Emergency Landing To Terrain; Precautionary Landing With Engine Power - Skyleader 200 Pilot Operating Handbook

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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.

Direction - preferably into the wind. In hilly terrain to prioritize landing maneuver into the hill.

Magneto A and B switches - switch "OFF"

Landing gear - using depend on landing area character (time for L.G. openning takes approx. 20 sec.)

Flaps – use as needed

Fuel cock - CLOSE

Fuel pump - switch "OFF"

10. Seat belts - fasten and tighten

11. Radio call - report your situation and location

12. Approach - without any steep turns

After landing:

13. Do not taxi

14. Parking brake - use parking brake "ON" (if landing gear has been openned)

15. Transponder (if has been installed) - STB (Stand-By mode)

16. Toggle switches, Avionics - switch "OFF"

17. Master switch - switch "OFF"

18. Emergency Parachute System (if has been installed) - LOCK

19. Exit the ULL aircraft and seek assistance

A precautionary landing is generally carried out in the case of pilot disorientation, lack of daylight, crew health

issues, no fuel reserve, bad weather conditions, or technical problem.

Autopilot (if has been instaled) - switch "OFF"

Alititude loss during 180° turn is aproximately 460ft

Never change selected landing area at last minute.

Watch selected area during landing maneuvre.

2 333 371 B

KP 2U POH 05/2022

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