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1. REMOS G 3 600 E 04 Remarks and Alterations Applied Modifications Pos Page Description Date Sign EREM os G 3 600 05 Table of Contents General information about this handbook This Flight Operation Handbook is divided into several chapters These chapters can be identified quickly by the use of the colored markings on the top corners of each side The structure of this handbook complies to the Light Sport Aircraft airworthiness standards Contents 1 General Information Page 1 1 Introduction 12 1 2 Certification 12 1 3 Quick Reference 12 1 4 Technical Specifications 13 2 1 Engine overview 14 2 2 Engine 15 2 3 Propeller Gearbox 15 2 4 Fuel and fuel capacity 15 2 5 Engine oil coolant 16 2 6 Operating weights and loading 16 2 7 Cockpit and basic equipment 17 2 8 Center panel controls and circuit breakers 18 2 9 Engine control gauges Rotax Flydat 19 2 10 Additional gauges basic equipment 20 ER EMOS G 3 600 06 Table of Contents 3 1 3 2 3 3 3 4 3 5 3 6 3 7 4 4 1 4 2 4 3 4 4 4 5 4 6 4 7 Airspeed limits Crosswind and wind limitations Service ceiling Load factors Prohibited maneuvers Center of gravity range Permissible flight maneuvers Weight and Balance Information Installed equipment list Weight and balance form Center of gravity CG range and determination CG calculation CG calculation exa
2. 9 3 Passenger warning Passenger Warning This aircraft was manufactured in accordance with Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements 9 4 No intentional spins NO Aerobatics NO IMC Flights or robatics IMC Flights Spins PROHIBITED NO Intentional Spins REMOS G 3 600 E 60 9 5 Required Placards and Markings Miscellaneous placards and markings The following safety placard is located in front of the rescue system area indicating that no luggage or clothes should be placed there This is a safety advisory to guarantee the proper operation of the rescue system CAUTION CAUTION CAUTION Do not block this area due to rescue system operation Overhead each cabin door you will find the following emergency placard This placard indicates the direction to which the door safety pin has to be removed in order to release the door from the fuselage Emergency Eject Beside the sight fuel gauge behind the seats you will find the following decal which indicates the fuel empty position When the indicated fuel quantity is level with that marked by the decal 0 5 gallons of fuel remains in the fuel tank EMPTY 4 EREM os G 3 600 61 9 Required Placards and Markings Inside the cabin a starting checklist and related placards are provided as quick reference guide for starting the engine FUEL SHUT OFF VA
3. 2 10 Additional gauges Electrical fuel quantity gauge basic equipment For a comfortable fuel quantity reading an electrical fuel gauge is provided with the basic equipment of your REMOS G 3 600 additional to the fuel level sight gauge If the needle indicates zero there are 0 5 gallons left in the fuel tank For flight safety it is strongly recommended to double check the reading on the level sight gauge Manifold outside temperature gauge optional This digital temperature gauge enables a precise measurement of manifold and outside temperature An alert function indicates when carburetor heating is recommended Alert temperature threshold is adjustable Manifold Outside Temp 65 _ lt _ _ _ pas YN IN Manifold temperature Out Outside temperature Dace For detailed information please refer to the sepearate operators manual EREM os G 3 600 20 Choose between carburetor manifold temperature and outside temperature see left Adjust alert temperature Reset button Choose temperature to be displayed manifold outside Alert tell tale to indicate that true temperature is below alert temperature setting Recommended 55 F Instruction placard 3 Operating Limitations 3 1 Airspeed limits all airspeeds at maximum takeoff weight Mark Speed CAS Description VNE Never exceed speed 153 mph Airspeed which shall never be 133 kts
4. 37 kts 39 mph 34 kts As the aircraft approaches the stall speed this will be indicated by slight aerodynamic buffeting The stall speed is reached when the aircraft becomes unstable in flight but should still be controllable It is also possible to perform a stall while in a turn but it has to be considered that the stall speed will increase see table above EREM os G 3 600 46 8 Aircraft Ground Handling and Servicing 8 1 Servicing fuel oil and coolant The REMOS G 3 600 is designed to be easily serviceable Access to all components which have to be lubricated or checked regularly is possible without detaching any panels A flap in the upper cowling allows checking water and oil without removing the cowling The fuel filler cap is located on the right hand side of the fuselage behind the wing After removing the lockable fuel filler cap refueling is easily possible The basic equipment provides two gauges to check fuel level from inside the cockpit The first one is a fuel level sight tube located between the seats and an additional electric fuel gauge is installed on the right hand side of the instrument panel Refer to Chapter 2 Airplane and Systems Descriptions for further instructions regarding specifications and capacities 8 2 Towing and tie down instructions Due to the low weight of the REMOS G 3 600 it is very easy to move the aircraft on the ground by hand That s why there is no special equipment for towi
5. Attention Near to the release clutch 3 Weak link maximum 300 daN REM os G 3 600 89 Pilot Operating Handbook REMOS G 3 600 Edition 4 Rev 03 01 07 2008 USA Editor Layout amp Graphics Hans Fuchs Advice Josef Sporer c REMOS 2000 2007 all rights reserved
6. Lubricate wing main bolts and horizontal stabilizer attachment bolts using regular grease 7 Lubricate wings plastic ball joints using regular grease 8 Check all joints bolts nuts splines for correct seating 9 0 1 Na Field test of wheel brakes and inspect brake pads discs for wear exchange if necessary Check tires air pressure profile and entire surface for wear and damage Check wings rudder stabilizer and landing gear for damage and proper attachment and connection to the fuselage 12 Check control cables and control linkage tubes for freeplay damage or cracks 13 Check propeller and spinner for cracks and other damage replace if necessary 14 Check and lubricate tow release clutch if fitted Every 200 hours spark plugs have to be exchanged REMOS G 3 600 E 48 8 Aircraft Ground Handling and Servicing 8 4 300 hr service Every 300 hours the following additional checks services are required 1 Exchange brake fluid DOT 4 aircraft brake fluid must NEVER be used 2 Check carburetors for wear and correct adjustment carburetor synchronization Check control wires of choke throttle propeller tow release clutch if fitted and oil cooler flap for corrosion and free play Check main gear bolts and bushes for corrosion and proper seating Check condition of rubber engine mounts for wear Exchange engine coolant Check all fuel coolant and oil hoses and fittings for wear and cracks Check m
7. position 2 Ensure that the elevator trim is in correct position 3 Whenever possible takeoff directly into wind The maximum crosswind limitation for takeoff is 17 mph 15 kts 4 Smoothly apply full throttle fully forward and maintain runway heading 5 As the aircraft accelerates gently pull back on the control stick to elevate the nose slightly until the aircraft becomes airborne 6 Once airborne slowly release the back pressure on the control stick to allow the airspeed to increase to 63 mph 55 kts Maintain this speed and avoid making any climbing turns until a sufficiently safe altitude has been reached 7 When all obstacles have been cleared rectract the flaps 0 position Takeoff at tailwind conditions Similar to normal take off except an extended takeoff run distance The takeoff run distance is affected by weather and surface conditions as well as the takeoff weight of the aircraft However average distance is 170 to 330 ft EREM os G 3 600 66 10 Supplementary Information 10 1 Flight training supplement 10 1 3 Climbing Climbing after takeoff Once airborne establish an indicated airspeed of 75 to 80 mph 65 to 70 kts This airspeed will achieve the aircrafts best rate of climb resulting in a 1100 to 1300 ft min climb rate During the climb it is essential to watch oil and water CHT temperatures Adjust the oil temperature regulation flap as required Climbing while in cruise If you have to climb
8. the wing must never be lifted or pushed on top 4 When the wing has reached its forward position the person at the fuselage position has to rotate the wing to align both connection latches Care has to be taken that the surface of the wing is not damaged by the fuselage connecting latches 5 When the connection latches between the fuselage and wing are aligned the wing must be lifted by the person at the wing tip The person at the fuselage must ensure that flap drive connection fits correctly into the bushing on the fuselage 6 Ifall latches have engaged and the wing fits properly to the fuselage the main bolt can be pushed into its support tube To install the main bolt correctly please use the special installation tool which comes with the aircraft Now secure the bolt with the securing pin 7 The person at the wing tip can now release the pressure supporting the wing tip Inside the cabin the pushrod connection of the ailerons MUST be established 8 Proceed in identical order with the second wing EREM os G 3 600 51 8 Aircraft Ground Handling and Servicing 8 9 Installing horizontal stabilizer Like connecting the wings it is recommended to follow this procedure by two persons One person is needed to hold the stabilizer in place while the second person applying the two fixing bolts into their bushes through the fuselage tail Afterwards each bolt have to be secured by a cowl pin Attention watch for the markings on the st
9. 1 1 Introduction 79 1 2 Certification 79 1 3 Quick reference 79 2 14 Cockpit 80 3 1 Maximum permissible towing speed V7 81 3 2 Maximum weak link strength 81 3 3 Maximum permissible all up weight of the glider to be towed 81 4 Weight and Balance Information Page 4 1 General 82 4 2 Equipment 82 5 1 Takeoff distances 84 5 2 Takeoff distance effected by external circumstances 84 5 3 Tested glider configuration 85 10 Supplementary Information 10 2 Towing glider _ Table of Content o O oO 6 1 Engine failure 6 2 Additional procedures 6 3 Failure of the release clutch 86 7 1 Preflight check 7 2 Takeoff A 7 3 Descent and landing 87 Aircraft Ground Handling and Servicing 8 1 Servicing tow release clutch 88 9 1 Cockpit 9 2 Release clutch EREM os G 3 600 78 10 Supplementary Information 10 2 Towing glider 1 General Information 1 1 Introduction This aircraft shall be operated only with a valid license including a glider towing rating An specific type rating on the REMOS G 3 600 is required This supplement is to be used in addition to the REMOS G 3 600 Pilot Operating Handbook only 1 2 Certification The REMOS G 3 600 complies to the rules of the Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements 1 3 Quick reference For the use as a glider towing aircraft the REMOS G 3 600 is equipped with the Tost E85 tow release clut
10. 10 seconds in order to avoid overheating the starter EREM os G 3 600 40 AO Ng continued next page 7 Normal Procedures continued from previous page If the engine does not start release the key to position 0 wait 2 minutes and repeat the procedure 5 Release ignition key immediately after the engine has started 6 Push the choke lever forward 7 Switch off the electric fuel pump Starting a hot engine 1 Pull the throttle lever back to the idle position 2 Turn the key clockwise to the Start position until the engine has started do not hold the key in the Start position for more than 10 seconds in order to avoid overheating the starter 3 Release ignition key immediately after the engine has started After starting the engine 1 Check oil pressure immediately after the engine has started 2 Adjust engine rpm as required for warm up maximum 2500 rpm 3 Before take off oil and water temperature must reach at least 120 F 4 Switch on avionics master switch and avionics as required Engine rpm and propeller check Set parking brake Adjust engine to 4000 rpm Check both magnetos maximum rpm decrease 300 rpm Set engine to idle release parking brake EREM os G 3600 41 PUNS 7 Normal Procedures 7 3 Taxiing The steerable nosewheel of the REMOS G 3 600 allows easy ground handling Turns of 49 feet in diameter can be conducted easily The main gear is equipped with effective hydraulic disc br
11. 21 Trim and Flap indicators 8 Flydat refer to page 19 17 9 18 REMOS G 3 17 2 Airplane Systems and Description 2 8 Center panel controls and circuit breakers The most important switches for operation of the aircraft are placed on the center panel The illustration below shows the basic equipped aircraft ee a RS EEEE i task worse at 2 Illustration below Circuit breakers and related devices if fitted 10 11 Main Fuses Master Fuse 25A 5 Fi Clock Temp Gauge Memory 3 6 A Master Switch Fuel Pump Position Lights ACL 10A 6 Landing Instr Lights Volt Fuel Gauge Eng Gauges 10A Trim Flap Drive 10A 7 Starter Relay Adjustable Prop Constant Speed 10A 8 Avionics Fuses GPS 12V Receptacle 10A 9 inni Flight Computer Directional Gyro 10A Avionics Switch EFIS PFD Attitude Gyro 10A 10 EFIS MFD Turn Indicator 10A Transponder Blind encoder 10A Radio Intercom 10A REMOS G 3 600 18 Trim control switch Flap control switch Flaps are extended continuously while pushing down the switch Flaps are automatically retracted when switched to the upper position Flap position is indicated on the gauge beneath All switches in upper position on ACL switch anti collision light Electric fuel pump Position lights Instrument avionics illumination if installed Circuit breakers for master amp avionics circuits Master switch all electric systems on or off C
12. Once the aircraft is trimmed well it will maintain its altitude and heading without doing anycorrection to the control stick for extended periods If required the aircraft is capable of achieving an airspeed up to 138 mph 120 kts at full power setting If doing so it is strongly recommended not to exceed the maximum continuous engine rpm for more than five minutes Please refer also to the latest engine operators manual Cruising in gusty conditions When flying in gusty weather conditions the maximum permissible airspeed of 115 mph 100 kts should not be exceeded for safety reasons The REMOS G 3 600 offers very stable flight characteristics even in heavy weather conditions similar to that of a Cessna 172 EREM os G 3 600 68 10 Supplementary Information 10 1 Flight Training Supplement 10 1 5 Stall The REMOS G 3 600 is fully controllable when flying at a wide range of airspeeds however if the lower speed limits exceeded the aircraft will display very stable stall characteristics If the airspeed is reduced by the pilot gradually pulling back on the control stick aerodynamic buffet will occur indicating that the aircraft is approaching the stall speed Should the aircraft then be allowed to stall the aircraft will remain controllable and the maneuver will result in a gentle and stable descent The aircraft can be stalled both with flaps extended or retracted Conducting a stall maneuver does not require a special skill never
13. b Takeoff weight glider 1300 Ib Pressure alt 1550 1615 1680 1745 1810 1875 1940 2005 2070 2135 2200 air pressure ft InHG Takeoff distance in feet wind calm above 50 ft obstacle within the condition of the ICAO standard atmosphere Flaps 15 EREM os G 3 600 84 10 Supplementary Information 10 2 Towing glider 5 Performance 5 2 Takeoff distance effected by external circumstances Various circumstances will have an effect on the takeoff distance of the aircraft The following listing gives you an estimation of the values e High grass 15 to 20 e Dirty wings rain drops 10 to 15 e High air temperatures 5 to 10 e Nose wind component 20 e Tail wind component 15 to 20 5 3 Tested glider configuration The following gliders have been tested and certified by the factory LS 4 Baby lll Twin lll Hornbach Discus Blanik DG 500 ASK 21 DuoDiscus MiniNimbus Astir CS ASW 24E motorglider REMOS G 3 600 85 10 Supplementary Information 10 2 Towing glider 6 Emergency Procedures 6 1 Engine failure If an engine failure occurs during glider towing the glider pilot must be informed immediately by radio to disengage the tow rope Alternatively the rope can be released at the towing aircraft For further information please refer to the chapter Emergency Procedures included in the REMOS G 3 600 Pilot Operating Handbook 6 2 Additional procedures If an
14. balance form The CG determination shall refer to the valid weight and balance form REMOS G 3 600 a 24 4 Weight and Balance Information 4 3 Center of gravity CG range and determination To determine the real weight and the center of gravity it is required to follow the descriptions below Wing Reference Point R P Main Chord d O To get the correct values it is necessary to put the aircraft on three weighing scales located on a level Y ii surface Before conducting the weighing procedure it is important to achieve a level wing main chord use suitable pads between main wheels and scale beneath to hoist aircraft vag es A check mark R P on the leading edge of the left wing G1 adjacent to the wing root is provided to ease examination that ee a wing main chord is level use a flexible clear tube filled with n water as spirit level To get the total weight G you have to add i value G1 and G2 The center of gravity has to be calculated using this value The CG located at the distance X from R P is measured near the fuselage ee REMos 63600 ___ 25 4 Weight and Balance Information 44 CG calculation The following procedure allows the correct calculation for the center of gravity Torque Ib Inch Weight Ib x Leverarm Inch Total Torque Ib Inch Center of Gravity Inch Total Weight Ib Weight Leverarm Torque lb Inch Ib Inch Empty weight Seats 8 3 Fu
15. be within the limits of 9 6 thru 16 3 inch measured from the leading edge of the wing close to the fuselage To determine the CG the weight of the aircraft has to determined equipped with all devices ready to fly except fuel and baggage 2 10 Permissible flight maneuvers The following maneuvers are permitted e Stall e Night VFR flights e Slow controlled figure eight e Turns e Maximum angle of bank 60 Permissible only with the REMOS Night VFR Kit installed according to Section 16 REMOS G 3 600 Maintenance Manual issued July 1 2008 REMOS G 3 600 23 4 Weight and Balance Information 4 1 Installed equipment list To comply with the rules of the Light Sport Aircraft airworthiness the listed minimum instrumentation and equipment is provided as standard equipment e Airspeed indicator e Altimeter e Vertical speed indicator e Compass e Slip indicator e RPM gauge Rotax Flydat e Oil pressure gauge Rotax Flydat e Oil temperature gauge Rotax Flydat e CHT gauge Rotax Flydat e Exhaust gas temperature gauge Rotax Flydat e Electric fuel gauge e Position lights e ACL Anti Collision Light e Master avionics and engine kill ignition switch e Electrical system including circuit breakers e 4 Point safety belts pilot and passenger 4 2 Weight and balance form The complete equipment list including all additional and optional equipment has to be listed in the separately provided weight and
16. exceeded Vu Maximum speed in 137 mph Maximum airspeed at maximum level flight 119 kts continuous power setting Va Maneuvering speed 98 mph Maximum airspeed for all 85 kts permissible maneuvers Vg Maximum airspeed in 123 mph Airspeed which shall never be turbulence 107 kts exceeded in gusty weather conditions VEE Speed range 45 to 81 mph Airspeed which shall never be Flaps extended 39 to 71 kts exceeded in flaps down configuration Vso Minimum airspeed 45 mph Minimum permissible airspeed in Flaps extended 40 39 kts flaps down configuration Vs Minimum airspeed 49 mph Minimum permissible airspeed in Flaps retracted 0 42 kts flaps up configuration Vapproach Approach airspeed 59 mph Recommended airspeed for 51 kts approach with full payload REMOS G 3 600 21 3 Operating Limitations 3 2 Crosswind and wind limitations This aircraft must be flown under VFR flight conditions only Maximum permissible wind speed Headwind 28 mph 25 kts at takeoff and landing Crosswind 17 mph 15 kts 3 3 Service ceiling Maximum permissible service ceiling 15 000 ft 3 4 Load factors Safe multiple load range 49 2g 3 5 Prohibited flight maneuvers Flight conditions not permitted e IFR flights e Aerobatics e Tailspin e Flights through or within clouds e Flights in icing conditions REMOS G 3 600 o 22 3 Operating Limitations 3 6 Center of gravity range The permissible range for the center of gravity during flight has to
17. exercise crosswind landings only when accompanied by an experienced flight instructor until sufficient experience has been gained Approach in turbulent weather conditions If turbulences are indicated or wind shifts are expected we recommend to establish an airspeed of 65 mph 56 kts This will give you a reserve airspeed to balance any unexpected deviations in altitude and heading In more gusty conditions it may beneficial to stabilize the glide slope by keeping the flap setting to the 15 position Increasing airspeed above 65 mph 56 kts will not be helpful to stabilize the aircraft so this should be avoided Approach in rain showers Raindrops on the wing surfaces influence the aerodynamic characteristics of the airfoil drag will increase while lift decreases The REMOS G 3 airfoil used on the REMOS G 3 600 features stable flight characteristics in rain conditions So there are no special advisories for flights within rain we recommend to operate the aircraft like in turbulent weather conditions see Approach at turbulent weather conditions EREM os G 3 600 73 10 Supplementary Information 10 1 Flight training supplement 10 1 9 Approach Approach in the slip configuration If a high descent rate is required on final we recommend to conduct a slip manoeuver In no case push the control stick forward this will cause higher airspeeds and result in a missed approach Conducting an approach in the slip configuration will
18. it is important to watch engine temperatures During descent the temperatures will decrease which could cause engine failures or carburetor icing to develop So it is strongly recommended not to exceed the lower limits of these temperatures REMOS G 3 600 71 10 Supplementary Information 10 1 Flight training supplement 10 1 9 Approach Approach under normal conditions Always land on the most suitable runway consider the wind direction size of the runway obstacles on the approach etc Avoid airspeeds above 75 mph 65 kts or below 55mph 48 kts when on final Due to the excellent gliding performance of the G 3 600 higher airspeeds would not be helpful during the flare and would extend landing Approach under tailwind conditions When making a final approach with a slight tailwinds present the G3 does not require different approach or flare procedures to that when flown in calm or headwind conditions you do however have to keep in mind that the landing distances will increase EREM os G 3 600 72 10 Supplementary Information 10 1 Flight training supplement 10 1 9 Approach Approach in crosswind conditions Cross winds will not have a big effect to the flight characteristics or the G 3 600 as long as wind speed stays within the maximum permissible speed up to 17 mph 15 kts Conducting a cross wind landing does will not require special skills nevertheless if not yet familiar with the aircraft we recommend to initially
19. stabilizer 52 8 10 Final check after assembling 52 8 11 Disassembling the aircraft 52 8 12 Airframe servicing 53 8 13 Main gear servicing 53 8 14 Nose gear servicing 54 8 15 Hydraulic brakes 54 8 16 Disassembling and assembling wheels 55 8 17 Wheels and tires 56 8 18 Changing engine oil 56 8 19 Exhaust system servicing 57 8 20 Propeller servicing 58 8 21 Airbox system and air cleaner element 58 Table of Contents 9 Required Placards and Markings Page 9 1 Airspeed indicator range markings 59 9 2 Operating limitations on instrument panel 60 9 3 Passenger warning 60 9 4 No intentional spins 60 9 5 Miscellaneous placards and markings 61 10 Supplementary Information Page 10 1 Flight training supplement 64 10 2 Towing glider 77 REMO s G 3 600 10 Views The REMOS G 3 600 is designed as full composite carbon fiber amp fiberglass aircraft You will find detailed information on the following pages Wingspan 32 3 ft 9800mm Height 5 5 ft 2280mm r Overall Length 21 4 ft 6470mm EEMS C3600 11 1 General Information 1 1 Introduction This Operation Handbook is designed to help enable a safe and successful completion of each flight with the REMOS G 3 600 It provides you with all necessary information for regular maintenance and operation of the aircraft Therefore we recommend that the pilot keeps this Operating Handbook upgraded with the newest information available You can get the newe
20. wheel nut the axle can be withdrawn from the wheel spat and the complete wheel assembly can be removed from the fairing 3 Remove the wheel Remove the luggage compartment by Discard two cable ties to disconnect B from the axle and unscrewing the three fixing screws the T connector from the fuselage withdraw the wheel assembly from the fairing Watch for the assembling order of each part during disassembling Assembling Remark has to be carried out in reverse order Take great care to secure all bolts and nuts as required EREM os G 3600 55 8 Aircraft Ground Handling and Servicing 8 17 Wheels and tires The wheels of the REMOS G 3 600 consists of three piece aluminum wheel equipped with multiply tires The maximum air pressure applied in the tires must not exceed 34 psi Low air pressure should also be avoided as it enables slip between tire and wheel which could cause damage to the air bleed valve and tube To ensure that no slip has occurred remove the word please check the slip markings on each main wheel prior to every flight Whenever tires have to be replaced we strongly recommend to check the wheel discs for cracks especially the area where the discs are screwed together After fitting new tires wheels have to be balanced because badly balanced wheels will create vibrations after takeoff during taxiing and braking Safety main gear wheel with piake ee uppalt 8 18 Changing engine oil also see Rotax oper
21. 1260 12130 13000 13860 14720 15590 16460 17320 Total torque regarding to the CG calculation Ib Inch EREM os G 3 600 28 4 Weight and Balance Information 4 7 Aircraft specific weights Below the aircraft specific data shall be notified Pilots must use this information to ensure a correct weight and balance calculation prior to every flight This is essential for a safe conduction of each flight Empty weight Ib Maximum take off weight Ib Maximum payload Ib Center of Gravity CG inches behind R P ae ReMos G 3600 29 5 Performance 5 1 Takeoff and landing distances Distance 100 hp engine Takeoff run distance 330 ft Takeoff distance flaps 0 730 ft Takeoff distance flaps 15 660 ft Landing distance 850 ft 5 2 Rate of climb Description 100 hp engine Airspeed for best 63 mph 55 kts 5100 rpm climbing Maximum climb rate 1300 fpm Descent rate at idle 400 fpm Airspeed for best gliding 60 mph 52 kts flaps 15 wind calm over 50 ft obstacl in ICAO standard atmosphere conditions EREM os G 3 600 30 5 Performance 5 3 Takeoff distance effected by external circumstances Various circumstances have an effect to the takeoff distance of the aircraft The following listing gives you some suggestions about the values e High grass 15 to 20 e Dirty wings rain drops 10 to 15 e High air temperatures 5 to 10 e Nose w
22. Engine oil Automobile engine oils Engine oil capacity 0 75 gallons 2 8 litre Recommended oil Shell Advance 10W 40 semi synthetic Recommended cooling fluid BASF Glysantin green Coolant capacity 0 65 gallons 2 5 liters mixture antifreeze water 1 1 2 6 Operating weights and loading Maximum permissible take off weight W 1320 Ib 600 kg Minimum useful load Wy 430 Ib 195 kg Maximum empty weight We 890 Ib 405 kg Minimum empty weight 626 Ib 280 kg Minimum flying weight 740 Ib 336 kg Occupants at minimum empty weight 513 Ib 233 kg Baggage 66 lb 30 kg Fuel max 126 b 57 kg No aircraft engine oils refer to Rotax operation instructions Empty weight with basic equipment like described within the Pilot Operating Hanbook without rescue System REMOS G 3 Values are subject to change without notice please refer to 16 the latest issues of the appropriate manufacturer manuals 2 Airplane and Systems Descriptions 2 7 Cockpit and basic equipment Remark This illustration shows the basic equipment only Instruments and switches 1 Airspeed indicator 10 22 Throttle lever 2 11 23 Charge indicator light 3 Altimeter 12 24 Master switch 4 Slip indicator 13 25 Ignition key magneto check 5 14 19 Trim Flap control switch 26 Avionics master switch 6 Vertical speed indicator 15 20 Device switches 27 Circuit breakers 7 Compass 16 Fuel quantity gauge
23. Ib We recommend to maintaining 1300 Ib as maximum weight of the glider to be towed when operated with the standard fixed pitch propeller During glider towing operations the REMOS G 3 600 must be operated only by one pilot no passenger allowed except for training instruction The total take off weight towing aircraft glider must not exceed 2400 Ib REM os G 3 600 81 10 Supplementary Information 10 2 Towing glider 4 Weight and Balance Information 4 1 General When the aircraft is used for glider towing the weight and balance calculations like in the standard configuration are valid also for towing operation Concerning payload there are some restrictions which have to be observed see also chapter 3 within this supplement 4 2 Required equipment The following additional equipment is required for the use as glider towing aircraft Tost tow release clutch type E 85 REMOS mounting frame for tow release clutch Order No 06 005 A Release handle colored yellow REMOS oil temperature regulation flap Order No 08 023 Back view mirror with strut mounting bracket Order No 06 005 G amp 06 005 H a 2 2 a Glider towing is only permitted when the aircraft is equipped with the 100 hp Rotax engine 912 UL S o Remos G 3 600 82 10 Supplementary Information 10 2 Towing glider 4 Weight and Balance Information The following equipment is not part of the center of gravity calculation but necessary for g
24. LVE __START CHECKLIST ee Preflight Control Fuel Level Fuel Shut Off Valve Open Rescue System Unsecured Safety Belts Closed Doors Locked Parking Brake release Controls Checked Master Switch ON Propeller in Start Position Flaps in Take Off Position 15 Oil Temperature Control Pull Avionics Switch OFF Altimeter Set Brakes Locked Choke Pull Engine cold 7 15 oo a0 Propeller clear Starter Engage Avionics Switch ON Outside the cabin this placard is located by the fuel filler it indicates the recommended fuel qualities get 1a approved for the REMOS G 3 600 Refer to the i we a ys 3 engine operators manual to check for additional o SS a fuel types g Le 5 S lt N GF ee E lt Uyg s Freney soyes280 REMOS G 3 600 E N ue 62 acne 9 Required Placards and Markings Outside the aircraft located beneath each wing main bolt you will find this safety placard concerning safety precautions regarding the folding or reassembling of the wings VATTENTION Before removing wing main bolt disconnect aileron rod connection On both sides of the fuselage beneath each static port you will find this decal Please keep in mind that both static ports have to be kept clean Dirt or water inside the static ports will create wrong indicator readings The following placard is
25. abilizer bolts because they are different in length The forward bolt is marked by a V the rearward bolt by H At the end of each bolt you will find a little hole Once the bolt is installed this hole must be aligned with the appropriate hole of the stabilizer bush to fit the cowl pin Now you can connect the cable plug for the electric trim and the elevator pushrod same as aileron connection Finally attach the tail cover and fix it by two screws 8 10 Final check after assembling As final step you have to attach the pitot tube and make sure that all connections are fitted properly and secured as required Make sure that all control surfaces are working without friction and full travel is provided 8 11 Disassembling the aircraft To disassemble the aircraft you have to do the above described procedures in reverse order EREM os G 3 600 52 8 Aircraft Ground Handling and Servicing 8 12 Airframe servicing The body design of the G 3 600 consists from carbon fiber materials which ensures extreme strength and a long lifetime of the whole aircraft Maintenance is reduced to checks of the moving parts such as locks hinges and connections Prior to each flight a visual check of the whole surface for cracks dents or other damages should be conducted Damage to the airframe composite bodywork must be repaired by skilled and authorized persons only Repairs and services may only be conducted using REMOS original replacemen
26. ain gear for damage and cracks wo ON ROOK 8 5 Cleaning and care After every flight especially in warm climates it is recommended to clean the surface of the aircraft using pure water and a soft cotton towel only Take special care when cleaning the windows to use lots of water to loosen and rinse away bugs and dirt and use with only a soft cotton towel or otherwise you will create scratches If cleaned regularly you may not need to use any special cleaning products If for any reason special cleaning products need to be used please contact your dealer for advice We have approved several products for each area of cleaning please ask for an appropriate recommendation Furthermore we recommend the polishing of the whole aircraft once per year You can use almost any car polish but be sure that no silicone is used in that product Be careful that windows are not touched with polish EREM os G 3600 49 Wing securing aids 8 Aircraft Ground Handling and Servicing 8 6 Folding wing system The G 3 600 is manufactured at highest quality standards all components are highly accurate and provide a maximum aerodynamic quality It is therefore strongly recommended to be most careful when assembling or disassembling components like the wings stabilizer and other parts To fold or attach the wings two persons are required The following instructions will provide you with all the necessary information 8 7 Preparation for assemblin
27. akes which are operated by a lever on top of the middle section between the seats 7 4 Normal takeoff Set flaps to the 15 position Set electric trim to neutral position Switch on electric fuel pump Move rudder and elevator to neutral position at crosswind aileron in wind direction Move throttle lever to full power position After reaching a speed of about 35 mph 30 kts gently raise the nose The aircraft will be airborne after exceeding a speed of about 46 to 52 mph 40 to 45 kts PO One O gt The minimum engine speed for takeoff is 4900 rpm Remark Take off from concrete or hard surface runways can be done also with flaps in retracted position 0 flaps up EREM os G 3 600 42 7 Normal Procedures 7 5 Best angle of climb speed Vx The best angle of climb is at an airspeed of 58 to 64 mph 50 to 55 kts Please watch oil and water temperature during long climbing periods If an oil temperature regulation flap is mounted it must be set to position open or cooler Flight conditions Full throttle flaps up within the ICAO standard atmosphere 7 6 Best rate of climb speed Vy The maximum climb rate of 1300 ft min with fixed pitch propeller is at an airspeed of about 72 to 76 mph 63 to 66 kts Please watch oil and water temperature during long climbing periods If an oil temperature regulation flap is mounted it must be set to position open or cooler Flight conditions Full throttle Flaps up w
28. all obstacles have been cleared then retract flaps Climb to required altitude while increasing airspeed to 72 to 76 mph 63 to 66 kts REMOS G 3 600 E 44 7 Normal Procedures 7 12 Low airspeed and stall The center of gravity is within the permissible range the aircraft will be fully be controllable until reaching the stall speed If stall speed is reached the pilot should lower the nose of the aircraft to reestablish a safe airspeed Performing a stall from level flight CG at most rearward position airspeeds as CAS Flap position 0 15 40 Vmin at idle 42 mph 37 kts 39 mph 34 kts 38 mph 33 kts Vmin at full power 41 mph 36 kts 38 mph 33 kts CG at most forward position airspeeds as CAS Flap position 0 15 36 mph 31 kts 40 Vmin at idle 45 mph 39 kts 44 mph 38 kts 43 mph 37 kts Vmin at full power 45 mph 39 kts 42 mph 36 kts EREM os G 3 600 45 37 mph 32 kts 7 Normal Procedures Performing a stall in turns CG at most rearward position airspeeds as CAS Flap position 0 15 40 Vmin at idle 45 mph 39 kts 42 mph 37 kts 40 mph 35 kts Vmin at full power 44 mph 38 kts 40 mph 35 kts 38 mph 33 kts CG at most forward position airspeeds as CAS Flap position 0 15 40 Vmin at idle 47 mph 41 kts 45 mph 39 kts 44 mph 38 kts Vmin at full power 45 mph 39 kts 43 mph
29. ators manual To change engine oil you have to spin the propeller in operation direction first until you can hear a bubbling noise out of the oil expansion tank Now the engine oil is transferred to the tank and it is possible to drain it completely by opening the drain plug Do not unscrew the drain plug at the bottom of the crank case To refill you need about 0 8 gallons of new engine oil as recommended m Please refer also to the Rotax operators manual u We recommend the use of tank Shell Advance 10W 40 semi synthetic oil 8 Aircraft Ground Handling and Servicing 8 19 Exhaust system servicing The REMOS exhaust system used on the REMOS G 3 600 is manufactured from stainless steel To provide suitable cabin temperature especially in cold climates a cabin heating system is included The muffler is held in place by eight wire springs at the connection to the down pipes These springs are sealed with heat resistant silicon to protect them from cracking When reassembling the exhaust system great care has to be taken to ensure no part of the exhaust system touches other components in the engine compartment No welding should be done to the muffler cabin heater if any cracks are visible the muffler has to be exchanged The exhaust system needs no servicing between regular service intervals but we recommend to check for cracks prior to each flight Please take care about the following steps when reassembling the
30. attached to the wheel fairings indicating the maximum air pressure of each tire Do not exceed this recommended air pressure EREM os G 3 600 63 10 Supplementary Information 10 1 Flight Training Supplement 10 1 1 Introduction 10 1 2 Takeoff 10 1 3 Climbing 10 1 4 Cruise 10 1 5 Stall 10 1 6 Slip 10 1 7 Gliding 10 1 8 Descent 10 1 9 Approach 10 1 10 Touch down EREM os G 3 600 64 10 Supplementary Information 10 1 Flight training supplement 10 1 1 Introduction This chapter should enable you to familiarize yourself with the flight performance and flight characteristics of the REMOS G 3 600 To conduct these instructions you have to refer to the appropriate chapters provided by the POH The following pages describe flight characteristics experienced during various flights configurations and weather conditions e Takeoff e Climbing e Cruise e Stall e Slip e Gliding e Descent e Approach e Touch down This chapter was introduced only as an additional guide to experience the capabilities of the aircraft it is not a substitute to flight school training If you are not yet familiar with the aircraft we strongly recommend to follow these instructions only when accompanied by a skilled flight instructor EREM os G 3 600 65 10 Supplementary Information 10 1 Flight training supplement 10 1 2 Takeoff Takeoff under normal conditions 1 After the preflight check has been carried out extend flaps to 15
31. aution Do not switch off with engine running because serious damage to avionics components could occur Avionics master switch all devices connected to the avionics bus fuse 7 12 on or off 2 Airplane Systems and Description 2 9 Engine control gauges Rotax Flydat The Rotax Flydat provides the following engine gauges Engine speed Exhaust temperature Cylinder head Oil temperature e Engine speed gauge rpm forward cylinders water temperature ARG F C FC Operation hour gauge Exhaust temperature gauge Water temperature gauge a Gn Gl Oil temperature gauge G e Oil pressure gauge ee corre Olt TEMP p PLY dat om Illustration below ROTAX An special placard on the ae esta aa mean panel shows the limits for DURS Ee Teas was Leer OIL PRE rpm oil and water 92 5 morada fat you eat De 3 erat Varad tx erty T yau aoo ndentar parye fe Ma donot wn ba ere temperature oil pressure and exhaust temperature For further information fer to the Rot Operation hours Exhaust temperature Indicates whether left Oil pressure please reter to the Rotax multiply displayed rearward cylinders or right side exhaust Displayed value must be user manual value by 0 1 FIC temp is displayed multiplied by 0 1 RPM 5800 6000 EGT 1600 1650 F CHT 300 320 F OIL T 280 300 F Warning Limit max 72 100 Alert Limit EGT 1600 1650F OIL P nin 29 12 eo REMOS G 3 600 19 2 Airplane Systems and Description
32. ch connected to the fuselage tail by a specially developed mounting frame To release the tow rope a release lever is located on the left hand side of the pilot seat colored yellow Additionally a back view mirror has to be installed at the left wing strut by the use of a specially developed mounting bracket Glider towing operation is only permissible with a 100 hp Rotax 912 UL S engine installed REM os G 3 600 79 10 Supplementary Information 10 2 Towing glider 2 Airplane and Systems Descriptions 2 1 Cockpit Inside the cabin of the REMOS G 3 600 a tow release handle is installed You will find that handle located at the left hand side of the pilot seat colored yellow If the handle is pulled out the tow rope will be disengaged The handle should provide a free play of 1 2 to 1 Inch EREM os G 3 600 80 10 Supplementary Information 10 2 Towing glider 3 Operating Limitations 3 1 Maximum permissible towing speed V7 The airspeed during glider towing operations must not exceed the maximum permissible airspeed of the towed glider The minimum airspeed when towing a glider must not drop below 1 3 x Vs of the towed glider 3 2 Maximum weak link strength e Tow ropes should be a length of at least 165 to 200 ft e A weak link of Q 5 300 daN has to be installed 3 3 Maximum permissible all up weight of the glider to be towed The maximum permissible all up weight of the glider to be towed shall not exceed 1400
33. eel exhaust system Carburetor heating REMOS Airbox Carburetor Battery Voltage regulator Ceramic firewall REMOS engine mount Coolant expansion tank 14 2 Airplane Systems and Descriptions To ensure maximum durability and performance of your Rotax engine it is essential to use the lubricants and maintain the values described in this chapter 21 Engine overview 2 Airplane and Systems Descriptions 2 2 Engine Engine manufacturer ROTAX Engine type 912 ULS Max power at take off 73 6 kW 100 hp permanent 69 9kW 95hp Max rpm at take off 5800 rpm permanent 5500 rpm Max cylinder head temperature 275 F 135 C Max fuel pressure 5 7 psi 0 4 Bar Max oil temperature 266 F 130 C Min oil temperature 120 F 50 C 2 3 Propeller Gearbox Propeller manufacturer F Ili Tonini Sensenich Propeller type no of blades GT 169 5 164 2 blade wood 2A0 R5R70 EN Gearbox manufacturer ROTAX Gearbox ratio Propeller 2 43 1 Clutch yes 2 4 Fuel and fuel capacity Permissible fuel qualities Premium Unleaded Auto Fuel 100 LL Aviation Fuel Useable fuel capacity 21 gallons Total fuel capacity 22 gallons Manufacturer specification till overhaul TBO 1500 hrs Values are subject to change without notice please refer to REMOS G 3 the latest issues of the appropriate manufacturer manuals 15 2 Airplane and Systems Descriptions 2 5 Engine oil coolant
34. einstall the pin after each flight so that the rescue system cannot be activated by mistake 6 4 Operating the rescue system 1 Stop the engine by switching off the ignition 2 Pull out the emergency handle Refer to the BRS operators manual for detailed advisory REMOS G 3 600 E 34 6 Emergency Procedures 6 5 Illustrated rescue system installation Components Emergency handle Connection kevlar bridles to main spar Recovery system rocket Softpack parachute Rubber protection of the eject area akwWNn w w PEMS C3600 35 6 Emergency Procedures 6 6 Engine failure Loss of power before takeoff If any trouble regarding engine power is determined during taxiing or take off run the following procedures shall be applied e Pull throttle lever to idle position e Activate wheel brakes by pushing the brake lever carefully e Stop the engine and determine the problem and remedy or repair as necessary 6 7 Engine failure after takeoff If the engine fails during climbing after takeoff apply the following procedures A Below 500 ft above ground e Push the control stick forward carefully to get into a safe airspeed range e Cut off ignition and close fuel valve e Touch down straight forward or choose a suitable landing field depending on obstacles and pilot experience B More than 500 ft above ground e Push the control stick forward carefully to get into a safe airspeed range e Shut o
35. el 37 8 Luggage 37 4 Total Weight Total Torque The permissible CG range measured from R P must be within 9 6 and 16 3 inch oRemos G 3 600 E 26 4 Weight and Balance Information 45 Calculation example This example shows how to calculate the center of gravity Weight Leverarm Torque Ib Inch Ib Inch Empty weight 670 12 5 8375 Seats 175 8 3 1452 5 Fuel 120 37 8 4536 Luggage 30 37 4 1122 Total weight 995 Total torque 15485 5 CG of the empty weight refer to aircraft specific weight and balance form or see page 29 in this handbook Total Torque Ib Inch Center of Gravity Inch Total Weight Ib 15 56 Inch Calculation example for payload In the examples below the max takeoff weight is 1320 Ib at an empty weight of 670 Ib A Fuel quantity 10 gallons 60 Ib B Fuel quantity 20 gallons 120 Ib Permissible payload 590 Ib Permissible payload 530 Ib ae REMos G 3600 27 4 Weight and Balance Information 4 6 CG Diagram 1320 Ib 1298 Ib 1276 Ib CG in forward position 9 6 Ingh behing R P 1254 Ib 1232 Ib 1210 Ib 1188 Ib 1166 Ib 1144 Ib NOT permitted 1122 Ib CG range 1100 Ib CG in rearward position 16 3 Inch behind R P 1078 Ib 1056 Ib 1034 Ib 1012 Ib 990 Ib 968 Ib 946 Ib 924 Ib Permissible CG rang 902 Ib 880 Ib 858 Ib 836 Ib 814 Ib 792 Ib 770 Ib MTOW 8660 9530 10400 1
36. ff ignition and close fuel valve e Touch down straight forward or make a turn back to the airfield or to a suitable landing field depending on obstacles and pilot experience REMOS G 3 600 E 36 6 Emergency Procedures 6 8 Engine failure in flight If the engine fails during flight check the fuel level first Now try to get the engine started again If the engine does not start again an emergency landing in gliding configuration has to be conducted 6 9 Emergency landing procedure e Determine the wind direction e Search for a possible landing area pay attention to the wind direction e Touch down into the wind if at all possible 6 10 Minimum gliding ratios The following table shows what distances can be flown in gliding configuration engine shut off from different altitudes Flight level in ft 400 800 1000 1500 3000 Distance in NM 1 0 2 0 2 5 4 0 7 5 EREM os G 3 600 37 6 Emergency Procedures 6 11 In flight engine fire procedures e Shut off fuel flow by closing the fuel valve e Push the throttle lever fully forward until engine stops e Try to extinguish the flames by a fast descent carried out as slip e Land as soon as possible 6 12 Emergency landing on water e The final approach has to carried out into the wind e Cut off the ignition and close the fuel valve e Eject the doors e Touch down on the water surface with minimum possible airspeed e Unbuckle and exit the aircraft immediate
37. g and disassembling For assembling and disassembling the wings no additional tools are required except the special tool for attaching and removing the wing and stabilizer bolts This tool is provided with the basic equipment for the aircraft To prepare for assembling the stabilizer place the stabilizer behind the aircraft on an appropriate foam support take care to avoid scratches and dents Remove both stabilizer bolts from their bushes on the stabilizer and place them nearby prepare with grease If you intend to move the aircraft by trailer or to store it with wings folded we recommend using our wing securing aids see illustration on the right With these supports mounted wings are secured properly and the handling of the aircraft will be much easier When the aircraft has to be moved by trailer please ask your authorized REMOS dealer for advice When placed on a trailer in a wrong way serious damage could result EREM os G 3 600 50 8 Aircraft Ground Handling and servicing 8 8 Connecting folded wings to fuselage 1 Withdraw the main wing securing bolt from the wing and place it nearby Ensure that the bolt stays clean till remounted 2 Remove the wing support aid bracket while a second person is supporting the wing at the wing tip 3 Now the second person at the wing tip moves the wing slowly forward while securing that the wing does not spin around its axis The weight of the wing is supported by its strut therefore
38. heck 8 Check propeller for damage and wear the engine oil level correctly 9 Check gear and wheels tires for damage wear and air pressure 10 Check wings and control surfaces for damage 11 Check main bolts struts and stabilizers for damage 12 Check all control surfaces and connections for proper operation 13 Check for free and full travel of all control surfaces 14 Check pitot tube static tubes and hoses for damage and dirt 15 Check fuel level and tank filler cap 16 Check rescue system emergency handle secured 17 Check that both seats are properly secured in position REMOS G 3 600 39 7 Normal Procedures Checks inside the aircraft Close and lock both doors Buckle up Set the parking brake Check for free travel of all control surfaces Check proper functioning of the flap drive and gauge Set oil temperature regulator flap if fitted to take off position Remove rescue system securing pin from emergency handle Open fuel valve 9 NOP OT eo 7 2 Engine starting NEVER start the engine without being in the cabin at the controls with the doors closed and locked Now switch on the master switch the ACL and ensure that the propeller area is clear Starting a cold engine Pull the throttle lever back to the idle position Pull out choke lever Switch on electric fuel pump Turn the key clockwise to the Start position until the engine has started do not hold the key in the Start position for more than
39. in cruise select an airspeed between 80 to 92 mph 70 to 80 kts At these speeds the aircraft will climb between 600 to 800 ft min depending on weather conditions altitude and weight of the aircraft It is strongly recommended to watch oil and water CHT temperatures Under no circumstances should any of the engine temperature limits be exceeded otherwise an engine failures may result Emergency climbing If you have to climb at a maximum angle due to any circumstances we recommend to establish an indicated airspeed of 57 to 63 mph 50 to 55 kts with maximum power setting yellow triangle on the airspeed indicator This will give you the maximum angle of climb at a minimum horizontal speed Watch engine temperatures during the climb REMOS G 3 600 67 10 Supplementary Information 10 1 Flight training supplement 10 1 4 Cruise Normal cruise The maximum continuous cruising speed in level flight and calm weather conditions is 123 to 126 mph 107 to 110 kts To achieve these airspeeds a 75 power setting is required which results in an average fuel consumption of 4 8 to 5 5 gallons per hour Fuel consumption is variable depending on external circumstances like temperature air pressure and payload of the aircraft The most effective economic cruise speed is at an indicated airspeed of 115 mph 100 kts At this speed a fuel consumption of 4 2 gph or less will result giving you a maximum range up to five hours of flight time
40. including Flight Training Supplement Pilot Operating Handbook Important Serial No Year of Construction Call Sign Manufacturer REMOS G 3 600 Pilot Operating Handbook Light Sport Aircraft REMOS G 3 600 with ROTAX 912S Engine The REMOS G 3 600 was manufactured in accordance with the Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements Engine Type Serial No Engine Propeller Type Serial No Propeller REMOS Aircraft GmbH Franzfelde 31 e D 17309 Pasewalk Germany Tel 49 03973 225519 0 Fax 49 03973 225519 99 e mail info remos com Internet www remos com Date Signature Dealer Stamp REMOS G 3 600 02 Remarks and Alterations Applied Modifications Please make a notation below if any changes have been made to this manual or to the plane This manual is an important documentation for pilots in command to ensure a safe operation of the aircraft Therefore it is recommended to keep this Operating Handbook updated with the newest information available You can get the latest upgrades of this manual from your dealer or directly from the manufacturer s homepage Pos Page Description Date Sign REM os G 3 600 03 Remarks and Alterations Applied Modifications continued Pos Page Description Date Sign
41. ind component 20 e Tail wind component 15 to 20 5 4 Take off distance effected by pressure altitude Rotax 912 UL S 100hp 4000 26 00 3500 26 50 3000 27 00 2500 27 50 2000 28 00 1500 28 50 1000 29 00 500 29 50 Pressure alt 645 695 745 795 845 895 945 995 1045 air pressure ft In HG Takeoff distance in feet wind calm over 50 ft obstacle in ICAO standard atmosphere conditions REMOS G 3 600 31 5 Performance 5 5 Cruise speeds RPM fuel consumption and range Rotax 912 UL S 100 hp engine Engine speed Manifold Fuel True Maximum Maximum Pressure Consumption Airspeed Endurance Range rpm InchHG gph at 3000 ft mph kts hr min NM 5300 6 3 138 120 5100 5 5 132 115 3 35 408 5000 4 6 126 110 4 20 473 4800 4 2 120 104 4 45 494 4600 3 7 114 99 5 24 534 4400 3 2 105 91 6 15 568 4200 2 7 98 85 7 25 629 4000 2 4 92 80 8 20 666 All values concerning the 21 gallon fuel tank system 20 gallons usable within the ICAO standard atmosphere EREM os G 3600 32 6 Emergency Procedures This chapter will show you all the procedures which have to be applied in case of an emergency or another dangerous situation You will also get important information regarding the use of the recommended rescue system 6 1 Door emergency eject 1 Unlock the doors by rotating back the door lock handle 2 Unlock the do
42. ithin the ICAO standard atmosphere 7 7 Cruise For continuous operation the engine speed must not exceed 5300 rpm In no case the maximum permissible airspeed VNE of 153 mph 133 kts shall be exceeded Recommended power setting for continuous cruise 4800 to 5000 rpm REMOS G 3 600 43 7 Normal Procedures 7 8 Approach To prepare for approach switch on the electric fuel pump and set the elevator trim to the neutral position and set carburetor heat to warm as necessary When entering final we recommend establishing an airspeed of 60 to 63 mph 52 to 55 kts and extending flaps to the 40 position 7 9 Normal landing The airspeed for touch down should indicate about 40 mph 35 kts with flaps down 40 and 45 mph 39 kts with flaps up 0 The touch down should be first onto the main gear The maximum permissible crosswind component must not exceed 17 mph 15 kts In a headwind component of more than 17 mph 15 kts it is recommended to carry out the landing with a flaps setting of 15 7 10 Short field takeoff To conduct a short field takeoff set flaps to 15 position apply brakes and move the throttle to the full power position Release brakes Proceed as normal takeoff After the aircraft is airborne establish an airspeed of 57 to 63 mph 50 to 55 kts until all obstacles are cleared 7 11 Aborted landing procedure Apply full throttle establish an airspeed of 57 to 63 mph 50 to 55 kts while climbing After
43. lar service intervals do not try to clean the element replace it EREM os G 3 600 58 9 Required Placards and Markings 9 1 Airspeed indicator range and markings Marking Airspeed CAS Description White arc 45 to 81 mph Airspeed range for flaps extended 39 to 71 kts Green arc 49 to 123 mph Normal use 42 to 107 kts Yellow line 98 mph Maximum airspeed for full maneuverability 85 kts Yellow arc 123 to 153 mph Caution in gusty conditions 6G 107 to 133 kts Red line 153 mph Maximum permissible airspeed XX 80 133 kts N ee Yellow triangle 59 mph Recommended airspeed for approach ae 51 kts and best angle of climb Vy Additional placards Calibrated airspeeds related to flight level 128 mph 116 mph REMOS G 3 59 9 Required Placards and Markings 9 2 Operating limitations on instrument panel The following limitation placards are applied to the instrument panel as possible or could be find inside the cabin Airspeed Limitations Maximum permissible airspeed Vne 153 mph 133 kts Max airspeed at high turbulences VB 123 mph 107 kts Maneuvering airspeed Va 98 mph 85 kts Max airspeed flaps extended Vre 81 mph 71 kts RPM 5800 6000 EGT 1600 1650F CHT 300 320 F OIL T 280 300 F Warning Limit o max 72 100 Alert Limi EGT 1600 1650 F OIL P min 29 12 Weights Crew A ae eae The empty weight value has to be completed Empty weight o Capacity 2 Seats individually with each plane
44. lider towing Back view mirror Order No 06 005 G 1 Towing rope with ring connector 1 Weak link 300 daN green 1 Back view mirror Attention The pilot has to ensure that the required weak link is attached to the tow rope Strut mounting bracket otherwise the structure of the aircraft Order No 06 005 H may get overloaded W 7 Tow ropes made of polyamide polyester L1 and polypropylene manufactured to aviation standards may be used if the Left hand side appropriate information is provided and wing strut durable quality is guaranteed Rope connections should be protected by an appropriate cover to prevent wear An appropriate weak link must be provided with the tow rope to protect the towing aircraft against structural overload The rope should not be expanded by more than 30 at maximum permissible workload EREM os G 3600 83 10 Supplementary Information 10 2 Towing glider 5 Performance 51 Takeoff distances Aircraft Type MTOW Minimum Speed for Takeoff Press alt glider speed best climb distance air pressure in Ib mph kts kts ft ft InHG ASK 13 1120 57 50 58 1560 0 29 98 TWIN Astir 1270 69 60 66 1670 0 29 98 DG 1000 1320 72 63 69 1740 0 29 98 Takeoff distances effected by pressure altitude field elevation 4000 26 00 3500 26 50 3000 27 00 2500 27 50 Takeoff weight glider 110p 2000 28 00 1500 28 50 1000 29 00 500 29 50
45. ly after touch down 6 13 Recovery from unintended spin It is generally prohibited to carry out an intentional spin but if an unintended spin has to be recovered please follow the procedures below e Move rudder and control surfaces to neutral position e Apply rudder against spin direction e After spinning stops apply elevator carefully to recover normal flight condition It is most important that in no case you shall try to stop spinning by the use of the ailerons because this will not stop the spin REMOS G 3 600 E 38 7 Normal Procedures This chapter provides you with all the procedures for normal operation of the aircraft including preflight preparations 7 1 Preflight check Before each flight the following checks have to be conducted Checks outside the aircraft Important 1 Before moving the aircraft drain possible water from the fuel tank using to check the oil level it is the drain valve important to turn the propeller a few times in operating 2 Check the engine oil level Begs Smee direction till you can hear some 3 Check level of the engine coolant between min and max marking kind of bubbling noise coming 4 Check proper condition of engine mounting out of the oil expansion tank 5 Check mounting of the exhaust system ie that the eee key as been removed betore 6 Check all water hose connections minate orasele 7 Check that the cowling is closed and properly secured This is the only way to c
46. mple CG diagram Aircraft specific weights Takeoff and landing distances Rate of climb Takeoff distance effected by external circumstances Takeoff distance effected by pressure altitude Cruise speeds RPM fuel consumption and range Table of Contents 6 1 Door emergency eject 33 6 2 Recovering from stall 33 6 3 Rescue system 34 6 4 Operating the rescue system optional equipment 34 6 5 Illustrated rescue system installation 35 6 6 Engine failure Loss of power before takeoff 36 6 7 Engine failure after takeoff 36 6 8 Engine failure in flight 37 6 9 Emergency landing procedure 37 6 10 Minimum gliding ratios 37 6 11 In flight engine fire procedures 38 6 12 Emergency landing on water 38 6 13 Recover from unintended spin 38 7 1 Preflight check 39 7 2 Engine starting 40 7 3 Taxiing 42 7 4 Normal takeoff 42 7 5 Best angle of climb speed Vx 43 7 6 Best rate of climb speed Vy 43 7 7 Cruise 43 7 8 Approach 44 7 9 Normal Landing 44 7 10 Short field takeoff 44 EREM os G 3 600 08 Table of Contents 7 11 Aborted landing procedures 44 7 12 Low airspeed and stall 45 8 Aircraft Ground Handling and Servicing Page 8 1 Servicing fuel oil and coolant 47 8 2 Towing and tie down instructions 47 8 3 100 200 hr service 12 month inspection 48 8 4 300 hr service 49 8 5 Cleaning and care 49 8 6 Folding wing system 50 8 7 Preparation for assembling and disassembling 50 8 8 Connecting folded wings to fuselage 51 8 9 Installing horizontal
47. muffler Stainless steel downpipes Retaining springs with heat resistant silicon coating Aluminum cabin heater shell Stainless steel muffler Remark e Use copper grease on the connections between the down pipes and muffler e Seal each spring mount with heat resistant silicon to protect against cracking REMOS G 3 57 8 Aircraft Ground Handling and Servicing 8 20 Propeller servicing The standard propeller on the REMOS G 3 600 is manufactured by Tonini and is made from composite wood providing a white lacquer finish The propeller does not require any servicing at all However we strongly recommend a visual check for cracks and damage prior to each flight Damage to the lacquer finish may disturb the propeller balance due to the change in humidity of the wooden structure Therefore it is essential to repair any failure of the lacquer finish immediately 8 21 Airbox system and air cleaner element The REMOS air intake system consists of a carburetor heating system in conclusion with a special airbox This system needs no servicing during regular service intervals An air cleaner element is installed at the air intake section of the airbox we recommend the use of K amp N air cleaner elements part RC 1250 circular shape or part 33 2022 rectangular shape depending on the type of airbox installed If it is found that the air cleaner elements efficiency has decreased due to dust or dirt between regu
48. ng provided In no case the aircraft shall be towed by attaching any kind of towing equipment to the nose wheel To tie the aircraft we recommend the use of three ropes left wing right wing and tail Tie down each wing by attaching the rope to the strut bracket top end of each strut In addition you should connect a third rope to the latch on the small tail wheel When necessary a fourth rope can be slid around the propeller gear drive shaft at the nose of the aircraft EREM os G 3 600 47 8 Aircraft Ground Handling and Servicing 8 3 100 200 hr service 12 month inspection The first after sales service has to carried out after 20 hours of flight time Thereafter every 100 hours or at least every 12 months the aircraft has to maintained following the REMOS maintenance checklist Refer to the detailed factory checklist Visually check the outer skin of the aircraft for scratches dents and other damage Change the engine oil about 0 8 gallon and the oil filter element Some operating conditions require more frequent oil and oil filter changes 3 Check for leaks and secure attachment of all hoses tubes and cable connections as well as for possible damage to the hoses tubes and cables and fittings 4 Perform maintenance of the engine per the engine manufacturer s recommendations 5 Visually check the engine mounting frame and the proper and secure attachment and location all other components in the engine compartment 6
49. not require special skills nevertheless if not yet familiar with the aircraft we recommend to do this exercise only when accompanied by a experienced flight instructor for the first time EREM os G 3 600 74 10 Supplementary Information 10 1 Flight training supplement 10 1 10 Touch down Touch down under normal conditions Landing the REMOS G 3 600 is much easier than landing many other aircraft The aircraft has very good low speed characteristics and so is very controllable all the way through the landing phase After a good approach has been conducted the REMOS G 3 600 does not require much action to result with a perfect touch down It is important to establish a safe and stable airspeed during the approach The approach should be made at speeds between 60 70 mph REMOS G 3 600 75 10 Supplementary Information 10 1 Flight training supplement 10 1 10 Touch down Touch down in tailwind conditions Touch down with tailwinds present does not require different procedures to that of normal conditions You have to keep in mind however that landing distances will increase due to a higher ground speed Approach in crosswind conditions Cross winds will not have a big effect to the landing characteristics or the G 3 600 as long as wind speed stays within the maximum permissible speed up to 17 mph 15 kts EREM os G 3 600 76 10 Supplementary Information 10 2 Towing glider Table of Content 1 General Information Page
50. o be paid to keep all temperatures within the permissible range If required to keep temperatures at proper operation levels the throttle may be left at a setting just above the idle position Before descent it may be necessary to retract flaps to establish cruise configuration flaps up 0 otherwise the maximum permissible descent speed of VFEmax 75 mph 65 knots must not exceed Before landing the tow rope has to be released at a safe altitude 150 ft AGL Touch down with the tow rope still connected to the release clutch is not permissible EREM os G 3600 87 10 Supplementary Information 10 2 Towing glider 8 Aircraft Ground Handling and Servicing 8 1 Servicing tow release clutch During regular servicing intervals the tow release clutch has to be cleaned lubricated and checked to assure proper operation A general overhaul of the release clutch has to be conducted after 4 years 4000 towing operations For further information refer to the separate operators manual of the manufacturer REMOS G 3 600 88 10 Supplementary Information 10 2 Towing glider 9 Required Placards and Markings 9 1 Cockpit Inside the cabin of the REMOS G 3 600 the following placards are applied when equipped for towing gliders At the left cockpit panel Near to the tow release handle Tow release 92 Release clutch Outside the aircraft the following placards are applied when the aircraft is equipped for towing gliders
51. or hinges by pushing the securing pin red knob forward Do not throw away this pin 3 Push out the unlocked door by hand 6 2 Recovering from stall Push the control stick forward carefully until the indicated airspeed comes to the normal operation range REMOS G 3 600 33 6 Emergency Procedures 6 3 Rescue system optional equipment The installation of the rescue system shall be carried out complying with the recommendations of the manufacturer To do so the aircraft is already prepared for the installation of an BRS rescue system For maximum safety there are Kevlar bridles used to connect the parachute with the main spar in the wing fuselage section These bridles are built into the fuselage protected from dust and dirt see illustration right They need not to be controlled or serviced access is only possible by destroying the top skin of the fuselage A special steel clamp is used to connect the bridles with the rescue system which has to be inspected to assure that it is fixed securely before each flight Attention Do not make changes or modifications to any part of the rescue system to guarantee safety and proper operation Follow the recommendations published by the manufacturer of your installed system and pay special attention to the maintencance intervals Attention Before each flight please remove the securing pin at the emergency handle of the rescue system so the system is ready for use in case of an emergency R
52. sc brake on each wheel of the main gear A master cylinder mounted between the seats allows a sensitive control of brake performance The brake fluid reservoir is located behind the master cylinder and holds DOT 4 brake fluid NO aircraft brake fluid can be used as its use would cause damage to the rubber seals To check the fluid level unscrew the cover take care brake fluid will cause damage to your clothes as well as injury to your skin The brake pads can be checked visually from beneath the wheel fairings use a pocket light The thickness of both brake pads must be at least 0 08 inch The brake pads wear very slowly i e if the aircraft is used in a flight school the brake pads will not require replacement for about 10 000 touch downs and braking maneuvers on paved surfaces Only new original brake pads can be used when replacing any worn pads Brake pads must be replaced by an authorized and skilled person only ER EMOS G 3 600 54 8 Aircraft Ground Handling and Servicing 8 16 Disassembling and assembling wheels To prepare for disassembling the tires and brakes you have to remove the luggage compartment from inside the cabin To do so unscrew the appropriate fixing screws and remove the luggage compartment 1 Now access to hydraulic pipes is possible so you can remove the two cable ties remove comma fixing the T connector to the bottom of the fuselage 2 After you have hoisted and supported the aircraft and removed the
53. st version of this Handbook from your local dealer or directly from the manufacturer s homepage 1 2 Certification The REMOS G 3 600 complies to the rules of the Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements 1 3 Quick Reference Type Full composite carbon fiber fiberglass aircraft with two seats Design High wing design with struts front mounted engine and propeller traditional stabilizer concept differential ailerons aerodynamically compensated Electrically operated flaps 0 to 40 electric elevator trim three wheel landing gear with steerable nosewheel Fiberglass main gear with hydraulic disc brakes REMOS G 3 600 12 1 General Information The cabin is equipped with two seats side by side and will be entered and exited by doors on the left and right side of the fuselage Design Main components are built in halfshells from composite fiber material which are bonded together carbon fiber Kevlar and glass fiber Engine Rotax 912 ULS Propeller 2 blade fixed pitch wood 2 blade ground adjustable carbon 1 4 Technical Specifications Wingspan Length Height Wing area Wing load Wing width at 1320 Ib maximum takeoff weight 32 3 ft 21 4 ft 5 5 ft 131 0 ft2 10 08 Ib ft2 4 06 ft REMOS G 3 600 13 Components REMOS prop spacer Gearbox including clutch Oil cooler Water cooler REMOS stainless st
54. t parts The use of parts or materials not certified by REMOS aircraft is not permissible 8 13 Main gear servicing The main gear is made from glass fabrics with no metal reinforcements As with the fuselage the main gear requires no regular servicing The hydraulic hoses of the brake system are located within the hollow gear legs A visual check for scratches cracks and tire condition has to be carried out prior to each flight Repair works to the fiberglass main gear must only be conducted by skilled and authorized persons Air pressure within the tires should be maintained at 29 to 34 psi Please also check slip marking on each wheel prior to every flight m __ GRP main gear 4 Wheel axle Air pressure placard Slip marking REMOS G 3 600 53 Brake pad thickness min 0 08 inch 8 Aircraft Ground Handling and Servicing 8 14 Nose gear servicing The nose gear consists of a glass fiber nosewheel fairing by which the wheel axle is carried guided by a steel tube with a spring suspension system and shock absorbing components The nose gear needs no special servicing between regular service intervals A visual check for scratches cracks and tire condition has to be carried out prior to each flight Repair works to the fiberglass nose gear must only be conducted by a skilled and authorized person 8 15 Hydraulic brakes The standard brake system used in the REMOS G 3 600 is a hydraulic system with a di
55. theless if not yet familiar with the aircraft we recommend to do this exercise only when accompanied by a experienced flight instructor for the first time REMOS G 3 600 69 10 Supplementary Information 10 1 Flight training supplement 10 1 6 Slip The slip is a very stable flight condition and is also very easy to perform This maneuver is used to increase aerodynamic drag to enable a high rate of descent Before establishing a slip you have to ensure that the airspeed is within the required limits the maximum permissible indicated airspeed of 86 mph 75 kts VA should not be exceeded and if performing a slip with flaps extended a maximum indicated airspeed of 75 mph 65 kts VFE must be maintained You will achieve the maximum descent rate at an indicated airspeed of 63 mph 55 kts with flaps extended fully Conducting a slip will not require special skills nevertheless if not yet familiar with the aircraft we recommend to do this exercise only when accompanied by an experienced flight instructor for the first time EREM os G 3 600 70 10 Supplementary Information 10 1 Flight training supplement 10 1 7 Gliding The aircraft can glide well with the engine in idle or switched off Best glide ratios are achieved within an indicated airspeed of 63 to 75 mph 55 to 65 kts These speeds will establish a glide ratio between 1 15 to 1 17 with the flaps retracted 0 position 10 1 8 Descent When descending from level flight
56. unallowable attitude of the glider is determined which could cause an uncontrolled flight situation the tow rope has to be disengaged immediately If the glider is located outside an angle of 60 behind the towing aircraft Angle between tow rope and longitudinal axis of the towing aircraft gt 30 the rope has to be disengaged immediately 6 3 Failure of the release clutch If a failure on the release mechanism is determined the final approach has to be carried out maintaining a high rate of descent At touch down the aircraft along with the rope should touch the ground at the same time o Remos G 3 600 86 10 Supplementary Information 10 2 Towing glider 7 Normal Procedures 7 1 Preflight check Check tow release clutch to assure proper function and clean condition 7 2 Takeoff During takeoff special care has to be taken that the climb rate and airspeed are adopted are to the required values of the towed glider Watch your rate of climb immediately after take off do not exceed the gliders climb capability To maintain permissible water and oil temperatures during climb and descent the aircraft must be equipped with an oil temperature regulation flap During climb the operating lever of this flap should be in the open cooler position 7 3 Descent and landing After disengaging the glider and prior to descent it is recommended to close the oil temperature regulation flap position closed warmer Special care has t

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