FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.:P400-006.000 E Page: 4-12 Revision: ---
Date of Issue: 07. October 2008 Agency approved Date of Rev.: --.--.----
3. Propeller-blades VISUAL INSPECTION for damage.
Check condition of blades and spinner.
Movement of blade-tips up to 0.1 in / 3
mm tolerable (jiggle tips slightly).
Movement of pitch-angle up to 2°
tolerable. No unacceptable cracks and
no loose edge-guards. PU-strips must
be existent and without damage,
otherwise replace within 10 operating-
hours after last inspection.
4. Front-drive VISUAL INSPECTION for wear
1. Tire-pressure Main-wheels: 51 ± 1.5 psi /
3.5 ± 0.1 bar
Nose-wheel: 51 ± 3.0 psi /
2. Slip-marks and tread-pattern
3. Brakes CHECK effectiveness of brakes by
pulling the brake levers (pilot-side, and
optionally co-pilot side). There must be
1. Check horizontal-tail-unit for
correct rigging
The forward vertical-
horizontal-tail-unit-flange must be flush
with the leading-edge of the vertical-
stabilizer. The reel of the elevator-
deflection-lever must fit into the bracket
of the vertical stabilizer.
2. Check rudder for correct rigging The lower bolt of the rudder must be
inserted into the correct socket and
must be secured with nut and cotter-
3. Control-surfaces CHECK for mobility and for excessive
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