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Skyleader 200 Pilot Operating Handbook

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KP-2U
KP-2U (SKYLEADER 200)
PILOT OPERATING HANDBOOK
2 333 371 B
Production number:
.......................
Registration mark:
ULL
Category:
06 / 2022

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Summary of Contents for Skyleader 200

  • Page 1 KP-2U KP-2U (SKYLEADER 200) PILOT OPERATING HANDBOOK 2 333 371 B Production number: ....... Registration mark: Category: 06 / 2022...
  • Page 3 2 333 371 B 2 333 371 B Production number: Registration mark: Category: Manufacturer: ZALL JIHLAVAN airplanes, s.r.o., Znojemská 826/64, 586 01 Jihlava, Czech Republic. This ULL aircraft is operated at the operator’s own risk. KP 2U POH 05/2022...
  • Page 4 2 333 371 B OWNER – OPERATOR OF THE ULL AIRCRAFT: Owner of the ULL 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:...

  • Page 5: Table Of Contents

    2 333 371 B CHAPTERS: Pilot Operating Handbook 1. GENERAL INFORMATION........15 2.
  • Page 6 2 333 371 B CONTENTS: Pilot Operating Handbook ........11 GENERAL INFORMATION .
  • Page 7 2 333 371 B 2.4.2. Other engines limitations ......29 2.5. Fuel capacity .
  • Page 8 2 333 371 B 3.3.12. Electrical fire in flight ....... . . 44 3.3.13.
  • Page 9 2 333 371 B 4.7.3. Soft field takeoff ........64 4.8.
  • Page 10 2 333 371 B 6.3. Equipment list ........77 DESCRIPTION OF AIRPLANE AND SYSTEMS.
  • Page 11 2 333 371 B 8.7.1. Fuel ..........93 8.7.2.

  • Page 13: Pilot Operating Handbook

    2 333 371 B PILOT OPERATING HANDBOOK KP 2U POH 05/2022...

  • Page 15: General Information

    & 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%. As part of our continuing commitment to responding to your needs, we continuously improve the quality of the products and services we provide to all of our customers.

  • Page 16: Profile Of The Company

    The ZALL JIHLAVAN airplanes company has now developed the wide-body fuselage for its SKYLEAD-ER 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

    2 333 371 B 1.2. Introduction Validity: The Pilot Operating Handbook is valid exclusively for the plane whose number is on the first page of the manual. It is necessary for the crew to be familliar with this Pilot Operating Handbook before the flight! 1.3.

  • Page 18: Amendments List

    2 333 371 B 1.3.2. Amendments list Change Amendent update Numbers of Issue date of the Date of new pages were Number Number affected pages new pages changed (with signature) The holder of the PIlot Operating Handbook fills in thes chart. For instructions see Art 1.3.1 KP 2U POH 05/2022...

  • Page 19: Abbreviations And Definitions

    2 333 371 B 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 KP-2U (SKYLEADER 200) is a ULL category airplane, two-seater, all-metal, self-supported, low-wing ULL aircraft with side-by-side seats. Supporting surfaces are with two spars. They are composed of a rectangular centre-section and a trapezoidal outer wing with Fowler flap. The fuselage is of a semi-monocoque construction. Tail units are self- contained, all metal with a forward HTU.

  • Page 21: Fuel Tanks

    2 333 371 B 24°+-1° Tail unit Ailerons down 16°+-1° HTU span 2.95 m 9 ft 8.1 in deflection I 10°+-2° HTU area 2.28 m 24.54 sq ft Fowler flaps deflection II 35°+-2° VTU area 1.73 m 18.62 sq ft 33°+-3°...

  • Page 22: Diagram Of Ull Aircraft

    2 333 371 B 1.5.4. Diagram of ULL aircraft Dimensions are in milimeters (mm) KP 2U POH 05/2022...

  • Page 23: Instrument

    2 333 371 B 1.6. Instrument 1.6.1. Operating switches of the control sticks G5 head G1 head Trim – nose down Transceiver Trim – nose up Transceiver KP 2U POH 05/2022...

  • Page 25: Limitations

    2 333 371 B LIMITATIONS 2.1. Structural regulations SKYLEADER 200 ULL aircraft, construction, materials and performance correspond with UL-2, LTF-UL 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

    2 333 371 B 2.2.1. Pitot System Error IAS [km/h] Cruise Takeoff CAS [km/h] Landing IAS [km/h] Cruise CAS [km/h] IAS [kt] Cruise Takeoff CAS [kt] Landing IAS [kt] Cruise CAS [kt] KP 2U POH 05/2022...

  • Page 27: Airspeeds

    2 333 371 B 2.3. Airspeeds Airspeed Abbreviation [km/h] [km/h] Never exceed airspeed Design maneuvering speed Rough air speed Max. speed for landing gear extending and retracting Max. flap extended speed Stall speed in landing configuration Stall speed with flaps retracted 2.3.1.

  • Page 28: Engine Limitations

    2 333 371 B 2.4. Engine limitations 2.4.1. Rotax 912ULS Specifications stated in this article are not complete. For more information, see engine Operator‘s Manual. R912ULS Value Takeoff RPM 5800 1/min Max. RPM 5500 1/min Iddle RPM 1400 rpm max: 7 bar (102 psi), min 0.8 bar (12 psi) below 3500 rpm Oil pressure normal: 2.0 - 5.0 bar (29-73 psi) above 3500 rpm min: 50°C (120°F), max 130°C (266°F)

  • Page 29: Other Engines Limitations

    2 333 371 B 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

    2 333 371 B 2.6. Wind and air operational limitations Temperatures limitations: °C Engine type R912ULS Max. ambient temp. for engine start Min. ambient temp. for engine start For more information see the Engine Operator´s manual. KP 2U POH 05/2022...

  • Page 31: Load Factors

    2 333 371 B 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 KP 2U POH 05/2022...

  • Page 33: Type Of Operation

    2 333 371 B 2.9. Type of operation Only non-aerobatic daytime flights under VFR conditions and without known icing conditions are approved. 2.10. Other limitations • When handling the ULL aircraft on the ground, always use the tow bar • Push the ULL aircraft from the centre section of wing preferably or by holding the root part of propeller blades carefully! •...
  • Page 34 2 333 371 B Empty weight 305, 5 Useful load Max. take-off weight 472,5 Max. weight in luggage space Fuel for 30 min. (8 l) 162,0 kg Min. pilot´s weight 25% fuel (20 l) Never exceed speed km/h 152,6 kg Stalling speed with full flaps km/h 50% fuel (40 l)
  • Page 35 2 333 371 B Switches: Control lights: - POSITION LIGHT Charging - LANDING LIGHT Fuel pump - FUEL PUMP Flaps position display - AVIONICS Landing gear position display - MASTER switch - MAGNETOS B - MAGNETOS A - socket: 12 V DC/10 A circuit breaker notations Labels on the back side of canopy (behind the seats): - Headphones:...

  • Page 37: Emergency Procedures

    2 333 371 B EMERGENCY PROCEDURES Procedures must be followed in the order they are given !!! Pilot must be familiar with: - Engine Operator’s Manual. - Transceiver Operator’s Manual - Transponder Pilot’s User Guide - Garmin G5 Operator’s Manual - Emergency Parachute System Manual 3.1.

  • Page 38: Emergency Procedure Checklists

    2 333 371 B 3.3. Emergency procedure checklists 3.3.1. Engine failure after Takeoff 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 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: Emergency Landing To Terrain

    2 333 371 B 3.3.2. Emergency landing to terrain 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 Autopilot (if has been instaled) - switch “OFF” Landing area - consider landing direction, ground surface/slope, wind direction/speed, obstructions/hazards.
  • Page 40 Make an ‘into the wind’ low pass in takeoff configuration at a height of 100 - 200 ft AGL and an airspeed of 100-110 km/h on right side of landing area - check landing surface, estimate altitude of field (x ft) and ‘runway’...

  • Page 41: Belly Landing

    2 333 371 B - Trim – as required to reduce control stick forces - RWY and area of finals – clear for approach - Fine-tune the landing approach FINAL APPROACH - Descend for landing at a shallow angle with increased engine power - Airspeed 100-110 km/h - Flaps - landing position - Trim –...

  • Page 42: Landing With A Flat Tire

    2 333 371 B 3.3.5. Landing with a flat tire Final Approach - Normal During landing, keep damaged wheel above ground as long as possible using opposite aileron deflection Hold landing direction by rudder control or use brakes as needed Be prepared for the ULL aircraft to yaw suddenly after damaged wheel touches the ground.

  • Page 43: Loss Of Engine Power In Flight

    2 333 371 B Move primary landing gear control lever to “DOWN” position (bottom position) – if not already in “DOWN” position Re-circ the landing gear circuit breaker and wait 30 seconds If three red lights or combination of green and red are shinning (for each wheel must shine at least one light) turn the emergency landing gear control lever until three greens are shinning or the mechanical indicator is in correct position Proceed with normal landing (see Art.

  • Page 44: Engine Fire - In Flight

    2 333 371 B Heating (if has been installed) - push in to CLOSE Leave cockpit immediately and extinguish fire (if it is possible) Time necessary to deplete fuel from carburettor system is approx. 30 sec. Do not attempt to restart the engine after extinguishing fire! 3.3.11.

  • Page 45: Loss Of Oil Pressure

    2 333 371 B 3.3.13. Loss of oil pressure On ground Immediately stop the engine and check cause. Check oil system. Check oil quality A maintenance inspection should be carried out In flight Throttle - reduce to minimum necessary for flight Carry out a Precautionary landing with engine power (according to 3.3.3) Be prepared for engine failure and Emergency landing to terrain (see Art.

  • Page 46: Overvoltage

    2 333 371 B 3.3.16. Overvoltage All unnecessary equipment - switch “OFF” Engine RPM - degrase to minimum necessary for flight Voltmeter (if has been installed) - check values If the overvoltage indication persists: Land as soon as possible 3.3.17. Engine trouble shooting All checks in accordance with the engine Maintenance Manual.

  • Page 47: Inadverent Icing Encounter

    2 333 371 B Throttle - CLOSE Control stick - push forward to neutral position Ailerons - neutral position Rudder - full deflection opposite to the sense of rotation (to stop rotation) After rotation stops: Rudder control - neutral position Elevator control - control stick pull gently back to recover from diving Flaps - retract (if there are opened) Throttle - use as required...

  • Page 48: Loss Primary Instruments

    2 333 371 B If vibrations increase, turn off the engine and proceed as Emergency landing to terrain (see Art. 3.3.2). If you fail to recover the engine power or normal flight conditions, land on the nearest airfield (if possible) or depending on the circumstances, perform a Precautionary landing with engine power according to Art.

  • Page 49: Inadvertent Canopy Opening

    2 333 371 B 3.3.23. Throttle linkage failure maximum power setting! In the case of throttle linkage failure, engine goes to the Fuel cock – OPEN the fuel tank with greater fuel quantity (if left-side fuel tank is filled more than 1/2 of fuel capacity, it is necessary to switch fuel cock to the left fuel tank) Establish a climb (max.

  • Page 50: Carbon Monoxide (Co) Poisoning - Signs & Symptoms

    2 333 371 B 3.3.25. Carbon monoxide (CO) poisoning - signs & symptoms • Light-hearted and exuberant or vice versa (lethargy, drowsiness, ataxia, inaccurate) • A greater sense of confidence (paradoxical euphoria) • Rapid heart rate, rapid breathing • Discomfort, moods •...

  • Page 51: Emergency Parachute System Activation

    2 333 371 B 3.3.26. Emergency Parachute System activation Fuel cock - CLOSE Magneto A and B switches – switch “OFF” both Seat belts - tighten and fasten Pull handle to release the Emergency Parachute System Radio call - May Day, report your situation and location After reaching ground: Master switch - switch “OFF”...
  • Page 52 2 333 371 B KP 2U POH 05/2022...

  • Page 53: Normal Procedures

    2 333 371 B 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..
  • Page 54 2 333 371 B a) Before entering cockpit (1.) • Seat attachment - Check • Seat harnesses - Check • Control systems motion - Check full range and free of any binding • Brake function - Check • Landing gear lever - in DOWN position - check •...
  • Page 55 2 333 371 B 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 •...
  • Page 56 2 333 371 B 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 2 333 371 B 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 KP 2U POH 05/2022...
  • Page 58 2 333 371 B g) Flaps (7. 8. 15. 16.) – check the following: • Skin - Check • Nuts and screws secure - Check • Clearance in flap installation points - Check • Flap control system - Check • Rollers free motion (during flap movement) •...
  • Page 59 2 333 371 B 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

    2 333 371 B 4.2. After entering cockpit Emergency Parachute System handle - Check if it is locked Adjust seat position, lock seat by locking mechanism LOCK 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

    2 333 371 B 19. Radio and keys function - Check 20. Trim – Check function, return to neutral position 21. Flaps – Check free motion, retract Electric fuel pump must not be switched “ON” with empty fuel tanks and closed fuel cock! Max.

  • Page 62: Taxiing

    2 333 371 B 4.5. Taxiing Emergency Parachute System - UNLOCK before taxiing Transponder - SBY mode (Stand-by mode) Release the brakes (remove wheel chocks) Report - use transciever 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) 4.6.

  • Page 63: Takeoff

    2 333 371 B 19. Traffic pattern area - clear for entry to RWY 20. Report about to Lineup on RWY (radio call) 21. Release the brakes. 22. Lineup 4.7. Takeoff 4.7.1. Normal takeoff RWY area – clear for takeoff Check time on clock.

  • Page 64: Soft Field Takeoff

    2 333 371 B 10. Flaps retract at altitude 150 ft AGL, than climb at 120 km/h airspeed (at 5500 RPM) 11. Landing gear - UP in altitude 300 ft AGL (max. speed with opened Landing Gear 150 km/h) 12. Engine instruments – check values 13.

  • Page 65: Cruise

    2 333 371 B 4.10. Cruise Set ULL aircraft to horizontal flight Trim - as required to reduce control stick forces Fuel pump - switch “OFF” Fuel pressure - check value Throttle and propeller angle - set as required • 4300 rpm at 26.3 inHG Manifold pressure •...

  • Page 66: On Base Leg

    2 333 371 B 4.12. On Base leg Airspeed 100-110 km/h Flaps – set to takeoff position Trim – as required to reduce control stick forces RWY and area of finals – clear for approach - Check Plan the landing maneuvre 4.13.

  • Page 67: Soft Field Landing

    2 333 371 B Maintain direction with rudder control. Reduce speed by holding the nose high with elevator control. Brakes - use brake adequately 4.13.3. Soft field landing Final approach - Normal, but: • Touch-down at the lowest practicable speed and hold the nose wheel above the ground as long as possible (by means of the elevator control).

  • Page 68: Engine Shut Down

    2 333 371 B 4.15. Engine shut down Normally the cooling down of the engine during descenting and taxiing will be sufficient to allow the engine to be shut off as soon as the ULL aircraft has stopped. At increased operating temperatures cool down the engine at least minimum of 2 minutes. Engine instruments - check values Avionics - switch “OFF”...

  • Page 69: Cold Start Procedure

    2 333 371 B 4.17. Cold start procedure With throttle closed and choke activated (NOTE: an open throttle makes starting carb ineffective). Be aware, there is no spark below a crankshaft speed of 220 rpm (prop. speed of 90 rpm). As performance of electric starter is greatly reduced when hot, limit cranking to periods not much longer than 1 sec.

  • Page 71: Performance

    2 333 371 B PERFORMANCE 5.1. Takeoff and landing distances All performances depend on ULL aircraft actual Data are valid for concrete RWY takeoff weight and actual weather conditions. Takeoff Distance 250 m Total distance of takeoff until reaching 15m (50ft) 820 ft 130 m Rolling distance...

  • Page 72: Climbing

    2 333 371 B 5.2. Climbing Using takeoff power. Engine mode IDLE STOPPED Optimal speed for gliding 90 km/h 100 km/h 2.0 m/s 3.8 m/s Sink rate 400 fpm 750 fpm Max. velocity with flaps fully extended 100 km/h Engine mode STOPPED 460 ft After 180°...

  • Page 73: Flight Range

    2 333 371 B 5.4. Flight range This data are for INFORMATION ONLY! Data are taken for 75% continuous power. Standard FT (2x40 l ) Distance 746 km Range 403 nm 463 mi. Endurance 3,8 + 0.5 hrs 5.5. Ceiling Ceiling altitude: 4500m 14764 ft 5.6.

  • Page 75: Equipment List / Weight And Balance

    2 333 371 B 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 position (%MAC)= (EW*X + (P*500) + (F*330) + (B*1150) CGLE) -74,7 * 0,0785...

  • Page 76: Weights And Loading Distribution

    2 333 371 B 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. KP 2U POH 05/2022...

  • Page 77: Equipment List

    Airspeed indicator 16-312-260 C4819 Altimeter BG-3E 3814 Vertical speed indicator 8-310-20 A7781 Compass CM-13 CM13210320 Slip ball QM-II EFIS - Garmin G5 011-03809-00 4JQ059094 Landing gear supervisory display PGC 201 2105/23 Flaps control electronics PFC 200 2105/27 KP 2U POH 05/2022...
  • Page 78 2 333 371 B Engine instruments Type Serial number Engine speed indicator IF61.2B35.2301 99G2108/021363 Oil pressure indicator IE.61.2B35.2201 99C2202/022672 Coolant temperature indicator IH91.2B35.22 99B2218/022639 Oil temperature indicator IH61.2B35.2201 99B2217/022651 Fuel pressure indicator IE71.2B35.2201 99G2115/021357 Manifold pressure indicator UMA 7-100-10 C6951 Fuel gauges VDO A2C3833100001 11038,11040...
  • Page 79 2 333 371 B Other equipment Type Serial number Accumulator GWL POWER LP12V20AHB Emergency parachute sys. 5/560 SOFT B1 8705-22-6779-10326 Strobe-LAWT2 0045 Position lights Pos.Light-Red-LART2 0079 Pos.Light-Green-LAGT2 0079 KP 2U POH 05/2022...

  • Page 81: Description Of Airplane And Systems

    Repairman maintenance that has received additional task specific training for the function to be performed to perform heavy maintenance on the SKYLEADER 200 as described in the Basic principles for repair and maintenance of the ULL aircraft document..

  • Page 82: Flight Controls

    2 333 371 B 7.3. Flight controls 7.3.1. Dual controls The ULL aircraft is equipped with a full dual control system and it can be fully 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 83: Elevator And Aileron Control System

    2 333 371 B 7.3.3. Elevator and Aileron control system Elevator surfaces are controlled by combination of pull-rods, levers and angle levers system. 7.3.4. Aileron control system Aileron surfaces are controlled by combination of pull-rods, levers and angle levers system. KP 2U POH 05/2022...

  • Page 84: Flap Control System

    2 333 371 B 7.3.5. 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. 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.

  • Page 85: Brakes

    2 333 371 B 7.3.6. Brakes Hand brake The hand brake lever is situated on the pilot’s control stick. This brakes are used for stop airplane from low speed and for securing the ULL aircraft against move. They cannot be used for permanent braking! It cause brake damage. Control the airplane speed with the throttle lever! The brakes are activated by pushing the brake lever to yourself.

  • Page 86: Landing Gear Supervisory Control

    2 333 371 B 7.3.7. Landing gear supervisory control The undercarriage control lever is situated on central part of the instrument panel and is used for landing gear opening and retracting. Actual position of landing gear shows landing gear supervisory display, whitch is situated next to landing gear control lever (on the instrument panel).

  • Page 87: Seat Position Setting

    2 333 371 B 7.3.8. Seat position setting • Pull forward a lock button and move the seat to selected position • Push back a lock button to fix a seat position • Check if seat position is secured correctly Move Seat Lock button...

  • Page 88: Engine

    2 333 371 B 7.4. Engine Enigne dates: 4-stroke, 4 cylinder horizontaly opposed, spark ignition engine, single central camshaft pull rods - OHV Liquid cooled cylinder heads Ram air cooled cylinders Engine type: Rotax 912ULS2 Dry sump forced lubrication Serial Number: 9 143 976 Dual breakerless capacitor discharge ignition 2 constant depression carburetors Mechanical fuel pump...

  • Page 89: Propeller

    2 333 371 B 7.4.2. Propeller Detailed data of the propeller is stated in the Propeller Technical Manual. E-PROPS DURANDAL DUR-3-170-C4-T is a three bladed ULL aircraft propeller of carbone construction. Type DUR-3-170-C4-T Serial number 148809,148810,148811 Number of Blades Outer diameter of propeller 1700 mm Adjustable on ground...

  • Page 90: Instrument Panel Scheme

    2 333 371 B 7.5. Instrument panel scheme Emergency Parachute System handle Transciever Transponder Charging LED Fuel pump LED Engine speed ind. Slip ball Manifold pressure ind. Altimeter Oil pressure ind. Airspeed ind. Oil temperature ind. Trim position ind. Coolant temp. ind. Vertical speed ind.

  • Page 91: Handling, Service And Maintenance

    8.3. Ground handling The SKYLEADER 200 is a lightweight ULL aircraft, which is easy to handle on the ground. It is preferable to move the ULL aircraft with its special towing handle. The ULL aircraft may be pulled carefully from the propeller (by grasping beside the spinner) or pushed from the upper surface of centroplan carefully.

  • Page 92: Towing Instructions

    8.4. Towing instructions The SKYLEADER 200 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 ULL aircraft on the ground, it is preferable to use the tow bar When the tow bar is attached to the nose landing gear, the ULL aircraft can be easily moved by hand.

  • Page 93: Tie-Down Instructions

    2 333 371 B 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 912ULS MOGAS min. RON 95 (min. AKI 91) European standard EN 228 Super EN 228 Super plus...

  • Page 94: 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 SKYLEADER 200. It is not stated in this handbook. 8.8.

  • Page 95: Accumulator Maintenance

    2 333 371 B 8.9. Accumulator maintenance A non-maintenance gel accumulator 12V/20Ah (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 96: The Governor Rectifier Circuit Breaker

    2 333 371 B 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 97: Ull Aircraft Maintenance At The End Of Flying Day

    2 333 371 B 8.11. ULL 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 99: Electric Wiring Diagram

    2 333 371 B ELECTRIC WIRING DIAGRAM See separate list: Electric wiring diagram KP 2U POH 05/2022...

  • Page 101: Maintenance Plan

    2 333 371 B MAINTENANCE PLAN See separate list: Maintenance plan. KP 2U POH 05/2022...
  • Page 103 2 333 371 B NOTES: KP 2U POH 05/2022...
  • Page 104 2 333 371 B NOTES: KP 2U POH 05/2022...
  • Page 105 2 333 371 B NOTES: KP 2U POH 05/2022...
  • Page 106 2 333 371 B NOTES: KP 2U POH 05/2022...

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