Skyleader 600 Pilot Operating Handbook
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Skyleader 600 Pilot Operating Handbook

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6 210 229 R
CC-AHB
February / 2018

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Summary of Contents for Skyleader 600

  • Page 1 6 210 229 R CC-AHB February / 2018...
  • Page 3 2 210 229 R Production number: CC-AHB Registration mark: S-LSA Category: Manufacturer: Zall JIHLAVAN airplanes, s.r.o., Znojemská 826/64, 586 01 Jihlava, Czech Republic.
  • Page 4 OWNER – OPERATOR OF THE AIRCRAFT: Owner of the aircraft: The change of the ownership: Name: Name: Address: Address: Identity number: Identity number: Registration mark: Registration mark: From, To: (Dates) From, To (Dates) The change of the ownership: The change of the ownership: Name: Name: Address:...

  • Page 5: Table Of Contents

    CHAPTERS: Pilot Operating Handbook 1. GENERAL INFORMATION........15 2.
  • Page 6 CONTENTS: Pilot Operating Handbook ........13 GENERAL INFORMATION .
  • Page 7 2.4.2. Other engines limitations ......29 2.5. Fuel capacity ........29 2.6.
  • Page 8 3.3.12. High oil pressure ........44 3.3.13.
  • Page 9 4.7.3. Soft field takeoff ........64 4.8.
  • Page 10 DESCRIPTION OF AIRPLANE AND SYSTEMS..... 77 7.1. General......... . 77 7.2.
  • Page 11 8.10. The governor rectifier circuit breaker ..... . 94 8.11. Aircraft maintenance at the end of flying day ....95 ELECTRIC WIRING DIAGRAM .

  • Page 13: Pilot Operating Handbook

    PILOT OPERATING HANDBOOK...

  • Page 15: General Information

    GENERAL INFORMATION Dear Customer! Kindly accept our congratulations to the purchase of the ULL aircraft SKYLEADER, which is a pure result of our own research & development. Please remember - flying with SKYLEADER ULL aircraft is low-cost, safe and fun! We believe that SKYLEADER ULL aircraft will satisfy your needs on more than 100%.

  • Page 16: Profile Of The Company

    The ZALL JIHLAVAN airplanes company has now developed the wide-body fuselage for its SKYLEADER 200 and SKYLEADER 500, and more recently the new SKYLEADER 400 and 600. It extends the comfort of crew by enlarging the cockpit width, without sacrificing the top flying qualities, minimal operating costs or safety. The newest members of the SKYLEADER fleet are GP One, a wide-body carbon composite model, and a new all-metal model, the single-seat SKYLEADER 100.

  • Page 17: Introduction

    1.2. Introduction Validity: The Pilot Operating Handbook is valid exclusively for the plane whose number is on the first page of the manual. 1.3. Amendments 1.3.1. Amendments and supplements of the Pilot Operating Handbook All amendments and supplements of the Pilot Operating Handbook should be done as follows: a) the manufacturer of LSA aircraft sends an operational update with new and revised information to the owner of the Pilot Operating Handbook.

  • Page 18: Amendment List

    1.3.2. Amendment list Change Amendent update Numbers of affected Issue date of the new Date of new pages Number Number pages pages were changed (with and signature)

  • Page 19: Abbreviations And Definitions

    1.4. Abbreviations and definitions Indicated Air Speed is the reading of the in-built airspeed indicator. Calibrated Air Speed is the airspeed after the IAS instrument and pitot port errors have been corrected (CAS is equivalent to the true airspeed at zero level of international standard atmosphere). True Air Speed is the aircraft speed considering “undisturbed”...

  • Page 20: Basic Technical Data

    Basic technical data 1.5.1. Technical description SKYLEADER 600 is a LSA category airplane, two-seater, self-contained, low-wing with side-by-side seats. Main construction of the airplane is metal, consist of duralumin metal sheets. Upper part of a cockpit is made of fibre composite.

  • Page 21: Fuel Tanks

    1.5.3. Fuel tanks Maximum capacity of fuel tanks: 2x60 l / 2x15.85 U. S. gal Detailed information about fuel tanks are in chapter 2.5.

  • Page 22: Diagram Of Aircraft

    1.5.4. Diagram of aircraft...

  • Page 23: Instrument

    1.6. Instrument 1.6.1. Operating switches of the left control stick Button on the G1 head could be used for Transceiver or Intercom or stay unused. G5 head G1 head Intercom “ON”/”OFF” Trim – nose down Trim – nose up Transceiver Autopilot disconnect Transceiver or Intercom...

  • Page 25: Limitations

    LIMITATIONS 2.1. Structural regulations SKYLEADER 600 aircraft, construction, materials and performance correspond with ASTM F2245. 2.2. General Limitations and performances correspond to sea level in International Standard Atmosphere. Main pilot seat: Left / Right Pilot must be familiar with: - Engine Operator’s Manual.

  • Page 26: Pitot System Error

    2.2.1. Pitot System Error IAS [km/h] Cruise Takeoff CAS [km/h] Landing IAS [km/h] Cruise CAS [km/h] IAS [kt] 32,4 37,8 43,2 48,6 54,1 59,5 64,9 70,3 75,7 81,1 86,5 91,9 Cruise 44,9 47,0 49,7 53,0 55,7 58,9 62,7 66,5 70,3 74,6 78,9 83,8...

  • Page 27: Airspeeds

    2.3. Airspeeds Airspeed Abbreviation [km/h] [km/h] [kt] [kt] Never exceed airspeed Design maneuvering speed Max. speed of cruising flight - it can be exceeded in calm air only Maximum flap extended speed Stall speed with flaps retracted Stall speed in landing configuration 2.3.1.

  • Page 28: Engine Limitations

    2.4. Engine limitations 2.4.1. Rotax 912 ULS R 912 ULS Value Specifications stated in this article are not complete. Takeoff RPM 5800 (max 5 minutes) Detailed data of the engine is stated in the engine Operator‘s Manual. Max. RPM 5500 Idle RPM 1400 max: 7 bar (102 psi), min 0.8 bar (12 psi) below 3500 rpm...

  • Page 29: Other Engines Limitations

    2.4.2. Other engines limitations - do not use max. engine power for a prolonged time (max. 5 min) - takeoff is prohibited: - if engine is running unnaturally - if data on engine instruments is not in operating ranges - if you smell exhaust gas odour in the cockpit - if the tank does not have enough fuel 2.5.

  • Page 30: Wind And Air Operational Limitations

    2.6. Wind and air operational limitations Temperatures limitations: °C °F Engine type R912 UL/A/ULS/S Max. ambient temp. for engine start Min. ambient temp. for engine start For more information see the Engine Operator´s manual.

  • Page 31: Load Factors

    2.7. Load factors Max. load factor positive – flaps off + 4,0 Max. load factor negative – flaps off - 2,0 Max. load factor positive – flaps extended + 2,0 2.8. Flight envelope...

  • Page 33: Type Of Operation

    2.9. Type of operation Daytime VFR. Night VFR (operations allowed if operated by an appropriately rated pilot with equipment as required by local regulations). Flights in known icing conditions are prohibited. 2.10. Other limitations • When handling the aircraft on the ground, always use the tow bar •...
  • Page 34 CC-AHB Empty weight 375 kg 826 lb Max. takeoff weight 600 kg 1320 lb Max. baggage weight 30 kg 66 lb Min. pilot weight 60 kg 132 lb 60L/15.9U.S.gal 120L/31.7U.S.gal Max. pilot weight 120 kg 264 lb Never exceed speed...
  • Page 35 Control lights: Controls: Labels under the seat: - BATTERY - CHOKE - parking brake: - VENTILATION - OPEN/CLOSED Switches: - HEATING - OPEN/CLOSED - INTERCOM - EMERGENCY PARACHUTE SYSTEM HANDLE - TRIM - STARTER BUTTON - HEAD LIGHT - FUEL COCK - POS.

  • Page 37: Emergency Procedures

    EMERGENCY PROCEDURES Pilot must be familiar with: - Engine Operator’s Manual. - ELT Instalation and Operation Manual - SkyView Pilot’s User Guide - Autopilot Operator’s Manual - Emergency Parachute System Manual - Propeller Operator’s Manual 3.1. General information This section provides checklists and amplified procedures for coping with various emergencies that may occur. Emergencies caused by aircraft or engine malfunction are extremely rare if proper pre-flight inspections and maintenance are practiced.

  • Page 38: Emergency Procedure Checklists

    3.3. Emergency procedure checklists 3.3.1. Engine failure after Take-off Emergency landings are generally carried out in the case of engine failure (i.e. the engine cannot be re-started) Immediately establish a glide, with airspeed of 100-110 km/h (54-60kt) Flight altitude: - if altitude less than 150 ft AGL - continue straight ahead and land in RWY direction (possibility to change direction to 15 °...

  • Page 39: Precautionary Landing With Engine Power

    Fuel cock - CLOSE Fuel pump - switch “OFF” Seat belts - fasten and tighten 10. Radio call - report your situation and location 11. Approach - without any steep turns After landing: 12. Do not taxi 13. Parking brake - “ON” 14.
  • Page 40 - Fuel pressure - check value - Fuel gauges - check fuel amount - Fuel cock – OPEN the fuel tank with greater fuel quantity - Seat belts - fasten and tighten - Brakes – check function - RWY, area of base leg and finals - clear for descent and landing - Report (Downwind radio call) - Plan the landing maneuvre - Check landing area surface...

  • Page 41: Landing With A Flat Tire

    - Transponder - STB (Stand-By mode) - Toggle switches and avionics – switch “OFF” - Magneto A and B switches – switch “OFF” - Master switch - switch “OFF” - Fuel cock - CLOSE - Emergency Parachute System - LOCK - Exit the aircraft and seek assistance 3.3.4.

  • Page 42: Loss Of Engine Power In Flight

    - try to restart engine according to Art. 3.3.7 - if unsuccessful, perform an Emergency landing to terrain (according to Art. 3.3.2) 3.3.7. In flight engine restart All unnecessary equipment - switch “OFF” Continue according to Art. 4.2 Starting the engine Be prepared for engine failure and Emergency landing to terrain (see Art.

  • Page 43: Electrical Fire - In Flight

    Time necessary to deplete fuel from carburettor system is about 30 sec. Do not attempt to restart the engine after extinguishing fire! 3.3.10. Electrical fire - in flight Toggle switches, Avionics - switch “OFF” Magneto A and B switches – switch “OFF” Master switch - switch “OFF”...

  • Page 44: High Oil Pressure

    Throttle - moderate level to not further raise oil press As engine warms up and the pressure might reduce If oil pressure does not become normal, stop engine. Check oil viscosity - via engine Operator’s manual. In flight The oil pressure may achieve a high value if after an oil line blockage. Apply the following procedure: Throttle - reduce to 50% power Land as soon as possible Be prepared for engine failure and Emergency landing to terrain (see Art.

  • Page 45: Inadvertent Spin Recovery

    • Engine keeps running with ignition off • Knocking under load Oil pressure • Low oil pressure • High oil pressure Oil level • Oil level is increasing Cold engine start • Engine hard to start at low temperature Detailed information about engine Abnormal Operations have been written in engine Operator’s Manual. 3.3.16.

  • Page 46: Engine And/Or Propeller Vibrations

    After 1 – 2 min gradually increase power of the engine to cruising power If you fall to regain engine power, perform an Emergency landing to terrain (see 3.3.2). Aircraft is approved to operate in conditions VFR without creating known icing only In the case of icing on the wing leading edge, the stall speed could be increased.

  • Page 47: Loss Of Flight Control

    - Throttle lever position - Engine noise in the cockpit - Land at the nearest airport 3.3.20. Loss of flight control Lateral (roll) control failure - Use elevator and rudder control for aircraft banking Avoid steep turns – keep less than 15° of bank! Longitudinal (pitch) control failure - Use elevator trim and throttle for aircraft pitch control Avoid abrupt manoeuvres! A longer runway will be need for landing!

  • Page 48: Carbon Monoxide (Co) Poisoning - Signs & Symptoms

    Perform an Emergency landing to terrain (according to Art. 3.3.2) DO NOT USE EMERGENCY PARACHUTE SYSTEM WITH CANOPY OPENNED Close and lock the canopy before takeoff !!! Opening the canopy during the flight may cause pilot injury, upper part of the fuselage damage and rudder (vertical tail unit) destruction.

  • Page 49: Elt Operation (Ak-451-2)

    3.3.24. ELT operation (AK-451-2) The ELT automatically activates during a crash and transmits the standard swept tone. The Green ON lights flashing located on both the ELT Main Unit and the Cockpit. Remote Switch unit and the buzzer sound periodically indicates when the ELT is activated. The ON switch on the Remote Switch Unit allows you to turn on the ELT for testing.

  • Page 50: Emergency Parachute System Usage

    3.3.25. Emergency parachute system usage Fuel cock - “CLOSE” Magneto A and B switches - switch “OFF” both Seat belts - tighten and fasten Pull the hand lever to release the Emergency Parachute System Radio call - May Day, report your situation and location After reaching ground: Master switch - switch “OFF”...

  • Page 51: Autopilot Failure

    3.3.26. Autopilot failure Pilot must be familiar with Skyview Autopilot Operator’s manual Autopilot system - switch “OFF” (there is three ways, to switch OFF autopilot) • AP Servos switch - situated on the instrument pannel • Autopilot disconect button - situated on the pilot’s control stick (see Art. 1.6.1) •...

  • Page 53: Normal Procedures

    NORMAL PROCEDURES 4.1. Pre-flight check Take off the protective coverings. If parked out of hangar unfasten guy ropes, chock the wheels. After rain or if the canopy glass is wet, wipe dry before you open the canopy! The numbered checking points on the drawing refer to the checking procedures described below.. When checking some parts it is necessary to open hatches or inspection covers.
  • Page 54 a) Before entering cockpit (1.) • Seat attachment - Check • Seat belts - Check • Control systems motion - Check f range and free of any binding • Brake function - Check • Master switch - switch “ON” • Engine &...
  • Page 55 b) Engine area (2. 3. 4.) – check the following: Pilot must be familiar with engine Operator’s Manual! • Engine cover - OPEN • Engine equipment - Check • Exhaust equipment - Check • Electric installation - Check • Fuel hoses installation - Check •...
  • Page 56 c) Front landing gear (2. 3. 4.) – check the following: • Tyre pressure - Check • Nose wheel, shock absorber - Check • Tyre surface and tyre position with regard to wheel rim (according to red mark) - Check •...
  • Page 57 f) Ailerons (6. 7. 16. 17.) – check the following: • Skin - Check • Nuts and screws secure - Check • Clearance in aileron installation points - Check • Aileron moves - Check - freely in whole range of deflection...
  • Page 58 g) Flaps (7. 8. 15. 16.) – check the following: Flaps in Takeoff position and check the following: • Skin - Check • Nuts and screws secure - Check • Clearance in flap installation points - Check • Flap control system - Check •...
  • Page 59 i) Fuselage (1. 8. 9. 11. 12. 14. 15. 19.) – check the following: • Fuselage skin - Check • Anti-collision beacon (bottom) - Check • Fibreglass cover (over stabilizator installation points) - Check • Directional control system - Check •...

  • Page 60: After Entering Cockpit

    4.2. After entering cockpit Emergency Parachute System handle - Check if it is locked Adjust seat position, lock seat by locking mechanism LOCK (Canopy lock LED doesn´t shine when canopy is closed and locked) Canopy - Close and Seat belts – fasten and tighten Head sets - put on head, adjust head band and microphone position Control stick –...

  • Page 61: Engine Warm Up And Engine Check

    20. Electrical charging - check function 21. Radio and keys function - Check 22. Trim – Check function, return to neutral position 23. Flaps – Check free motion, retract Electric fuel pump may not be switched “ON” with empty fuel tanks and closed fuel cock! Max.

  • Page 62: Taxiing

    4.5. Taxiing Emergency Parachute System - UNLOCK before start taxy Transponder - SBY mode (Stand-by mode) Release the brakes (remove wheel chocks) Report - use transceiver to make a broadcast call Check brake function and range of directional control when taxiing Adjust speed of taxiing to airfield surface condition and to wind direction / speed Maximum taxy speed is 15 km/h (8 kt) (9 mph) 4.6.

  • Page 63: Takeoff

    20. Toggle switches and avionics – switch “ON” - check 21. Trim - set neutral position 22. Traffic pattern area - clear for entry to RWY 23. Report about to Lineup on RWY (radio call) 24. Release the brakes. 25. Lineup 4.7.

  • Page 64: Soft Field Takeoff

    At speed 50 km/h (30 kt) smoothly p control stick back to lift front wheel. The aircraft will lift-off at 70 km/h (40 Level off aircraft at 3 ft above the ground, until reaching 90 km/h (48 kt) Climb at 110 km/h (60 kt) ; engine speed max. 5800 RPM (for max. 5 min) 10.

  • Page 65: Downwind Procedures

    • 5000 rpm at 27.2 inHG Manifold pressure - 75% max. continuous power • 5500 rpm at full throttle - maximal continuous power Engine and flight instruments - check values EMS-display - check for any error messages regulary Fuel gauges - check fuel amount regularly 4.10.

  • Page 66: Final Approach And Landing

    4.12. Final approach and Landing 4.12.1. Normal landing Airspeed at 100-110 km/h (54-60kt) Brakes – released (make sure) Flaps – takeoff or landing position (according to pilot discretion) Trim – adjust as required to reduce control stick forces RWY – check if it is clear for landing, report (radio call) At 15 ft AGL: Throttle - CLOSE and round out to fly level at 3 ft above RWY Lose speed by smoothly ping back on control stick.

  • Page 67: Balked Landing Procedures

    4.12.4. Balked landing procedures Repeat takeoff from levelling point Recovery from rebound or high flare Takeoff resumed after touching down (Touch and Go) Throttle – max. power Continue to glide Assess length of runway needed for takeoff - Wait for speed to: reach 100-110 km/h (54-60 kt) (62-68 mph) Throttle –...

  • Page 68: Leaving Aircraft

    Avionics - switch “OFF” Toggle switches - switch “OFF” Throttle - CLOSE Magneto A and B switches - switch “OFF” Wait for engine stop. Master switch - switch “OFF” 4.15. Leaving aircraft Magneto A and B switches - switch “OFF” (check) Master switch and toggle switches –...

  • Page 69: Performance

    PERFORMANCE 5.1. Takeoff and landing distances Data are valid for concrete RWY Takeoff Distance 250 m Total distance of takeoff until reaching 15m (50ft) 820 ft 130 m Rolling distance 427 ft Landing Distance 250 m Total distance of landing from 15m (50ft) 825 ft 100 m Run out distance...

  • Page 70: Climbing

    5.2. Climbing Using takeoff power. Rotax 912 ULS 3,9 m/s Climbing 768 fpm At speed 120 km/h (65kt) 5.3. Gliding Gliding velocities when engine idling. Engine mode IDLE STOPPED Optimal speed for gliding 105 km/h (57kt) 105 km/h (57kt) 2.8 m/s 3.0 m/s Sink rate 500 fpm...

  • Page 71: Flight Range

    5.4. Flight range This data are for INFORMATION ONLY! Data are taken for 75% continuous power. Standard FT (120l / 31.7US gal) Distance 1365 km Range 7347 nm 841 mi. Endurance 6.0 + 0.5 hrs Distances are approximated. 5.5. Ceiling Ceiling altitude: 4500m 14764 ft 5.6.

  • Page 73: Equipment List / Weight And Balance

    EQUIPMENT LIST / WEIGHT AND BALANCE 6.1. Weight and Centre of Gravity Limits charts An example of how to use the Weight and Centre of Gravity Limits chart. C-G chart 1 366,87 1 322,77 1 278,68 baggage 1 234,59 pilot front 1 190,50 pilot rear 1 146,40...

  • Page 74: Weights And Loading Distribution

    6.2. Weights and loading distribution If all the limits of the variable load are respected, the C – G is situated in stated limits in all configurations.

  • Page 75: Equipment List

    6.3. Equipment list Engine: ROTAX 912 ULS 6 779 494 Propeller: WOODCOMP SR3000/2WN 18026 Landing gear: FIXED Flight instruments Type Serial number Airspeed indicator Winter 151872 7426 Altimeter Winter W17672 Vertical speed indicator BC-6 2544 Compass CM-13LS 001 12 2005 Flaps control PFC 10 0925/79...
  • Page 76 A3721 CHT temp. sensor No mark No mark Other equipment Type Serial number Battery Forte FG12170 12V/17AH Emergency parachute sys. GRS 6/600, SD S-LSA SOFT B 5479-12-2076-6234, 6234 AVE-WPSTR-20A A12-1205-01048 Position lights AVE-WPSTG-20A A19-1205-01048 AVE-POSW-002 AVVE-1110-00372 Fuel flow meter FT-60...

  • Page 77: Description Of Airplane And Systems

    LSA Repairman maintenance that has received additional task specific training for the function to be performed to perform heavy maintenance on the SKYLEADER 600 as described in the Basic principles for repair and maintenance of the aircraft document..

  • Page 78: Flight Controls

    7.3. Flight controls 7.3.1. Dual controls The aircraft is equipped with a f dual control system and it can be fy controlled from each pilot seat. Pilot -in- command is defined as the left hand pilot seat. The left hand seat provides best access to the main control elements (i.e.

  • Page 80: Elevator And Aileron Control System

    7.3.3. Elevator and Aileron control system Elevator and Aileron surfaces are controlled by combination of p-rods, levers and angle levers system.

  • Page 82: Flap Control System

    7.3.4. Flap control system The Wing Flap Control System controls is handled electrical strut. Movement is carried by the system of gears, levers and torque tubes on flaps.
  • Page 83 The whole complex is designed so that both of the flaps slides simultaneously, therefore it is impossible that the slide will be not on an even keel. Flap effect is compensated by deflection of lift-side trim surface. The lef-side trim surface is automaticaly deflected according to actual flap position.

  • Page 84: Brakes

    7.3.5. Brakes Foot brakes The foot brakes are situated above the rudder pedals. This brakes are used for stop airplane from low speed and for easier turning the airplane on the ground. They cannot be used for permanent braking! You could damage brake. Control the airplane speed with the throttle lever! The brakes are activated by pushing them forward with your big toe.

  • Page 85: Engine

    7.4. Engine Enigne dates: 4-stroke, 4 cylinder horizontaly opposed, spark ignition engine, single central camshaft push rods - OHV Engine type: Rotax 912 ULS Liquid cooled cylinder heads Serial Number: 6 779 494 Ram air cooled cylinders Dry sump forced lubrication Dual breakerless capacitor discharge ignition 2 constant depression carburetors Mechanical fuel pump...

  • Page 86: Propeller

    7.4.2. Propeller Detailed data of the propeller is stated in the Propeller Technical Manual. SR 3000/2WN is a two bladed electrically operated in flight adjustable ULL aircraft propeller of mixed tructure intended for the following engines: • Subaru EA 81, BMW •...

  • Page 87: Instrument Panel

    7.5. Instrument panel Compass Transciever Altimeter Engine speed indicator Airspeed indicator Variometer Dynon EMS Dynon EFIS Propeller control panel Flap position display Socket 12V/10A ELT control Fuse switches Ventilation P ON - handle Intercom switch Position light switch Water temp. indic. Head light switch Oil temp.

  • Page 89: Handling, Service And Maintenance

    8.3. Ground handling The SKYLEADER 600 is a lightweight aircraft, which is easy to handle on the ground. It is preferable to move the aircraft with its special towing handle. The aircraft may be ped carefy from the propeller (by grasping beside the spinner) or pushed from the upper surface of centroplan carefy.

  • Page 90: Towing Instructions

    8.4. Towing instructions The SKYLEADER 600 can accept a Tow Bar connection. The tow bar is attached to two short horizontal pins protruding from the nose landing gear leg. When handling the aircraft on the ground, it is preferable to use the tow bar When the tow bar is attached to the nose landing gear, the aircraft can be easily moved by hand.

  • Page 91: Tie-Down Instructions

    8.6. Tie-down instructions Use the guy eyes on the rear bottom part of fuselage and on the bottom part of wings! 8.7. Servicing of the fluids 8.7.1. Fuel Engine R912ULS MOGAS min. RON 95 (min. AKI 91) European standard EN 228 Super EN 228 Super plus Canadian standard CAN/CGSB-3.5 Quality 3...

  • Page 92: Oil, Coolant, Brake Fluid

    Oil servicing by Operator‘s Manual for all versions of ROTAX engines. It is not stated in this handbook. Cooling liquid servicing by Operator‘s Manual for all versions of ROTAX engines. It is not stated in this handbook. Brake fluid servicing by Maintenance Manual for JA 600. It is not stated in this handbook. 8.8.

  • Page 93: Accumulator Maintenance

    8.9. Accumulator maintenance A non-maintenance gel accumulator 12V/17Ah (or similar) is used in the airplane. With this type of accumulator it is not necessary to check the electrolyte level. The accumulator is placed on the right side of firewall in engine compartment. Charge the battery as required.

  • Page 94: The Governor Rectifier Circuit Breaker

    8.10. The governor rectifier circuit breaker The circuit breaker is instrumental for the protection of the electrical systems of the engine. The circuit breaker will cut out automatically if there is a current overload of these systems. When possible failure is rectified, pushing on the circuit breaker can reconnect the system.

  • Page 95: Aircraft Maintenance At The End Of Flying Day

    8.11. Aircraft maintenance at the end of flying day Wash the plane and the propeller with water without addition of detergents at the end of flying day. It is recommended to use any dish washing detergent or car shampoo for washing the surface behind the exhaust for easier removal of the dirt from the exhaust pipe.

  • Page 97: Electric Wiring Diagram

    ELECTRIC WIRING DIAGRAM See separate list: Electric wiring diagram...

  • Page 99: Maintenance Plan

    MAINTENANCE PLAN See separate list: Maintenance plan.
  • Page 102 NOTES:...

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