpressure 3 3 3 4 Use 3 3 4 The powder will normally start to flow within 15 seconds of activating the fixed equipment The units should be directed towards the base of the flames If possible from up wind Immediately after use all piping must be cleaned of any remaining powder This is to prevent powder lumps that may later block the hose piping Maintenance All rescue and safety equipment shall be maintained in good working order and be ready for use at all times Maintenance periodical testing and inspection must be carried out in accordance with established procedures DOCUMENT NO REVISION NO REVISION DATE
125. s Standard hand signals must be used See Enclosure A Exempted from this procedure are helicopters in shuttle traffic where both pilots remain in the cockpit Wheel chocks may then be used at the pilot s discretion Standard procedure e The wheel chocks must immediately be put in place as soon as the anti collision lights have been switched off The wheel chocks must be placed in front of and behind both main wheels Both pilots must remain in the cockpit until the wheel chocks are in place e The wheel chocks are removed when both pilots have taken their respective seats and the pilot has signalled Remove wheel chocks DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 24 4 2 4 2 1 4 2 2 4 2 3 OLJEINDUSTRIENS LANDSFORENING Cargo in the helicopter General The restrictions described in this chapter apply to all types of helicopter The restrictions are supplementary to the authorities requirements JAR OPS 3 Personal luggage must not exceed 10 kg per piece Cargo that is sent by helicopter should not weigh more than 15 kg per parcel Heavier packages must be divided if possible Exemptions may be made for priority cargo The cargo must then be specially labelled heavy cargo with the weight listed on each package and the installation destination must be notified Passenger cargo manifest Whenever passengers luggage and or cargo are transported by helic
126. s H re as Figure 1 4 Exterior Aircraft Dimensions Description Dimensions Main roter diameter blade tip circle 564 17 17 m Tail rotor diameter blade tip circle mo 3 35 m Fuselage length 562 17 10 m Fuselage width 129 3 88 m Fuselage height te top of tail pylon 1427 4 32 m Length over all including rotere 586 20 88 m enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Nor Way PROCEDURE TO OPEN AND CLOSE AIR STAIR DOOR TO OPEN AIR STAIR DOOR Upper door Upper door must be open first by turning door handle to open position Lock upper door struts with locking levers Lower air stair door Turn door handle in open position Lower the door TO CLOSE AIR STAIR DOOR The lower air stair door must be closed first Lower air stair door Pull up on the door cable to raise the door Turn and hold the door handle in open position while firmly closing the lower door Turn the handle to lock position and ensure thelock pins are engaged Upper door Unlock bouth upper door struts by depressing the locking levers Turn and hold the door handle in the open position while firmly closing the upper door turn the handle to the lock position and ensure the lock pins are engaged A indication light in the cocpit will indicate if the door is open or closed enclosure F2 to OLF Helideckmanual rev 01 09 2011 S 92 CHC Norway Cargo compartment CHC S 92 The Baggage Compartment on the Sikorsky S 9
127. s of 30 parts per million or lower 30 ppm The detector consists of an unbreakable 5 ml syringe and a plastic detection capsule containing water sensitive paper safety zone for helideck crews during landing take off shutting down and starting up the helicopter by the stairways to from the helideck not on installations not having stairways safety zone for embarking and disembarking passengers all movement of personnel shall primarily take place at a 90 degree angle from the main axis of the helicopter and thereafter outside the rotor disc Passengers waiting to embark shall follow the instructions given by the crew of the helideck in an area where there is a low risk of injury should there be a helicopter accident on the helideck safe rotor zone an area where there is no risk of contact with either the main rotor low or the tail rotor safe zone with eye contact with the pilot an area in the vicinity of the nose of the helicopter limited to the rear by eye contact with the pilot and taking into consideration a full view of the helideck and where there is no risk of contact with the main rotor end of hose sample sample taken from the end of the delivery hose through the filling nozzle satisfactory result fuel sample the fuel has the correct colour is visually clear and transparent free from particles and dissolved water at normal temperatures pressure fuel connector arrangement at the end of the filling hose nearest to
128. se by or longside ie a flotel and only one of the helidecks is to be used NB The marking shall not be used just because the helideck is not manned or due to general equipment failures A temporary or permanently closed helideck shall be marked in accordance with an internationally accepted standard with a yellow cross on red background The marking should be painted on the deck or by using a painted canvas laid out and secured The marking shall be placed over the H in the center of the helideck When the helicopter deck is marked closed the green perimeter lights shall be turned off AMB SAR helicopters will not land when the helideck is marked closed 3 2 Safety equipment This section describes in general terms the safety equipment available on the installations The type of equipment may vary from installation to installation Special information pertaining to a specific installation is included in the local operations manuals DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 19 O OLJEINDUSTRIENS LANDSFORENING 3 2 1 Alarm systems It must be possible to activate the alarm system from the helicopter deck or its immediate vicinity The start button for the alarm system must be clearly marked 3 2 2 Fire alarms and General alarms Alarm buttons are located at the helicopter decks fire posts These are only to be used in emergency situations including a fire in a helicopter
129. sorbing heat Fires involving inflammable liquids will be extinguished when covered by a thick carpet of foam The carpet must have the proper consistency and thickness and must be maintained for a sufficient length of time 3 3 2 2 Application Foam must be applied in the largest possible amounts so as to cover the whole surface of the fire Foam is suitable for all kinds of fire apart from electrical fires 3 3 2 3 Equipment There are three types of cannon and three types of hose reels Exceptions may be found on some of the older helicopter decks where there are only two cannon and two hose reels only two fire posts Producing foam requires the mixing of the following three components in a turbulent condition e Water e Air e Foam concentrate This is usually achieved by injecting the concentrate under pressure into the water flow The system will usually start to produce foam about 20 seconds after the start up of the equipment 3 3 2 4 Use The fixed foam system is controlled from permanently installed fire fighting cabinets After using the foam system all piping must be thoroughly flushed with water to remove any remaining foam solution Note that too much water will break down the foam 3 3 3 Dry powder system DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 22 OLJEINDUSTRIENS LANDSFORENING 3 3 3 1 Purpose and effect The effect of the dry powder in ve
130. ss then the values given above the helicopter crew shall be updated in the following format Wind direction given in degrees Wind speed including gust given in knots Visibility given in meters or km Clouds or Ceiling FEW BKN OVC given in feet above sea level Actual temperature given in degrees Celsius Dew point temperature if available given in degrees Celsius QNH given in HektoPascal Other information of interest to the helicopter crew like shower activity snow on the helideck etc Movement of the Helideck If the Helideck is moving less than 1 degree less than 1 to any direction from the horizontal plane and the vertical movements heave is less than 2 meters the Helideck is defined as not moving In this case there is no need to forward these details to the Helicopter crew Enclosure I to OLF Helideckmanual rev 01 09 2011 For installations witn HMS Helideck Monitoring System it should be adequate to announce We have a GREEN deck on the HMS unless that the Helicopter Crew is requesting the details Return load This is given in the following format Number of passengers PAX Total weight including pax luggage and cargo weight of luggage cargo Obstructions in the vicinity within 500 meters in the approach and departure missed approach sectors The reason for the need of this information 1 To verify that obstruction free sectors according to CAAN regulations in BS
131. stems hot refuelling standard helideck monitoring systems reporting form ground occurrences elideck report form See separate PDF attachment DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 50 enclosure to OLF Helideckmanual rev 01 09 201 leng Hand signals Handsignal 1 Chocks away Chocks in position enclosure to OLF Helideckmanual rev 01 09 201 leng Handsignal 2 p External power on p External power off enclosure to OLF Helideckmanual rev 01 09 201 leng Handsignal 3 Start engine no 1 i i Start engine no 2 enclosure to OLF Helideckmanual rev 01 09 201 leng Handsignal 4 Start rotor enclosure to OLF Helideckmanual rev 01 09 201 leng Handsignal 5 Shut down alternatively stop refuelling enclosure B to OLF Helideckmanual rev 01 09 2011 Helicopter danger zones Sikorsky S 92 DANGER D Normal route HE Alternate route 00 Heliguard limited DANGER Alternate route to be used only under HLO supervision See Enclosure G alternative access for procedures enclosure B to OLF Helideckmanual rev 01 09 2011 Helicopter danger zones EC225 SuperPuma DANGER ZZ Normal route GE Alternate route gt Heliguard limited DANGER Alternate route to be used only under HLO supervision See Enclosure G alternative access for procedures enclosure B to OLF Helideckmanual
132. t least one light at each level must be visible from all directions Operational equipment The helicopter deck shall at all times maintain all the equipment that is required for operations such as Wheel chocks Ropes for tying down a parked helicopter Scales for weighing luggage cargo should be available on the installation Equipment for removing snow and ice Rescue equipment The following rescue equipment should be found in the immediate vicinity of the helicopter deck 2 Fire axes 3 Non corrosive knives for cutting seat belts 2 Flashlights Explosion proof 1 Crowbar 1Wire cutter 1 Hacksaw w spare blades 1 Hammer 1 Cutting chisel 1 Sheet metal shears 1 Bolt cutter 1 Jack for minimum lift of 1 2 tonne The equipment must be stored so that it is readily available visible and in a safe place preferably in a sealed locker or container If the locker or container can be locked with a key the key must be placed behind a window of breakable material The locker or container shall be painted red and marked Nedutstyr and Emergency Equipment One metal hook on a 3 m long metal handle together with a light ladder of about 3 m in length shall be stored in a suitable place near the locker or container holding the emergency equipment 3 1 10 Communications equipment Personnel who comprise the minimum manning requirement for the helicopter deck shall be equipped with portable two way VHF radios capable of c
133. t least one person dressed in fire protection clothing as stated in Chapter 2 11 shall be stationed at the remote control unit for the helideck s foam cannon or at the most practical foam cannon to be used in the prevailing weather conditions During refuelling with the engine running the helideck crew shall consist of Refer also to Chapter 5 12 6 and enclosure K e The operator of the refuelling plant e The operator of the pistol grip nozzle e The fireguard The HLO may be one of the three persons The fireguard shall be dressed as described for take off and landing When required additional personnel without training and or experience could be utilised on the helideck Such personnel must be briefed by the HLO and be under constant supervision during helicopteroperations Helideck report Not later than one hour before planned helicopter departure from base the offshore installation shall give the helicopter operator updated information regarding the status of the helideck and flying conditions The information shall be given on a separate form see separate PDF enclosure Helideck Report Form OLF v1 See separate enclosure to the manual by choosing attachements in upper left corner The report is valid maximum 6 hours on condition there are no changes in the information The helideck report shall be forwarded in pdf format as attachment to an E mail The subject field in the E mail shall be filled in as follows lt Name of
134. t of the helicopter with a clear view of the pilot inside the helicopter of the heliguard and the refuelling cabinet Portable powder extinguisher must be available on the helideck 3 The Fireguard will now assume responsibility for safety on the helideck 4 On the signal from the pilot the fireguard will signal to the HLO that fuelling can commence Finishing refuelling HELIGUARD 1 On the signal from the fireguard the HLO will stop refuelling from the refuelling cabinet 2 The HLO will take a new fuel sample This will be checked by the pilot who will then sign the fuel log 3 The HLO will proceed to the helideck take up his position next to the Fireguard and re assume responsibility for safety on the helideck 4 When the heliguard is ready the HLO will signal to the fireguard to start boarding 1 When signalled by the Fireguard to stop refuelling closes the connector valve on the fuel hose 2 The fuel hose and earthing are disconnected and the hose rolled up on the drum 1 On the signal from the pilot to stop refuelling the Fireguard will immediately signal to the HLO and the Heliguard stop refuelling 2 Remain in position until the HLO is in position and may re assume responsibility for safety on the helideck 3 Disconnect earthing cable and roll it up on its drum NB Some helicopters have integrated automatic fuel shut off systems enclosure L to OLF
135. tandard heave period of 10 seconds for manual calculations of average heave rate Max Heave rate expression for Max Average Heave rate Shall be entered if measurement equipment for this purpose is available Heave rate shall be reported as the highest value average heave rate meaning average speed from top to bottom or bottom to top of a wave measured over the last 20 minutes If measurement equipment in not available the column should not be filled in The pilots will calculate average heave rate manually by dividing maximum total heave measured over the last 10 min by half the motion period heave period DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 13 OLJEINDUSTRIENS LANDSFORENING HELIDECK REPORT WEATHER OBSERVATION elidec MIQNH hPa heading uec ben jeu fw stn ove net OLF ver 1 DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 14 2 14 2 15 OLJEINDUSTRIENS LANDSFORENING Helideck Monitoring Systems Unstable Helidecks The helicopter Companies and CAA N have set requirements to all installations and vessels with unstable helidecks that a system which can measure Pitch Roll Helideck Inclination and Heave Rate must be installed Definition The definition of an unstable helideck is in this context a helideck mounted on ships floating production units semi submersible rigs jack up rigs when they a
136. test edition enclosure J to OLF Helideckmanual rev 01 09 2011 shall be installed This unit is designed to absorb any water still present in the fuel and to cut off the flow of fuel once a certain amount of water has been exceeded The fuel filter monitor shall also be equipped with e Adifferential pressure gauge for monitoring the conditions of the elements e Anair eliminator which automatically vents any air entering the vessel e A pressure relief valve e A closed circuit sampler connected to the sample point e Aself closing valve on the 77 minimum drain connection Bonding equipment A ground indicator approved for the purpose shall be installed to restrict the pumps being operated until the ground indicator has approved the continuity A spring loaded bonding cable reel sized for 30m cable and bonding clip shall be installed A yellow Ex zone 2 lamp installed outside on top of the dispensing cabinet will indicate when the helicopter is properly bonded Recycle module not a requirement The recycle tank shall have a slope of minimum 1 on 30 The tank shall be equipped with an inspection hatch in order to clean the tank properly The tank shall be designed according to TBK ASME BS or other appropriate code The same rules apply for this unit as for the pump and dispensing unit If a pump is included it shall be of a flanged positive displacement vane type pump or centrifugal pump Revisions Revisions of this document a
137. the exit e Rotate handle towards open position and remove the emergency exit Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Cockpit emergency exits P d EXIT 1 PUSH RED BUTTON TO RELEASE HANDLE 2 ROTATE HANDLE FULLY i 1 Figure 5 Cockpit emergency exit The two cockpit emergency exits are not hinged to the aircraft When operating the handle the emergency exit will be forced out on the bottom and then slide out of the frame on the top WARNING SUPPORT HATCH DURING PROCEDURE IF YOU DO NOT DO THIS HATCH CAN FALL AND CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT To open the exit e Push red button to release handle e Rotate handle towards open position and remove the emergency exit Encl F3 to OLF Helideckmanual rev 01 09 201 1 s Bristow Norway Engine fire fighting from the outside To fight engine fire Aim extinguishant at openings Figure 6 Engine inlets The two engine inlets have openings for venting the engine compartment In case of fire aim the fire extinguishant at these openings The engine compartments are protected through the onboard fire extinguishing system APU fire fighting from the outside The APU is in a sealed compartment and does not have any openings The APU compartment is protected through the onboard fire extinguishing system Encl F3 to OLF Helideckmanual rev 01 09 2011 se Bristow Norway Open radar dome and disconnect battery Op
138. this standard Category B Small ships diving vessels and similar with measuring and monitoring equipment deviating from this standard enclosure L to OLF Helideckmanual rev 01 09 2011 Category B Cat B with measuring and monitoring equipment installed and functional in accordance with this standard 4 Operational Limitations 4 1 1 1 1 Landing and planning Category Pitch Roll Helideck Inclination Heave rate Day Night Day Night A 3 2 1 0 m s 0 5 m s A 132 9 5 22912659 1 3 m s 1 0 m s B 2 Not approved 0 5 m s Not approved B 2 2 5 1 5 2 1 0 m s 0 5 m s For Semi Submercibiles Category A the night limit is 3 3 5 5 Principles Basic reference is made to e Requirements in BSL D 5 1 8 2 Reference is also made to e Sintef Report 22D114 199 11 09 FPSO Helideck Motion Criteria The measuring equipment shall provide sufficient information to the operator to complete all sections of the standard Rig Report provided for by the helicopter operators Measuring equipment sensors for helideck movement wind and weather data shall be located in optimum positions in order to provide relevant information relating to the helideck All information shall be numerically displayed in relevant locations on the vessel or rig for easy communication with helicopters in flight and the helicopter land base operations The system shall facilitate transmittal of elect
139. tions ssssseeee 8 2 3 Iris eR nes 8 2 4 SUPPE TS I M 8 2 5 Maintenance eere F UMLAND o onana 8 2 6 pj M 8 2 7 Training of helideck BELOW REE RE RE EE ET 8 2 8 mee P EE ER EE RE TN RR ES 9 2 9 Ser EE EE EE NR idu 9 2 10 Special responsibilities and duties for the leader of the helicopter deck HLO 9 2 11 Clothing and protective equipment for the helideck crew eseeeeeesees 10 2 12 Manning the helicopter deck rrnnnrnnnnnnnnnnnnnnvnvnnnnnnnnrnnnnnnnnnnnnenrrnnnnnnnnnnnnenenenennnnnnnennnnnnn 11 Ede sio ricos qe m m aE EEA Aa iA 11 2 14 Helideck Monitoring Systems u sace tei rni oa Roe tiu Elba uae tbe pet a nus ost lg tue Rara pep UP Eu RR RUD 15 215 Reporting FET 15 3 Helicopter deck and equipment parts rnnnnnnnnvnnnnnnnnnnnnnnnnnnnnennnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnne 16 3 1 The helicopter deck in general i cicctecaciassasseancictantcncei dose indiendinaatsannseeesiaeedaetaageuteddeluenletes 16 3 2 S fety PPT Se 19 3 3 Firefighting sl PTE mete bc C 21 4 Operation D mM een ees 24 4 1 Operating on the helicopter deck eene 24 4 2 Cargo in the helicopter t UE 25 4 3 618400 10 116 1 erei EE EE EE RE 27 5 Aviation fuel Introduction sissies eee deste ied ada aside zc Rcx M Rida s t E LONE 30 5 1 ON e
140. tor lights switches are installed If there is a fire the red FIRE 1 ENG FIRE 2 ENG or the FIRE APU will illuminate This indicates that there is a fire in that compartment To shut off fuel and stop engine APU e Lift all three red covers and push each button 10 se Bristow Norway Encl F3 to OLF Helideckmanual rev 01 09 201 1 Aircraft battery When both engines and APU is stopped the aircraft can be deenergized by switching off the battery The switch is located in the centre part of overhead console POWER aC p AIR SRCE EXT APU GEN APU HEAT PUR BATT OFF CTRL START RESET OFF RESET ON JJ A E r W COW m AC CH 4 NO BACKUP To switch battery OFF OFF Move switch to OFF 9 Figure 10 Aircraft battery switch To switch off battery e Move BATT switch to OFF 11 Encl F3 to OLF Helideckmanual rev 01 09 2011 se Bristow Norway Rotorbrake General WARNING ENGINES MUST BE STOPPED PRIOR TO APPLYING ROTORBRAKE AFTER the engines have been stopped the main and tail rotor might be stopped and immobilized to prevent wind milling by applying rotor brake The rotor brake handle is located to the right of the overhead console Move handle forward to locked position Figure 11 Rotor brake handle To stop and immobilize the main tail rotor e Move rotor brake handle forward to locked position 12 Encl F3 to OLF Helideckmanual rev 01 09 2011 se
141. uld also be maintained to the extent necessary 6 1 3 Crash on the helicopter deck The characteristics of a helicopter crash Due to the fact that a helicopter has no wings the engine s and the fuel tanks are positioned in the immediate vicinity of the cabin In the event of a crash this means that DOCUMENT NO REVISION NO REVISION DATE 01 09 2011 Page 45 OLJEINDUSTRIENS LANDSFORENING There is a possibility that parts from the rotor blades may be slung around It is less likely that the helicopter will remain standing in a vertical position It is easier to drag hoses around a helicopter and there are far less sheltered areas beneath the fuselage The shorter distance to the secondary fire fighting equipment increases the advantage effects As the cabin engines and fuel tanks are so close to each other rapid intervention may be decisive If a helicopter crashes on the helideck the fireguard shall e Start the fire pumps sound the alarm e Cover the helideck with foam e Extinguish any fire e Maintain a sharp lookout for fire This is especially with regard to spilt fuel that may run down to the lower decks of the installation Rescuing passengers and pilots The helicopters doors and hatches are of a relatively simple construction and there is little probability of them jamming Should this be the case then they must be forced open Should it be necessary to use m
142. uselage fire guard operates the fire fighting equipment on the helideck and assists the heliguard with the loading and unloading of passengers and cargo from the helicopter drainage samples fuel samples taken from the lowest point of the tank or from the filter housing specific weight measuring of Jet A 1 measuring the specific weight density of the fuel To be conducted when receiving fuel offshore The specific weight is checked by using a hydrometer and a thermometer free approach and departure sector within the 210 degree approach and departure sector there must be no obstacles neither on nor in the immediate vicinity that reach above the level of the helideck filling nozzle arrangement on the refuelling hose at the end nearest to the helicopter used for gravity refuelling of the helicopter helideck crew consists of a minimum of three persons HLO heliguard and fireguard HFIS Helicopter Flight Information Service heliguard responsible for the embarkation and disembarkation of passengers and cargo and assisting the fireguard and the HLO in emergency situations HLO helicopter landing officer supervises the heliguard and the fireguard winching area a pre defined area which in situations where the helideck is closed is suitable for winching patients and personnel up to a rescue helicopter chocks wheel chocks blocks which are placed in front of and behind the wheels on both sides of the helicopter

Aviation OLF helideckmanual_010911_en

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