Preflight Inspection 13 / 15
► Continuing
NOTE
In case of operation from contaminated runways, it is necessary to
carefully examine propeller blades, where traces of abrasion may be
found. Propeller damage may reduce blade life time and degrade
performance. Any propeller damage should be referred to maintenance
personnel.
Nose gear
97 - Shock absorber ........................................................................... Check
98 - Doors ........................................................................................... Check
99 - Tire .............................................................................................. Check
100 - Wheel well ................................................................................... Check
NOTE
Without passengers and baggages on board, the unpainted surface of
the nose gear shock absorber tube must be visible about:
-
57 mm (2.24 in) of minimum height
with full tanks,
-
63 mm (2.48 in) of minimum height
with half tank.
NOTE
Crush or relieve the shock absorber one time or twice before the
inspection to remove possible sticking.
In case of doubt, request a check of the shock absorber pressure.
101 - Right-side exhaust stub ................................................ Condition / No cracks
Right-side wing - V
Additional remarks are identical to those of left-side wing.
102 - Fuel tank drain (two on each wing) ........................................................ Drain
Fuel free of water and contamination
Continue ►
Pilot's Information Manual
Section 4
Normal Procedures
PIM TBM 960 - Edition 0
Rev. 01
Page 4.4.13
PIM - DO NOT USE FOR FLIGHT OPERATIONS
