Flight Manual SL 200 Book 1
h) Main landing gear (8. 15.) – check the following:
- Tire pressure (use a tire pressure gauge)
- Tire surface and tire position with regard to wheel rim
(according to red mark)
- Nuts tightness on wheel axis, attachment points and
the joint connecting folding strut and shock absorber
* / Nuts on wheel axis, attachment points and shock
absorber
- Condition and position of rubber inserts and plates of
shock absorber
- Free passage of wheel between landing gear legs *
- Folding strut bearing against end stop on rear spar *
- Hydraulic hose and brake check – liquid emission
- Position and security of landing gear sensors *
i) Fuselage (1. 8. 9. 11. 12. 14. 15. 19.) – check the following:
- Fuselage facing
- Cable covers, belts and casing of emergency parachute system (if installed)
- Bottom anticollision beacon (functioning correctly)
- Attachment of fi berglass “boot” of fi n
- Cables and cable adjusters of directional control
- VTU guiding lever, its attachment and attachment of tighteners
- End stops of directional control (7th bulkhead)
- Elevator clearance in carrier
- HTU balance beam (6th bulkhead) and its joint
- Elevator pull-rod joint
- Longitudinal end stops
- Angled elevator lever, carriers and its joints (7th bulkhead)
- Pull-rods HTU
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