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Remos G-3 /600 Pilot Operating Handbook

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Edition 4 / Rev. 03 USA

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Summary of Contents for Remos G-3 /600

  • Page 1 including Flight Training Supplement Edition 4 / Rev. 03 USA...
  • Page 2 REMOS G-3 /600 - Pilot Operating Handbook Light Sport Aircraft REMOS G-3 /600 with ROTAX 912S Engine. Important: 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.
  • Page 3 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.
  • Page 4 Remarks and Alterations Applied Modifications (continued) Pos. Page Description Date Sign...
  • Page 5 Remarks and Alterations Applied Modifications Pos. Page Description Date Sign...

  • Page 6: Table Of Contents

    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 General Information Page...
  • Page 7 Table of Contents Operating Limitations Page Airspeed limits Crosswind and wind limitations Service ceiling Load factors Prohibited maneuvers Center of gravity range Permissible flight maneuvers Weight and Balance Information Page Installed equipment list Weight and balance form Center of gravity (CG) range and determination CG-calculation CG-calculation example CG-diagram...
  • Page 8 Table of Contents Emergency Procedures Page Door emergency eject Recovering from stall Rescue system Operating the rescue system (optional equipment) Illustrated rescue system installation Engine failure / Loss of power before takeoff Engine failure after takeoff Engine failure in flight Emergency landing procedure 6.10 Minimum gliding ratios...
  • Page 9 Table of Contents Normal Procedures Page 7.11 Aborted landing procedures 7.12 Low airspeed and stall Aircraft Ground Handling and Servicing Page Servicing fuel, oil and coolant Towing and tie-down instructions 100/200 hr service / 12 month inspection 300 hr service Cleaning and care Folding wing system Preparation for assembling and disassembling...
  • Page 10 Table of Contents Required Placards and Markings Page Airspeed indicator range markings Operating limitations on instrument panel Passenger warning No intentional spins Miscellaneous placards and markings Supplementary Information Page 10.1 Flight training supplement 10.2 Towing glider...
  • Page 11 Views The REMOS G-3 /600 is designed as full composite carbon fiber & fiberglass aircraft. You will find detailed information on the following pages. Wingspan 32.3 ft (9800mm) Overall Length 21.4 ft (6470mm)

  • Page 12: General Information Page

    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.

  • Page 13: Technical Specifications

    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).

  • Page 14: Airplane And Systems Descriptions Page

    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. Components Engine overview 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...

  • Page 15: Engine

    Airplane and Systems Descriptions Engine Engine manufacturer: ROTAX Engine type: 912 ULS* Max. power: at take-off: 73.6 kW / 100 hp permanent: 69.9 kW / 95 hp Max. rpm: at take-off: 5800 rpm. permanent: 5500 rpm. Max. cylinder head temperature: 275°F (135°C) Max.

  • Page 16: Engine Oil,Coolant

    Airplane and Systems Descriptions Engine oil,coolant 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) Operating weights and loading Maximum permissible take-off weight (W): 1320 lb...

  • Page 17: Cockpit And Basic Equipment

    Airplane and Systems Descriptions Cockpit and basic equipment Remark: This illustration shows the Instruments and switches basic equipment only. Airspeed indicator Optional throttle Throttle lever Reserved for att. gyro Reserved for GPS Charge indicator light Altimeter Reserved for XPDR Master switch Slip indicator Reserved for radio Ignition key / magneto check...

  • Page 18: Center Panel Controls And Circuit Breakers

    Airplane Systems and Description 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. 3 4 5 6 7 8 Trim control switch Flap control switch.

  • Page 19: Engine Control Gauges (Rotax Flydat)

    Airplane Systems and Description Engine control gauges (Rotax Flydat) The Rotax Flydat provides the following engine gauges: Engine speed Exhaust temperature Cylinder head / Oil temperature Engine speed gauge forward cylinders water temperature ° F/°C ° F/°C ° F/°C Operation hour gauge Exhaust temperature gauge Water temperature gauge Oil temperature gauge...

  • Page 20: Additional Gauges (Basic Equipment)

    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.

  • Page 21: Operating Limitations Page

    Operating Limitations Airspeed limits (all airspeeds at maximum takeoff weight) Mark. Speed Description Never exceed speed 153 mph Airspeed which shall never be 133 kts exceeded. Maximum speed in 137 mph Maximum airspeed at maximum level flight 119 kts continuous power setting. Maneuvering speed 98 mph Maximum airspeed for all...

  • Page 22: Crosswind And Wind Limitations

    Operating Limitations 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 Service ceiling Maximum permissible service ceiling: 15,000 ft Load factors Safe multiple load range:...

  • Page 23: Center Of Gravity Range

    The following maneuvers are permitted: Stall Night VFR flights * Slow controlled figure-eight Turns 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.

  • Page 24: Weight And Balance Information Page

    Weight and Balance Information Installed equipment list To comply with the rules of the Airspeed indicator Light Sport Aircraft Altimeter airworthiness, listed Vertical speed indicator minimum instrumentation and Compass equipment provided Slip indicator standard equipment. RPM gauge (Rotax Flydat) Oil pressure gauge (Rotax Flydat) Oil temperature gauge (Rotax Flydat) CHT gauge (Rotax Flydat) Exhaust gas temperature gauge (Rotax Flydat)

  • Page 25: Center Of Gravity (Cg) Range And Determination

    Weight and Balance Information 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 To get the correct values, it is necessary to put the aircraft on three weighing scales, located on a level surface.

  • Page 26: Cg-Calculation

    Weight and Balance Information CG-calculation The following procedure allows the correct calculation for the center of gravity. Torque (lb-Inch) = Weight (lb) x Leverarm (Inch) Total Torque (lb-Inch) Center of Gravity (Inch) = Total Weight (lb) Weight Leverarm Torque Inch lb-Inch Empty weight ____...

  • Page 27: Cg-Calculation Example

    Weight and Balance Information Calculation example This example shows how to calculate the center of gravity Weight Leverarm Torque Inch lb-Inch Empty weight 12.5* 8375 Seats 1452.5 Fuel 37.8 4536 Luggage 37.4 1122 Total weight: 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 (lb-Inch) Center of Gravity (Inch) = = 15.56 Inch...

  • Page 28: Cg-Diagram

    Weight and Balance Information CG-Diagram 1320 lb CG in forward position 1298 lb (9.6 Inch behind R.P.) 1276 lb 1254 lb 1232 lb 1210 lb 1188 lb 1166 lb NOT permitted 1144 lb CG range CG in rearward position 1122 lb (16.3 Inch behind R.P.) 1100 lb 1078 lb...

  • Page 29: Aircraft Specific Weights

    Weight and Balance Information 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: Maximum take-off weight: Maximum payload:...

  • Page 30: Takeoff And Landing Distances

    Performance Takeoff and landing distances Distance 100 hp engine Takeoff run distance ~ 330 ft Takeoff distance* ~ 730 ft (flaps 0°) Takeoff distance* ~ 660 ft (flaps 15°) Landing distance ~ 850 ft Rate of climb Description 100 hp engine Airspeed for best 63 mph / 55 kts...

  • Page 31: Takeoff Distance Effected By External Circumstances

    Performance 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: High grass + 15 to 20 % Dirty wings / rain drops + 10 to 15 % High air temperatures +5 to 10 %...

  • Page 32: Cruise Speeds, Rpm, Fuel Consumption And Range

    Performance 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 InchHG at 3000 ft, mph / hr : min. 5300 138 / 5100 132 / 3:35 5000...

  • Page 33: Emergency Procedures Page

    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. Door emergency eject Unlock the doors, by rotating back the door lock handle.

  • Page 34: Rescue System

    Emergency Procedures 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.

  • Page 35: Illustrated Rescue System Installation

    Emergency Procedures Illustrated rescue system installation Components Emergency handle Connection kevlar bridles to main spar Recovery system rocket Softpack parachute Rubber protection of the eject area.

  • Page 36: Engine Failure / Loss Of Power Before Takeoff

    Emergency Procedures 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: Pull throttle lever to idle position Activate wheel brakes by pushing the brake lever carefully Stop the engine and determine the problem and remedy or repair as necessary Engine failure after takeoff If the engine fails during climbing after takeoff, apply the following procedures:...

  • Page 37: Engine Failure In Flight

    Emergency Procedures 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. Emergency landing procedure Determine the wind direction Search for a possible landing area - pay attention to the wind direction...

  • Page 38: In-Flight Engine Fire Procedures

    Emergency Procedures In-flight engine fire procedures 6.11 Shut-off fuel flow by closing the fuel valve Push the throttle lever fully forward until engine stops Try to extinguish the flames by a fast descent carried out as slip Land as soon as possible Emergency landing on water 6.12 The final approach has to carried out into the wind...

  • Page 39: Normal Procedures Page

    Normal Procedures This chapter provides you with all the procedures for normal operation of the aircraft including preflight preparations. Preflight check Before each flight the following checks have to be conducted: Important: Checks outside the aircraft Before moving the aircraft: drain possible water from the fuel tank, using to check the oil level, it is important to turn the propeller the drain valve...

  • Page 40: Engine Starting

    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 Engine starting...
  • Page 41 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. Release ignition key, immediately after the engine has started Push the choke lever forward Switch off the electric fuel pump Starting a hot engine: Pull the throttle lever back to the idle position Turn the key clockwise to the "Start"...

  • Page 42: Taxiing

    Normal Procedures 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 brakes, which are operated by a lever on top of the middle section between the seats.

  • Page 43: Best Angle Of Climb Speed (V X )

    Normal Procedures Best angle of climb speed (V 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"...

  • Page 44: Approach

    Normal Procedures 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°...

  • Page 45: Low Airspeed And Stall

    Normal Procedures Low airspeed and stall 7.12 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...
  • Page 46 Normal Procedures Performing a stall in turns CG at most rearward position (airspeeds as CAS) Flap position 0° 15° 40° at idle 45 mph / 39 kts 42 mph / 37 kts 40 mph / 35 kts at full power 44 mph / 38 kts 40 mph /...

  • Page 47: Aircraft Ground Handling And Servicing Page

    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 towing provided. In no...

  • Page 48: 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.

  • Page 49: 300 Hr Service

    Aircraft Ground Handling and Servicing 300 hr service Every 300 hours, the following additional checks/services are required: Exchange brake fluid (DOT 4 - aircraft brake fluid must NEVER be used) 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...

  • Page 50: Folding Wing System

    When the aircraft has to be moved by trailer, please ask your authorized REMOS dealer Wing securing aids for advice. When placed on a trailer in a wrong way, serious damage could result.

  • Page 51: Connecting Folded Wings To Fuselage

    Aircraft Ground Handling and servicing Connecting folded wings to fuselage Withdraw the main wing securing bolt from the wing and place it nearby. Ensure that the bolt stays clean till remounted. Remove the wing support aid bracket while a second person is supporting the wing at the wing tip.

  • Page 52: Installing Horizontal Stabilizer

    Aircraft Ground Handling and Servicing 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.

  • Page 53: Airframe Servicing

    Airframe servicing 8.12 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.

  • Page 54: Nose Gear Servicing

    8.15 min. 0.08 inch The standard brake system used in the REMOS G-3 /600 is a hydraulic system with a disc 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).

  • Page 55: Disassembling And Assembling Wheels

    Aircraft Ground Handling and Servicing Disassembling and assembling wheels 8.16 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).

  • Page 56: Wheels And Tires

    Wheels and tires 8.17 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.

  • Page 57: Exhaust System Servicing

    Aircraft Ground Handling and Servicing Exhaust system servicing 8.19 The REMOS exhaust system used on the REMOS G-3 /600 is manufactured from EGT- stainless steel. To provide suitable cabin probes temperature, especially in cold climates, a cabin heating system is included. The muffler...

  • Page 58: Propeller Servicing

    Aircraft Ground Handling and Servicing Propeller servicing 8.20 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.

  • Page 59: Required Placards And Markings Page

    Required Placards and Markings V NE Airspeed indicator range and markings Marking Airspeed CAS Description V SO 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...

  • Page 60: Operating Limitations On Instrument Panel

    Required Placards and Markings Operating limitations on instrument panel The following limitation placards are applied to the instrument panel as possible or could be find inside the cabin. RPM 5800/6000 EGT 880/900 CHT 150/160 OIL-T 140/150 Airspeed Limitations RPM 5800/6000 EGT 1600/1650˚F CHT 300/320˚F OIL-T 280/300˚F...

  • Page 61: Miscellaneous Placards And Markings

    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!
  • Page 62 Starter "Engage" Avionics Switch "ON" Choke 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.
  • Page 63 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. !ATTENTION! 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.

  • Page 64: Flight Training Supplement

    Supplementary Information 10.1 Flight Training Supplement Page 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...
  • Page 65 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...
  • Page 66 Supplementary Information Flight training supplement 10.1 10.1.2 Takeoff Takeoff under normal conditions After the preflight check has been carried out, extend flaps to 15˚ position Ensure that the elevator trim is in correct position Whenever possible, takeoff directly into wind. The maximum crosswind limitation 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...
  • Page 67 Supplementary Information Flight training supplement 10.1 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.
  • Page 68 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...
  • Page 69 10.1 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.
  • Page 70 Supplementary Information Flight training supplement 10.1 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) (V A ) should not be exceeded and if performing a slip with flaps extended, a maximum indicated airspeed of 75 mph (65 kts) (V FE ) must be maintained.
  • Page 71 Supplementary Information Flight training supplement 10.1 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°...
  • Page 72 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...
  • Page 73 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...
  • Page 74 Supplementary Information Flight training supplement 10.1 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 not require special skills, nevertheless, if not yet familiar with the aircraft we recommend to do this exercise only...
  • Page 75 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...
  • Page 76 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: Towing Glider

    Supplementary Information Towing glider 10.2 Table of Content General Information Page Introduction Certification Quick reference Airplane and Systems Descriptions Page Cockpit Operating Limitations Page Maximum permissible towing speed (V Maximum weak link strength Maximum permissible all up weight of the glider to be towed Weight and Balance Information Page General...
  • Page 78 Supplementary Information Towing glider 10.2 Table of Content Emergency Procedures Page Engine failure Additional procedures Failure of the release clutch Normal Procedures Page Preflight check Takeoff Descent and landing Aircraft Ground Handling and Servicing Page Servicing tow release clutch Required Placards and Markings Page Cockpit Release clutch...

  • Page 79: Introduction

    Quick reference 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.

  • Page 80: Cockpit

    Airplane and Systems Descriptions 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.

  • Page 81: Maximum Permissible Towing Speed (V T )

    We recommend to maintaining 1300 lb 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...

  • Page 82: General

    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.
  • Page 83 10 Supplementary Information Towing glider 10.2 Weight and Balance Information The following equipment is not part of the center of gravity calculation, but necessary for glider towing: Back view mirror: Towing rope with ring connector* Order No. 06-005-G Weak link 300 daN (green) Back view mirror Attention: The pilot has to ensure, that the required...

  • Page 84: Takeoff Distances

    10 Supplementary Information Towing glider 10.2 Performance Takeoff distances Aircraft Type MTOW Minimum Speed for Takeoff Press. alt./ glider speed best climb distance air pressure in lb mph / ft / InHG ASK 13 1120 57 / 1560 0 / 29.98 TWIN Astir 1270 69 /...

  • Page 85: Tested Glider Configuration

    10 Supplementary Information Towing glider 10.2 Performance 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: High grass + 15 to 20 % Dirty wings / rain drops + 10 to 15 % High air temperatures...

  • Page 86: Engine Failure

    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. Additional procedures If an unallowable attitude of the glider is determined which could cause an uncontrolled flight situation, the tow rope has to be disengaged immediately.

  • Page 87: Preflight Check

    10 Supplementary Information Towing glider 10.2 Normal Procedures Preflight check Check tow release clutch to assure proper function and clean condition. 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.

  • Page 88: Servicing Tow Release Clutch

    10 Supplementary Information Towing glider 10.2 Aircraft Ground Handling and Servicing 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.

  • Page 89: Cockpit

    10 Supplementary Information Towing glider 10.2 Required Placards and Markings Cockpit Inside the cabin of the REMOS G-3 /600 the following placards are applied, when equipped for towing gliders. Attention! At the left cockpit panel: Watch your airspeed when glider towing!
  • Page 90 Pilot Operating Handbook REMOS G-3 /600 Edition 4, Rev. 03, 01/07/2008 USA Editor, Layout & Graphics: Hans Fuchs Advice: Josef Sporer (c) REMOS 2000-2007, all rights reserved...

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