Remos G-3 /600 Pilot Operating Handbook Download

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EMOS

600

EMOS

600

Weight and Balance Information

4.6

CG-Diagram

Total torque, regarding to the CG calculation (lb-Inch).

MTOW

1320 lb
1298 lb
1276 lb
1254 lb
1232 lb
1210 lb

1188 lb
1166 lb
1144 lb
1122 lb
1100 lb

1078 lb
1056 lb
1034 lb
1012 lb

990 lb
968 lb
946 lb
924 lb
902 lb
880 lb
858 lb
836 lb
814 lb
792 lb
770 lb

8660 9530 10400 11260 12130 13000 13860 14720 15590 16460 17320

CG in rearward position
(16.3 Inch behind R.P.)

Permissible CG range

NOT permitted
CG range

CG in forward position
(9.6 Inch behind R.P.)

Summary of Contents for G-3 /600

Page 1: ...Edition 4 Rev 03 USA including Flight Training Supplement ...

Page 2: ...03973 225519 0 49 03973 225519 99 info remos com www remos com Important Serial No Manufacturer Engine Type Year of Construction Serial No Engine Call Sign Propeller Type Serial No Propeller Date Signature Dealer Stamp 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 REMOS 360...

Page 3: ...lane 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 ...

Page 4: ...REMOS 3600 REMOS 3600 04 Remarks and Alterations Applied Modifications continued Pos Page Description Date Sign ...

Page 5: ...REMOS 3600 REMOS 3600 05 Remarks and Alterations Applied Modifications Pos Page Description Date Sign ...

Page 6: ...aft airworthiness standards Contents General Information Introduction Certification Quick Reference Technical Specifications Airplane and Systems Descriptions Engine overview Engine Propeller Gearbox Fuel and fuel capacity Engine oil coolant Operating weights and loading Cockpit and basic equipment Center panel controls and circuit breakers Engine control gauges Rotax Flydat Additional gauges basi...

Page 7: ...3 4 4 4 5 4 6 4 7 Weight and Balance Information Installed equipment list Weight and balance form Center of gravity CG range and determination CG calculation CG calculation example CG diagram Aircraft specific weights Page 24 24 25 26 27 28 29 5 5 1 5 2 5 3 5 4 5 5 Performance Takeoff and landing distances Rate of climb Takeoff distance effected by external circumstances Takeoff distance effected ...

Page 8: ... takeoff Engine failure after takeoff Engine failure in flight Emergency landing procedure Minimum gliding ratios In flight engine fire procedures Emergency landing on water Recover from unintended spin Page 33 33 34 34 35 36 36 37 37 37 38 38 38 Normal Procedures Preflight check Engine starting Taxiing Normal takeoff Best angle of climb speed VX Best rate of climb speed VY Cruise Approach Normal ...

Page 9: ...n for assembling and disassembling Connecting folded wings to fuselage Installing horizontal stabilizer Final check after assembling Disassembling the aircraft Airframe servicing Main gear servicing Nose gear servicing Hydraulic brakes Disassembling and assembling wheels Wheels and tires Changing engine oil Exhaust system servicing Propeller servicing Airbox system and air cleaner element Page 47 ...

Page 10: ...acards and Markings Airspeed indicator range markings Operating limitations on instrument panel Passenger warning No intentional spins Miscellaneous placards and markings Page 59 60 60 60 61 10 10 1 10 2 Page 64 77 Supplementary Information Flight training supplement Towing glider ...

Page 11: ...ingspan 32 3 ft 9800mm Overall Length 21 4 ft 6470mm Height 5 5 ft 2280mm The REMOS G 3 600 is designed as full composite carbon fiber fiberglass aircraft You will find detailed information on the following pages ...

Page 12: ...ook 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 ...

Page 13: ...8 4 06 ft ft ft ft2 lb ft2 ft Design Engine Propeller 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 Main components are built in halfshells from composite fiber material which are bonded together carbon fiber Kevlar and glass fiber Rotax 912 ULS 2 blade fixed pitch wood 2 blade ground adjustable carbon ...

Page 14: ...ed in this chapter Components REMOS prop spacer Gearbox including clutch Oil cooler Water cooler REMOS stainless steel exhaust system Carburetor heating REMOS Airbox Carburetor Battery Voltage regulator Ceramic firewall REMOS engine mount Coolant expansion tank 1 2 3 4 5 6 7 8 9 10 11 12 13 1 2 3 4 5 6 7 8 8 9 11 12 13 10 Airplane Systems and Descriptions 2 ...

Page 15: ...12 ULS 73 6 kW 100 hp 69 9 kW 95 hp 5800 rpm 5500 rpm 275 F 135 C 5 7 psi 0 4 Bar 266 F 130 C 120 F 50 C Permissible fuel qualities Useable fuel capacity Total fuel capacity Premium Unleaded Auto Fuel 100 LL Aviation Fuel 21 gallons 22 gallons Propeller manufacturer Propeller type no of blades Gearbox manufacturer Gearbox ratio Propeller Clutch F IIi Tonini Sensenich GT 169 5 164 2 blade wood 2A0 ...

Page 16: ...ommended oil Recommended cooling fluid Coolant capacity mixture antifreeze water 1 1 Automobile engine oils 0 75 gallons 2 8 litre Shell Advance 10W 40 semi synthetic BASF Glysantin green 0 65 gallons 2 5 liters Airplane and Systems Descriptions 2 Operating weights and loading 2 6 Maximum permissible take off weight W Minimum useful load WU Maximum empty weight WE Minimum empty weight Minimum flyi...

Page 17: ...peed indicator Compass Flydat refer to page 19 Opt oil cooler flap control 1 2 3 4 5 6 7 8 9 Optional throttle Reserved for GPS Reserved for XPDR Reserved for radio Reserved for Intercom Reserved for Manifoldtemp Fuel quantity gauge Reserved for add gauges Reserved for RS 232 con 10 11 12 13 14 15 16 17 18 Throttle lever Charge indicator light Master switch Ignition key magneto check Avionics mast...

Page 18: ... optional Not used Circuit breakers for master avionics circuits Master switch all electric systems on or off Caution 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 1 2 3 4 5 6 7 8 9 10 11 Airplane Systems and Description 2 1 2 3 4 5 6 7 8 9 10 11 Main Fuses Master ...

Page 19: ...larmgrenze EGT 880 900 EGT 880 900 CHT 150 160 OIL T 140 150 OIL P max 5 0 7 0 min 2 0 0 8 Indicates whether left or right side exhaust temp is displayed Cylinder head water temperature F C Exhaust temperature rearward cylinders F C Operation hours multiply displayed value by 0 1 Engine speed rpm Exhaust temperature forward cylinders F C Oil pressure Displayed value must be multiplied by 0 1 Oil t...

Page 20: ...he 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 For detailed information please refer to the sepearate operators manual Choose between carburetor manifold temperature and outside temperature see left Adjust alert temperature Reset button Choose temper...

Page 21: ...ich shall never be exceeded Maximum airspeed at maximum continuous power setting Maximum airspeed for all permissible maneuvers Airspeed which shall never be exceeded in gusty weather conditions Airspeed which shall never be exceeded in flaps down configuration Minimum permissible airspeed in flaps down configuration Minimum permissible airspeed in flaps up configuration Recommended airspeed for a...

Page 22: ...2 Crosswind and wind limitations This aircraft must be flown under VFR flight conditions only Maximum permissible wind speed at takeoff and landing Headwind Crosswind 15 000 ft 4 g 2 g 28 mph 25 kts 17 mph 15 kts Operating Limitations 3 Flight conditions not permitted IFR flights Aerobatics Tailspin Flights through or within clouds Flights in icing conditions ...

Page 23: ...determine the CG the weight of the aircraft has to determined equipped with all devices ready to fly except fuel and baggage Permissible only with the REMOS Night VFR Kit installed according to Section 16 REMOS G 3 600 Maintenance Manual issued July 1st 2008 Permissible flight maneuvers 2 10 The following maneuvers are permitted Stall Night VFR flights Slow controlled figure eight Turns Maximum an...

Page 24: ... weight and balance form The CG determination shall refer to the valid weight and balance form Airspeed indicator Altimeter Vertical speed indicator Compass Slip indicator RPM gauge Rotax Flydat Oil pressure gauge Rotax Flydat Oil temperature gauge Rotax Flydat CHT gauge Rotax Flydat Exhaust gas temperature gauge Rotax Flydat Electric fuel gauge Position lights ACL Anti Collision Light Master avio...

Page 25: ...efore 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 A check mark R P on the leading edge of the left wing adjacent to the wing root is provided to ease examination that wing main chord is level use a flexible clear tube filled with water as spirit level To get the total weight G you hav...

Page 26: ... must be within 9 6 and 16 3 inch Torque lb Inch Weight lb x Leverarm Inch Empty weight Seats Fuel Luggage Total Weight Leverarm Inch ____ 8 3 37 8 37 4 Total Torque Weight lb ____ ____ ____ ____ ____ Torque lb Inch ____ ____ ____ ____ ____ Center of Gravity Inch Total Torque lb Inch Total Weight lb 4 4 CG calculation Weight and Balance Information 4 ...

Page 27: ...l Luggage Total weight Leverarm Inch 12 5 8 3 37 8 37 4 Total torque Weight lb 670 175 120 30 995 Torque lb Inch 8375 1452 5 4536 1122 15485 5 Center of Gravity Inch 15 56 Inch Total Torque lb Inch Total Weight lb Calculation example for payload In the examples below the max takeoff weight is 1320 lb at an empty weight of 670 lb Fuel quantity 10 gallons Permissible payload A B 60 lb 590 lb Fuel qu...

Page 28: ...1210 lb 1188 lb 1166 lb 1144 lb 1122 lb 1100 lb 1078 lb 1056 lb 1034 lb 1012 lb 990 lb 968 lb 946 lb 924 lb 902 lb 880 lb 858 lb 836 lb 814 lb 792 lb 770 lb 8660 9530 10400 11260 12130 13000 13860 14720 15590 16460 17320 CG in rearward position 16 3 Inch behind R P Permissible CG range NOT permitted CG range NOT permitted CG range CG in forward position 9 6 Inch behind R P ...

Page 29: ...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 Maximum take off weight Center of Gravity CG lb lb lb inches behind R P Maximum payload ...

Page 30: ...es 5 2 Rate of climb Distance 100 hp engine Description 100 hp engine Airspeed for best climbing 63 mph 55 kts 5100 rpm Maximum climb rate 1300 fpm Descent rate at idle 400 fpm Airspeed for best gliding 60 mph 52 kts flaps 15 Takeoff run distance 330 ft Takeoff distance flaps 0 730 ft Takeoff distance flaps 15 660 ft Landing distance 850 ft ...

Page 31: ...0 1000 29 00 500 29 50 645 695 745 795 845 895 945 995 1045 Rotax 912 UL S 100hp Takeoff distance in feet wind calm over 50 ft obstacle in ICAO standard atmosphere conditions Various circumstances have an effect to the takeoff distance of the aircraft The following listing gives you some suggestions about the values High grass Dirty wings rain drops High air temperatures 15 to 20 10 to 15 5 to 10 ...

Page 32: ...ithin the ICAO standard atmosphere Engine speed rpm Fuel Consumption gph Manifold Pressure InchHG True Airspeed at 3000 ft mph kts Maximum Endurance hr min 3 35 4 20 4 45 5 24 6 15 7 25 8 20 Maximum Range NM 408 473 494 534 568 629 666 5300 5100 5000 4800 4600 4400 4200 4000 6 3 5 5 4 6 4 2 3 7 3 2 2 7 2 4 138 120 132 115 126 110 120 104 114 99 105 91 98 85 92 80 Performance 5 ...

Page 33: ... out the unlocked door by hand 1 2 3 6 2 Recovering from stall Push the control stick forward carefully until the indicated airspeed comes to the normal operation range 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 Emergency Proc...

Page 34: ...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 eac...

Page 35: ...ated rescue system installation Components Emergency handle Connection kevlar bridles to main spar Recovery system rocket Softpack parachute Rubber protection of the eject area 1 2 3 4 5 Emergency Procedures 6 35 ...

Page 36: ...ick forward carefully to get into a safe airspeed range Cut off ignition and close fuel valve Touch down straight forward or choose a suitable landing field depending on obstacles and pilot experience B More than 500 ft above ground Push the control stick forward carefully to get into a safe airspeed range Shut off ignition and close fuel valve Touch down straight forward or make a turn back to th...

Page 37: ...as to be conducted 6 10 Minimum gliding ratios The following table shows what distances can be flown in gliding configuration engine shut off from different altitudes 6 9 Emergency landing procedure Determine the wind direction Search for a possible landing area pay attention to the wind direction Touch down into the wind if at all possible Flight level in ft Distance in NM 1 0 400 2 0 800 2 5 100...

Page 38: ...own on the water surface with minimum possible airspeed Unbuckle and exit the aircraft immediately 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 It is most important that in no case you shall try to stop spinning by the use of the ailerons because this ...

Page 39: ...k propeller for damage and wear Check gear and wheels tires for damage wear and air pressure Check wings and control surfaces for damage Check main bolts struts and stabilizers for damage Check all control surfaces and connections for proper operation Check for free and full travel of all control surfaces Check pitot tube static tubes and hoses for damage and dirt Check fuel level and tank filler ...

Page 40: ...r 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 Starting a cold engine 1 2 3 4 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 posi...

Page 41: ...mediately after the engine has started After starting the engine 1 2 3 4 Check oil pressure immediately after the engine has started Adjust engine rpm as required for warm up maximum 2500 rpm Before take off oil and water temperature must reach at least 120 F Switch on avionics master switch and avionics as required Engine rpm and propeller check 1 2 3 4 Set parking brake Adjust engine to 4000 rpm...

Page 42: ...o 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 The minimum engine speed for ta...

Page 43: ...peller 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 within the ICAO standard atmosphere For continuous operation the engine speed must not exceed 5300 rpm In no case the maximum permissible ai...

Page 44: ...d 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 airspee...

Page 45: ...ft to reestablish a safe airspeed Performing a stall from level flight CG at most rearward position airspeeds as CAS Flap position Vmin at idle 42 mph 37 kts Vmin at full power 41 mph 36 kts 0 39 mph 34 kts 38 mph 33 kts 15 38 mph 33 kts 36 mph 31 kts 40 CG at most forward position airspeeds as CAS Flap position Vmin at idle 45 mph 39 kts Vmin at full power 45 mph 39 kts 0 44 mph 38 kts 42 mph 36 ...

Page 46: ... it has to be considered that the stall speed will increase see table above Performing a stall in turns CG at most rearward position airspeeds as CAS Flap position Vmin at idle 45 mph 39 kts Vmin at full power 44 mph 38 kts 0 42 mph 37 kts 40 mph 35 kts 15 40 mph 35 kts 38 mph 33 kts 40 CG at most forward position airspeeds as CAS Flap position Vmin at idle 47 mph 41 kts Vmin at full power 45 mph ...

Page 47: ... the instrument panel Refer to Chapter 2 Airplane and Systems Descriptions for further instructions regarding specifications and capacities 8 1 Servicing fuel oil and coolant 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 towing provided In no case the aircraft shall be towed by attaching any kind o...

Page 48: ...d cables and fittings Perform maintenance of the engine per the engine manufacturer s recommendations Visually check the engine mounting frame and the proper and secure attachment and location all other components in the engine compartment Lubricate wing main bolts and horizontal stabilizer attachment bolts using regular grease Lubricate wings plastic ball joints using regular grease Check all joi...

Page 49: ...ks services are required 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 a...

Page 50: ...t 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 The G 3 60...

Page 51: ...has to be taken that the surface of the wing is not damaged by the fuselage connecting latches 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 If all latches have engaged and the wing fits properly to the fusel...

Page 52: ...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 ...

Page 53: ...nd services may only be conducted using REMOS original replacement parts The use of parts or materials not certified by REMOS aircraft is not permissible 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 cr...

Page 54: ...he 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 authori...

Page 55: ...le ties to disconnect the T connector from the fuselage 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 ...

Page 56: ...anced because badly balanced wheels will create vibrations after takeoff during taxiing and braking 8 18 Changing engine oil also see Rotax operators 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 openi...

Page 57: ... 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 muffler Use co...

Page 58: ...ailure 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 N air cleaner elements part RC 1250 circular s...

Page 59: ...or full maneuverability Caution in gusty conditions Maximum permissible airspeed Recommended airspeed for approach and best angle of climb Vx 45 to 81 mph 39 to 71 kts 49 to 123 mph 42 to 107 kts 98 mph 85 kts 123 to 153 mph 107 to 133 kts 153 mph 133 kts 59 mph 51 kts Description Airspeed CAS Additional placards Calibrated airspeeds related to flight level VNE Flightlevel MSL m Flightlevel MSL ft...

Page 60: ...T 880 900 CHT 150 160 OIL T 140 150 OIL P max 5 0 7 0 min 2 0 0 8 RPM 5800 6000 Warning Limit Alert Limit EGT 1600 1650 F EGT 1600 1650 F CHT 300 320 F OIL T 280 300 F OIL P max 72 100 min 29 12 Airspeed Limitations 153 mph 133 kts 123 mph 107 kts 98 mph 85 kts 81 mph 71 kts Maximum permissible airspeed VNE Max airspeed at high turbulences VB Maneuvering airspeed VA Max airspeed flaps extended VFE...

Page 61: ...ch 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 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 fue...

Page 62: ... 3600 62 Required Placards and Markings 9 Outside the cabin this placard is located by the fuel filler it indicates the recommended fuel qualities approved for the REMOS G 3 600 Refer to the engine operators manual to check for additional fuel types Inside the cabin a starting checklist and related placards are provided as quick reference guide for starting the engine Oil Temp Control Pull Push de...

Page 63: ... create wrong indicator readings The following placard is attached to the wheel fairings indicating the maximum air pressure of each tire Do not exceed this recommended air pressure 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 ATTENTION Before removing wing main bolt disco...

Page 64: ...ary Information 10 10 1 10 1 1 10 1 2 10 1 3 10 1 4 10 1 5 10 1 6 10 1 7 10 1 8 10 1 9 10 1 10 Flight Training Supplement Introduction Takeoff Climbing Cruise Stall Slip Gliding Descent Approach Touch down Page 65 66 67 68 69 70 71 71 72 75 ...

Page 65: ...vided by the POH The following pages describe flight characteristics experienced during various flights configurations and weather conditions Takeoff Climbing Cruise Stall Slip Gliding Descent Approach 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 th...

Page 66: ... for takeoff is 17 mph 15 kts Smoothly apply full throttle fully forward and maintain runway heading As the aircraft accelerates gently pull back on the control stick to elevate the nose slightly until the aircraft becomes airborne 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...

Page 67: ...h 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 Climbing while in cruise If you have to climb at a maximum angle ...

Page 68: ...mption of 4 2 gph or less will result giving you a maximum range up to five hours of flight time 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...

Page 69: ...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 nevertheless i...

Page 70: ...e 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 ye...

Page 71: ...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 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 limi...

Page 72: ...ach 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 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 high...

Page 73: ...ed 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 sh...

Page 74: ...e 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 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 ...

Page 75: ...g 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 ...

Page 76: ...sent 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 ...

Page 77: ... 79 Page 80 10 2 Towing glider 3 3 1 3 2 3 3 Operating Limitations Maximum permissible towing speed VT Maximum weak link strength Maximum permissible all up weight of the glider to be towed Page 81 81 81 4 4 1 4 2 Weight and Balance Information General Equipment Page 82 82 5 5 1 5 2 5 3 Performance Takeoff distances Takeoff distance effected by external circumstances Tested glider configuration Pa...

Page 78: ...entary Information 10 Emergency Procedures Engine failure Additional procedures Failure of the release clutch Normal Procedures Preflight check Takeoff Descent and landing 8 8 1 Aircraft Ground Handling and Servicing Servicing tow release clutch Page 88 9 9 1 9 2 Required Placards and Markings Cockpit Release clutch Page 89 89 ...

Page 79: ...g 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 For the use as a glider towing aircraft the REMOS G 3 600 is equipped with the Tost E85 tow release clutch 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 col...

Page 80: ...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 ...

Page 81: ...der must not drop below 1 3 x VS of the towed glider The maximum permissible all up weight of the glider to be towed shall not exceed 1400 lb We recommend to maintaining 1300 lb as maximum weight of the glider to be towed when operated with the standard fixed pitch propeller Tow ropes should be a length of at least 165 to 200 ft A weak link of Qnom 300 daN has to be installed During glider towing ...

Page 82: ...ve 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 1 1 1 1 1 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 brack...

Page 83: ...ructure of the aircraft may get overloaded Tow ropes made of polyamide polyester and polypropylene manufactured to aviation standards may be used if the appropriate information is provided and 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 s...

Page 84: ...8 66 69 Takeoff distance ft 1560 1670 1740 0 29 98 0 29 98 0 29 98 Takeoff distances effected by pressure altitude field elevation Pressure alt air pressure ft InHG 4000 26 00 3500 26 50 3000 27 00 2500 27 50 2000 28 00 1500 28 50 1000 29 00 500 29 50 1550 1615 1680 1745 1810 1875 1940 2005 2070 2135 2200 Takeoff weight glider 1100 lb Takeoff weight glider 1300 lb Takeoff distance in feet wind cal...

Page 85: ...d and certified by the factory LS 4 Baby III Twin III Hornbach Discus Blanik DG 500 ASK 21 DuoDiscus MiniNimbus Astir CS ASW 24E motorglider High grass Dirty wings rain drops High air temperatures 15 to 20 10 to 15 5 to 10 Nose wind component Tail wind component 20 15 to 20 Various circumstances will have an effect on the takeoff distance of the aircraft The following listing gives you an estimati...

Page 86: ...e and longitudinal axis of the towing aircraft 30 the rope has to be disengaged immediately 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 Operati...

Page 87: ...lation flap During climb the operating lever of this flap should be in the open cooler position After disengaging the glider and prior to descent it is recommended to close the oil temperature regulation flap position closed warmer Special care has to be paid to keep all temperatures within the permissible range If required to keep temperatures at proper operation levels the throttle may be left a...

Page 88: ...ing 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 ...

Page 89: ...llowing placards are applied when equipped for towing gliders 9 2 Release clutch Outside the aircraft the following placards are applied when the aircraft is equipped for towing gliders At the left cockpit panel Attention Watch your airspeed when glider towing Near to the release clutch Attention Weak link maximum 300 daN Near to the tow release handle Tow release ...

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