LEAD-IN LIGHTING Appendix A
Contents
1. NOTIAI N NVN NW AINA NITY NIVI a IN ATNI MWYN QAX Israel Airports Authority gt a Planning and Engineering Division LEAD IN LIGHTING Procurement of Equipment For OVDA Airport Appendix A Technical Specifications Requirements 17 10 2013 1 NOTIAI NIN NVVN 2xqw a noWwNA NITY NIVI a VHN ATNI Ynwn qax Israel Airports Authority a Planning and Engineering Division General 1 1 This specification covers the requirements for Lead In Lights and MALSR Sequenced Flashers for approach to land on Runway 21R in OVDA Airport ISRAEL 1 2 OVDA Airport has two parallel runways 03 21 East and 03 21 West situated 350 meters between centerlines as shown on the Aerodrome Chart below AIP AD 2 4 11 ISRAEL 26 JULY 12 AERODROME CHART esse ELEV 1483 FT TWR 129 9 OVDA a BEARING ELEVATIONS ARE IN FEET mwr onecnow mn acne ee 018 K 9 3 42 K N 03L ot BEARINGS ARE MAGNETIC F B Y U 44 a 21R 198 K 7 0 Asphalt a m2 i 0 Concete AR yE ledges pep ANNUAL RATE OF CHANGE 3 E SIMPLE APPROACH TERMINAL IC LIGHTING SYSTEM SAL CIVIL APRON STRIP 2720 x 150 PAPI 3 2600 x 45 ASPHALT T STRIP 3120 x 150 SWY 170 x 45 3000 x 45 ASPHALT ELEV mi SS R gt mf 91509 i s FIRE ae gt Z IN 4 a J r mo N r NOTES ARRESTING CABLES ARE PERMANENTLY RIGGED 1 3 Existing Airport Ground Lighting AGL includes 1 3 1 High Intensity Ru2. 1 Commissioning Installation Commissioning and start up KK K K K K K
3. Control from ATC Fe Gp 3 Control from ATC Extended Runway Center Line ILS APPROACH ROUTE TO RW 21R Approximately 4 600m NOTES 1 EACH OF LIGHTING SYSTEM IS INDIVIDUALLY WIRELESS CONTROLLED FROM ATC RAIL REIL LEAD IN 2 LEAD IN LIGHTS SHALL BE SWITCHED ON FOR SHIFTED ILS APPROACH TO LAND ON RUNWAY 21R 3 ILS MINIMA VISIBILITY 1 800M 4 ALL LIGHTS WITH LED OPTICS HEAD OUTPUT OVER 10 000 CANDELA VISIBLE OVER 14 8 KM 8 NM POWER SYSTEM CONSISTS OF SOLAR ARRAY BATTERY INTERCONNECTING CABLE 1 7 All these Solar Lighting shall have a minimum of 7 full days of autonomy at full light output without any solar or AC charging If in case there are an unusual number of days without sunlight the lights will not turn off they will only dim slightly according to the amount of energy that is still stored Lead in Lighting System 2 1 The system includes five barrettes of lights each containing 3 lights flashing simultaneously and in sequence towards the extended Runway 21R centerline The barrettes of lights shall be located approximately 500 meters apart 2 2 Each 3 lights barrette shall be furnished with a Battery Box and a Solar System including all the associated enclosures mountings interconnecting cables Power and Control Box as illustrated in Figure 2 below NOTIAI NIN NVVN YNWA NYNA NITY NIYI a VHA ATNI Ynwn qax Israel Airports Authority Planning and Engineering Division Figure 2
4. Lead In Barrette Schematic 3 LIGHTS BARRETTE SOLAR PANEL POWER amp CONTROL BOX INTERCONNECTING CABLES 2 3 Specification 2 3 1 Compliant to FAA E 2980 Clauses 3 1 3 2 1 amp 3 1 3 2 1 or UFC 3 535 01 Clause 3 5 4 2 Elevated Sequenced Flasher Effective Intensity The rated effective intensity must be not less than 8 000 FAA 7 500 UFC candelas or more than 20 000 FAA 22 500 UFC candelas for 15 degrees horizontally and 5 degrees vertically from the beam axis 2 3 2 Compliant to FAA EB67D Standard Clause 2 1 1 Chromaticity 2 3 3 Compliant to ICAO ADM Part 4 Chapter 6 Guidelines for Runway Lead in Lighting System 2 3 4 The lights shall be controlled and remote activated by a Wireless Handheld Controller 2 5 mile 4 km range up to 5 stepped intensities 100 20 4 0 8 0 16 or custom set The remote activation signal shall operate the barrette nearest to the Controller and shall be transmitted in chain to the other barrettes e g by internal GPS 2 3 5 A Control Box shall be located at the base of each barrette support tower and includes a 2 4GHz control radio antenna LOCAL REMOTE selection and control card The control box interfaces with the radio controller in the tower 2 3 6 The power system consists of the following components A Asolar array module with a high efficiency panel B A Battery Box Assembly BBA that provides energy storage of 24VDC C Int
5. er conditions or blackout 5 2 Grouping capabilities allow up to eight subsets of lights to be controlled independently 5 3 Contains a radio modem supporting electronics and external serial interface 5 4 Waterproof Tested to Condition B Method 104A of MIL STD 202F Immersion 5 5 Operating temperature range from minus 30 to plus 55 C 5 6 Weatherproof variable intensity back lit LED keypad and LED indicators 5 7 Antenna 1 2 wave dipole removable 5 8 Frequency 902 928 MHz FHSS 5 9 Maximum control range 2 5 miles 4 km 5 10 Maximum weight 1 5 kg 5 11 Housing Die cast aluminum 5 12 Battery Type SAFT Lithium ion MP long cycle life series 3 75 V 5300 mAh Continuous use 1 operation min 12 hours Standby 330 hours Long term storage without recharging 1250 hours Recharge time 5 hours 5 13 Battery State of Charge and Radio Health can be queried via the handheld controller Technical Documentation NOTIN NIN NVVN Yaw nownaA NITY NIYI a4 VHA ATNI Ynwn qax Israel Airports Authority Planning and Engineering Division The responder must attach to his offer at least the following 6 1 Detailed Specifications of the equipment 6 2 Installation and Operating Instructions 6 3 Maintenance Instructions including Trouble Shooting 6 4 Parts List 6 5 In house Detailed Tests Reports assuring the performance of the lighting systems as set above including a test or a simulation for exact number of days and hours the lighting sys
6. erconnecting cable 15 m 2 3 7 The solar module shall meet the full power consumption requirements The module will be installed and will be orientated for maximum solar harvesting nNOTIAI NIN NVN INW AYNA NITY NIVI a MIN ATNI MWN QAX Israel Airports Authority gt gt Planning and Engineering Division 2 3 8 A redundant universal AC on one side of the Battery Box Assembly BBA shall be provided It can be connected to AC power 231 VAC 50Hz Once the AC power source is removed the system will automatically revert to solar power 2 3 9 Each light assembly contains LED based optics to achieve low consumption high intensity and the sharpest color for maximum visibility in all weather conditions Individual head light outputs is visible for 8 nautical miles 14 8 km in good visibility conditions 2 3 10 Construction powder coated aluminum chassis Stainless steel and anodized aluminum hardware Ingress Battery Box and Control Box NEMA 4 or EN 60529 IP55 Aviation orange or yellow painting 2 3 11 The complete system shall function properly with no damage at A Ambient air temperature minus 30 C to plus 55 C B Desert dust and sand storms and very high UV radiation C Wind Loading 150 knots 278 km h D Seven full days operation at full light output without re charging the batteries from the SOLAR Array or from AC power 2 3 12 Chromaticity Fixtures must meet the chromaticity requirements per this paragraph for color of light em
7. itted Testing must be done using a spectroradiometer in increments of 2nm or less Testing must be conducted after the applicable photometric test warm up time or after stabilization if warm up time is not specified Aviation White LED Chromaticity Boundaries Yellow boundary x 0 440 Blue boundary x 0 320 Green boundary y 0 150 0 643x Purple boundary y 0 050 0 757x Boundary Intersection Points for Aviation White x 0 320 y 0 356 x 0 440 y 0 433 x 0 440 y 0 383 x 0 320 y 0 292 2 3 13 High Temperature Test Manufacturer must ensure that the light output of the fixture does not drop more than 30 of the photometric requirement when operated at high temperature The photometric measurement must be done after stabilization at 25 C and again after 4 hours of continuous operation at 55 C 2 3 14 The equipment shall include mounting hardware for permanent installation 3 Runway Alignment Indicator Lights RAIL 3 1 The system consists of five Sequenced Flashing Lights SFL towards Runway 21R threshold at a steady rate between 60 and 120 times per minute The interval between flashes of adjacent lights must nominally be 1 30 seconds The Flashing Lights shall be located on the extended centerline of RW 21R with 60 meters spacing at a distance of 720 to 480 m from the RW Threshold NOTIAI NIN NVN INW AYNA NITY NIVI a MIN ATNI MWN QAX Israel Airports Authority y Planning and Engineering Divisio
8. n 3 2 Each RAIL Light is powered by it s internal pure lead Valve Regulated Lead Acid batteries and is equipped with it s own solar panels ensuring the batteries are constantly charged Battery lifespan will be approximately 5 years Each light shall include provision for 230VAC 50Hz input to charge the batteries 3 3 Optical High power LEDs with proper heat management ensuring consistent photometric for the life of the product MALSR FAA and ICAO compliant Aiming 6 degrees above horizontal 3 4 Construction Powder coated aluminum chassis with integral handles Aviation orange or yellow Stainless steel and anodized aluminum hardware 3 5 Additional specification requirements for the RAIL flashers apply per paragraph 2 3 above Lead in Flashers sub paragraphs 2 3 1 2 3 2 2 3 4 2 3 11 2 3 12 2 3 13 2 3 14 Runway End Identifier Lights REIL Optional per IAA Discretion 4 1 In conjunction with the RAIL system a pair of two flashers shall located on both sides of the Threshold of Runway 21R These two flashers shall flash simultaneously synchronized at the end of each forward sequence of the RAIL flashers 4 2 The requirements and specifications for the lights are as detailed in paragraph 3 above RAIL Handheld Wireless Controller For The Solar Lighting Systems 5 1 Wireless control allows for remote operation of above mentioned solar lighting systems including mode changes for enhanced visibility in poor weath
9. nway Edge and Threshold lighting both runways 1 3 2 SALS Short Approach lighting 420 m 2 approaches to the West Runway 1 3 3 PAPI Precision Approach Path Indicator 2 sides of both runways 1 3 4 REIL RW End Indicator Lights 2 ends of West Runway 1 3 5 Taxiways Edge lighting 1 4 Runway 21R West is equipped with ILS DME The Localizer beam is shifted 5 degrees from the runway centerline 1 5 During Instrument approach to landing on runway 21R particularly in daytime with reduced visibility conditions the pilot might first distinguish Threshold 21L East RW td 7 Se a E O frm aja 2 nOTIAI PN NVVN YNN nownna NITY NIYI a VHN ATNI Ynwn qaX Israel Airports Authority P Planning and Engineering Division and divert to land on it instead of continuing the approach to land on Runway 21R West RW 1 6 To enhance visually the shifted approach route to land on Runway 21R additional Solar Ground Lighting shall be provided as follows and as illustrated in Figure 1 below 1 6 1 Lead In Lighting System 1 6 2 Runway Alignment Indicator Lights RAIL 1 6 3 Runway End Identifier Lights REIL Figure 1 Lead In Lighting amp Approach Sequenced Flashers APPROACH LIGHTING LEAD IN LIGHTS w k 850m 1 585m S Approximately 2 100m z ir Localizer 5 zoom 5 Sequenced Flashers RAIL 2 pogani REN Solar P A Whed 5 Sequenced Groups of 3 flashing lights Barrette i olar Powere eless Shit ete ee Solar Powered Wireless
10. scription Quantity Airport Heliport Month Year Remarks Contact Ref Lead in Flasher Lead in Solar Array Lead in Battery Lead In Wireless Control RAIL Flasher Solar RAIL Wireless Control REIL Flasher Solar REIL Wireless Control Wireless Hand Controller NOTIN NIN NVVN Yaw nowNaA NITY NIYI a VHA ATNI Ynwn qax Israel Airports Authority Planning and Engineering Division 8 Responder Proposal Bill of Quantities 8 1 The responder shall fill details for all equipment included in each item in the following table including listing of additional required equipment if not mentioned in the table 8 2 Final quantities are subject to customer discretion with no change in unit price 8 3 All prices include User Manual 3 hard copies Digital Data Item Title Equipment Included Model Qty 1 1 Lead In 3 Lights LED Assy 6 1 2 Barrette Solar Panel 6 1 3 Battery Box Assy 6 1 4 Power amp Control Box 6 1 5 Interconnecting Cables 6 1 6 Spare Light Head 3 2 1 RAIL Chassis Flasher Head 6 Sequenced GPD Radio Mounting Flasher hardware Battery Assy 2 2 Spare Light Head 3 1 REIL Flasher Chassis Flasher Head GPD Radio Mounting hardware Battery Assy 3 2 Spare Light Head 1 4 1 Handheld Controller Battery 1 4 2 Controller Spare Battery 1 5 Training 1 6 Optional Travel Assistance in
11. tems shall function without solar or AC recharge of batteries 6 6 Minimum Warranties Light fixtures must be warranted by the manufacturer for a minimum of 4 years after date of installation inclusive of all electrical and electronics batteries solar array wireless handheld controller 6 7 ETL Test Report of the Lights compliant per 6 7 1 FAA E 2980 Clauses 3 1 3 2 1 amp 3 1 3 2 1 or UFC 3 535 01 Clause 3 5 4 2 Elevated Sequenced Flasher Effective Intensity 6 7 2 FAA EB67D Standard Clause 2 1 1 Chromaticity Responder Declaration For Proposed Equipment The responder must fill the following tables 7 1 Table of Compliance to Requirements Paragraph Mandatory Comply Documents Attached Required YES or NO To be filled by the Responder 2 3 1 2 3 2 2 3 3 2 3 4 2 3 5 2 3 6 2 3 7 2 3 8 2 3 9 2 3 10 2 3 11 2 3 12 2 3 13 2 3 14 3 1 3 2 2RIWIA AINA NITY NIVI a Israel Airports Authority Ba Planning and Engineering Division NOTIAI PN NVVN VHX ATNI TAWN QAX Paragraph Mandatory Comply Documents Attached Required YES or NO To be filled by the Responder 3 3 3 4 3 5 4 1 4 2 5 1 5 2 5 3 5 4 5 5 5 6 5 7 5 8 5 9 5 10 5 11 5 12 5 13 7 2 Reference List The Responder shall provide full information for at least 2 projects De
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