Skyleader KP 2U, SL 200, 200 Flight And Maintenance Manual
SL200 FMM 2009-10-21
SL200 FMM 2009-10-21
Production number:
Registration mark:
Category: ULLa
Manufacturer: JIHLAVAN airplanes, s.r.o., Znojemská 826/64, 586 01 Jihlava, Czech Republic, European Union
SL200 FMM 2009-10-21
OWNER – OPERATOR OF THE AIRCRAFT:
Owner of the aircraft: The change of the ownership:
The change of the ownership:The change of the ownership:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
Name:
Address:
Identity number:
Registration mark:
From, To:
SL200 FMM 2009-10-21
CHAPTERS:
1. GENERAL INFORMATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
2. OPERATIONAL LIMITATIONS AND PERFORMANCE. . . . . . . . . . . . . . . . . . 35
3. STANDARD PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
4. OTHER PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
5. EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
Book 1 FLIGHT MANUAL
Book 2 MAINTENANCE MANUAL
1. AIRCRAFT MAINTENANCE REGULATIONS . . . . . . . . . . . . . . . . . . . . . . . 81
2. WINGS AND HORIZONTAL TAIL UNIT DISMANTLING . . . . . . . . . . . . . . . . 91
3. LANDING GEAR DISMANTLING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 99
4. CHANGING FUEL FILTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .104
5. ELECTRIC WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .105
6. MAINTENANCE PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106
SL200 FMM 2009-10-21
CONTENTS:
1. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
1.1. Pro le of the company. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
1.2. Equipment of the airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
1.3. Instrument panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
1.4. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
1.5. Amendments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
1.5.1. Amendments and supplements of the Flight Manual. . . . . . . . . . . . . 20
1.5.2. Amendments list . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
1.6. Abbreviations and de nitions . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
1.7. Basic technical data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.1. Technical description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.2. Aircraft dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
1.7.3. Defl ections of the control surfaces. . . . . . . . . . . . . . . . . . . . . . . . . 24
1.7.4. Fuel tanks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24
1.7.5. Diagram of aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25
1.8. Fluids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
1.8.1. Rotax 912 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
1.8.2. Rotax 914 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28
1.9. Propeller. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29
1.10. Instrument . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29
1.10.1. Operating switches of the left control stick . . . . . . . . . . . . . . . . . . . 29
1.10.2. Landing gear supervisory display . . . . . . . . . . . . . . . . . . . . . . . . . 30
Book 1 FLIGHT MANUAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
SL200 FMM 2009-10-21
1.10.3. Notices in the cockpit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30
2. OPERATIONAL LIMITATIONS AND PERFORMANCE . . . . . . . . . . . . . . . . 35
2.1. Structural regulations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35
2.2. General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35
2.3. Speeds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36
2.4. Take-o and landing distances . . . . . . . . . . . . . . . . . . . . . . . . . . 37
2.5. Climbing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37
2.6. Gliding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
2.7. Flight range. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
2.8. Ceiling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
2.9. Manoeuvres approved. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
2.10. Engine limitations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40
2.10.1. Rotax 912 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40
2.10.2. Rotax 914 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41
2.10.3. Other engines limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42
2.11. Fuel capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42
2.12. Wind and air operational limitations. . . . . . . . . . . . . . . . . . . . . . . 43
2.13. Weights and C-G limits. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44
2.13.1. Weight and Center of Gravity Limits charts . . . . . . . . . . . . . . . . . . . 45
2.14. Load factors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47
2.15. Flight envelope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47
2.16. Type of operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
2.17. Other limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
3. STANDARD PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
3.1. Pre- ight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
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3.2. Aircraft maintenance after each ight . . . . . . . . . . . . . . . . . . . . . . 57
3.3. Procedures after cockpit entering . . . . . . . . . . . . . . . . . . . . . . . . 57
3.4. Starting the engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58
3.5. Engine warm up and engine check . . . . . . . . . . . . . . . . . . . . . . . . 59
3.6. Procedures before taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 59
3.7. Procedures on holding point . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60
3.8. Start line procedures, take-o . . . . . . . . . . . . . . . . . . . . . . . . . . . 61
3.9. Downwind procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61
3.10. Base leg procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
3.11. Procedures on nal approach, landing . . . . . . . . . . . . . . . . . . . . . 62
3.12. Procedures after landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
3.13. Engine shut down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
3.14. Leaving airplane. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
3.15. Check list of standard procedures . . . . . . . . . . . . . . . . . . . . . . . . 63
4. OTHER PROCEDURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
4.1. Procedures for landing gear operation . . . . . . . . . . . . . . . . . . . . . 67
4.1.1. Signaling check before fl ight . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
4.1.2. Landing gear retraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
4.1.3. Landing gear extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
4.2. Indicated conditions of wing aps and LG positions . . . . . . . . . . . . . 69
5. EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.1. Engine failure during rolling . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.2. Engine failure after take-o . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.3. Engine failure during ight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70
5.4. Emergency undercarriage extension. . . . . . . . . . . . . . . . . . . . . . . 72
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5.5. Emergency landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 72
5.6. Belly landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73
5.7. Interrupted landing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73
5.8. Fire - on ground, engine not running. . . . . . . . . . . . . . . . . . . . . . . 73
5.9. Fire - on ground, engine running . . . . . . . . . . . . . . . . . . . . . . . . . 74
5.10. Fire - during ight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74
5.11. Carburettor freezing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
5.12. Engine and propeller vibrations. . . . . . . . . . . . . . . . . . . . . . . . . . 75
5.13. Emergency parachute system usage . . . . . . . . . . . . . . . . . . . . . . . 75
5.14. Check list of emergency procedures . . . . . . . . . . . . . . . . . . . . . . . 76
1. AIRCRAFT MAINTENANCE REGULATIONS . . . . . . . . . . . . . . . . . . . . . . 81
1.1. Periodic maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81
1.1.1. Inspection of control surfaces clearances . . . . . . . . . . . . . . . . . . . . 81
1.1.2. Maximal allowed control clearances. . . . . . . . . . . . . . . . . . . . . . . . 82
1.2. Lubrication of the aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 82
1.3. Accumulator maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 83
1.4. Hydraulic brakes settings and maintenance . . . . . . . . . . . . . . . . . . 84
1.4.1. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.2. Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.3. Refi lling and deaerating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
1.4.4. Adjusting jaw clearances. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85
1.4.5. Brake assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
1.5. Adjusting of control cables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
1.5.1. Changing cable adjusters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 87
Book 2 MAINTENANCE MANUAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79
SL200 FMM 2009-10-21
1.6. The governor recti er circuit breaker . . . . . . . . . . . . . . . . . . . . . . 88
1.7. Locking hook adjusting and checking . . . . . . . . . . . . . . . . . . . . . . 89
2. WINGS AND HORIZONTAL TAIL UNIT DISMANTLING . . . . . . . . . . . . . . . 91
2.1. Removal of cover strip between wing and central section . . . . . . . . . 91
2.2. Removal and replacement of inspection covers. . . . . . . . . . . . . . . . 91
2.3. Removal of seats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
2.4. Disassembly and assembly of outer wings . . . . . . . . . . . . . . . . . . . 92
2.4.1. Disassembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
2.4.2. Mark bolts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 93
2.4.3. Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 94
2.5. Disassembly and assembly of elevators. . . . . . . . . . . . . . . . . . . . . 96
2.6. Disassembly and assembly of stabilizer . . . . . . . . . . . . . . . . . . . . . 97
3. LANDING GEAR DISMANTLING . . . . . . . . . . . . . . . . . . . . . . . . . . . . 99
3.1. Removal of shock absorbers from main undercarriage . . . . . . . . . . . 99
3.2. Disassembly and assembly of main LG shock absorber . . . . . . . . . . . 99
3.3. Disassembly and assembly of main xed LG shock absorber . . . . . . 100
3.4. Front undercarriage shock absorber removal and assembly . . . . . . 101
3.5. Front undercarriage shock absorber disassembly and assembly. . . . 102
4. CHANGING FUEL FILTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .104
5. ELECTRIC WIRING DIAGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .105
6. MAINTENANCE PLAN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106
SL200 FMM 2009-10-21
SL200 FMM 2009-10-21
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200
BOOK 1
FLIGHT MANUAL
SL200 FMM 2009-10-21
SL200 FMM 2009-10-21
Flight Manual SL 200 Book 1
GENERAL INFORMATION1.
Dear Valued Customer!
Kindly accept our congratulations to the purchase of the UL/S-LSA aircraft SKYLEADER, which is a pure result of
our own research & development. Please remember - fl ying with SKYLEADER Aircraft is low-cost, safe and fun!
We believe that SKYLEADER 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.
Team of SKYLEADER Aircraft is constantly looking for your satisfaction across a wide range of attributes such as
performance, product quality, service and repair, technical support, training, delivery and most importantly, your
overall satisfaction with SKYLEADER Aircraft.
Our company sincerely thank all of you who became our clients. Your continued feedback is invaluable to us, and
supports our endless quest in pursuing your Total Satisfaction.
Let us wish You and Your new SKYLEADER Aircraft all the best!
Sincerely,
Team of JIHLAVAN airplanes, s.r.o. („SKYLEADER Aircraft“)
www.skyleader.aero
Flight Manual SL 200 Book 1
SL200 FMM 2009-10-21
Pro le of the company1.1.
The company JIHLAVAN airplanes, s.r.o. was set up in March 2005after
complete takeover of all incorporeal rights and the complete
technology of production of the ultra-light aircraft from its predecessor
company Kappa 77 a.s..
With the usage of workers know-how the company JIHLAVAN airplanes,
s.r.o., presented as SKYLEADER Aircraft, started the production of allmetal UL/S-LSA aircraft under its own trade mark SKYLEADER 150,
SKYLEADER 200 and SKYLEADER 500. The primary goal of the company
was start the serial production and further research & development of
the aircraft.
SKYLEADER Aircraft regularly supplies the market and continues in organizational steps for the enlargement of the
production. With support of the Institute of Aerospace Engineering at the Brno University of Technology, CZ is the
aircraft developed and modernized all the time despite its existing top characteristics. The 3.200 m2 of modern
production area in the company Jihlavan, Inc. off ers developing our activities in the future.
There are established trade contracts with the representatives in Italy, USA, South Africa, Taiwan, Germany, Poland, the
Netherlands, France, Spain, and many other countries. Its products are presented on the international exhibitions in
Friedrichshafen (Germany), Sun ´n Fun and Oshkosh (the USA), Rybnik (Poland), Blois (France), Cielo e Volo, Meeting
di Primavera (Italy) etc.
JIHLAVAN airplanes, s.r.o. developed the fi nal production of WideBody model, which is now available on the market
under trademark SKYLEADER 200 and SKYLEADER 500. It takes the top fl ying qualities and extends the comfort of
crew by enlarging the cockpit on the maximum width along with the keeping of minimal operating costs and maximal
safety.
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Equipment of the airplane1.2.
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Instrument panel1.3.
See separate list: Instrument panel.
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Introduction1.4.
Validity: The Flight Manual is valid exclusively for the plane whose number is on the fi rst page of the manual.
Amendments1.5.
Amendments and supplements of the Flight Manual1.5.1.
All amendments and supplements of the Flight Manual should be done as follows:
a) the manufacturer of UL aircraft sends an operational update with new and revised information to the owner of the
Flight Manual.
b) the holder of the Flight Manual is obliged:
1/ to change the original information with the revised edition, which is marked by the abbreviation „REV“
and the date of the change.
2/ to make a record of receiving the amendment into the amendment list. This list is found in art. B1-1.4.2..
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Amendments list1.5.2.
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Abbreviations and de nitions1.6.
CAS Calibrated airspeed. It is IAS corrected by errors due to instrument and pitot port errors. CAS is equivalent to
the true airspeed at zero level of international standard atmosphere.
IAS Indicated airspeed. It is the reading of the in-built airspeed indicator corrected by the instrument error.
TAS True airspeed. It is the aircraft velocity considering “undisturbed” air.
IFR Instrument fl ight rules.
VFR Visual fl ight rules.
ISA International standard atmosphere.
MAC Mean aerodynamic chord.
VTU Vertical tail unit (fi n with rudder).
HTU Horizontal tail unit (stabilizer with elevator).
VS0 Minimal allowed velocity in landing confi guration.
VS1 Stalling velocity with fl aps up.
VF0 Maximum velocity for fl ap extending and retracting.
VFE Maximum velocity with fl aps fully extended.
VA Designed maneuvering velocity.
VC Velocity of cruising fl ight.
VL0 Maximum velocity for landing gear extending and retracting.
VH Maximal speed of horizontal fl ight.
VNE Never exceed velocity.
RWY Runway
LG Landing gear
EPS Emergency Parachute System
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Flight Manual SL 200 Book 1
Basic technical data1.7.
Technical description1.7.1.
KP 2U (SKYLEADER 200) is an ultralight, two-seater, all-metal, self-contained, low-wing aircraft with side-by-side seats.
Maximal take-off weight of the airplane is 450 kg (992 lb), with Emergency Parachute System MTOW is 472,5 kg (1198
lb). Supporting surfaces are with two spars. They are composed of a rectangular centre-section and a trapezoidal
outer wing with Fowler fl ap. The fuselage is of a semi-monocoque construction. Tail units are self-contained, all metal
with a forward HTU. A three-wheeled undercarriage with a controlled front wheel is retractable or fi xed.
Aircraft dimensions1.7.2.
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Defl ections of the control surfaces1.7.3.
Fuel tanks1.7.4.
Maximum capacity of standard fuel tanks: 2x32 l / 2x8,45 U. S. gal
Maximum capacity of additional fuel tanks: 2x45 l / 2x11,9 U. S. gal
Detailed information about fuel tanks are in chapter B1-2.11.
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Diagram of aircraft1.7.5.
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Fluids1.8.
Rotax 9121.8.1.
For all the fl uids, follow the instructions in the Rotax 912 UL/ULS manual. Operating propellants used by
manufacturer:
Flight Manual SL 200 Book 1
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Rotax 9141.8.2.
For all the fl uids, follow the instructions in the Rotax 914 F/UL Manual. Operating propellants used by manufacturer:
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Propeller1.9.
Detailed data of the propeller is stated in the Propeller Technical Manual.
Type of the propeller is written in the section Equipment of the airplane at the beginning of this manual.
Instrument1.10.
Operating switches of the left control stick1.10.1.
Button on the G1 head could be used for Transceiver or Intercom or stay unused.
Transceiver
Trim – nose down
Trim – nose up
Autopilot disconnect
Intercom
Transceiver
Intercom
G1 head
G5 head
Transceiver
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Landing gear supervisory display1.10.2.
Notices in the cockpit1.10.3.
a) Limitations, restrictions, warnings
Notices are placed on the instrument panel within view of the pilot.
Key:
1. Control light of left gear unlocking – red
2. Control light of front gear unlocking – red
3. Control light of right gear unlocking – red
4. Control light of left gear extending – green
5. Control light of front gear extending – green
6. Control light of right gear extending – green
7. Shining lights check button
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