PILOT’S OPERATING HANDBOOK
SECTION 4
NORMAL PROCEDURES
EASA Approved
Edition 0 -- October 31, 2013
Rev. 1
Page 4.4.7
PREFLIGHT INSPECTION (7/9)
4 - L.H. exhaust stub
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Condition / No crack)
Inspect if possible pressure port located inside exhaust stub. A missing port or a cracked port may hinder
correct operation of continuous heating of air inlet lip.
5 - Upper engine cowls
OPEN
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
For the first flight of the day :
-
Oil cap
Closed / Locked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
Engine oil level
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
-
Fuel pipes
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(No leak, deterioration, wear)
6 - Engine cowls
Condition - Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Closed / Locked
7 - Air inlets
-
Main
No crack - Unobsctruted
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Check for no cracks, which are sometimes put in evidence by traces of soot resulting from exhaust
gases.
-
Lateral / upper
Unobstructed
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Lateral air inlets, which supply air conditioning system and oil cooler, are provided with blanking covers. It
is not the case for upper air inlets of RAM AIR system (circular grille located in front of R.H. windshield)
and of vapor cycle cooling system (two rectangular grilles located forward of the circular grille).
8 - Propeller and spinner
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(No nicks, cracks or oil leaks / Attachment)
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.
9 - Nose gear
-
Shock absorber / doors / tire / wheel well
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Without passengers and baggages on board, the unpainted surface of the nose gear shock absorber
tube must be visible about :
-
57 mm (2.22 in) of minimum height with full tanks,
-
63 mm (2.46 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.
10 - R.H. exhaust stub
Checked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Condition / No cracks)
Содержание TBM 900
Страница 349: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 2 7 Figure 7 2 2 2 2 WING FLAPS ...
Страница 385: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 3 Figure 7 4 1 2 2 ROLL ...
Страница 390: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 8 Figure 7 4 3 2 2 ELEVATOR ...
Страница 395: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 13 Figure 7 4 5 2 2 RUDDER ...
Страница 398: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 4 16 INTENTIONALLY LEFT BLANK ...
Страница 410: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 5 12 Figure 7 5 6 PARKING BRAKE ...
Страница 413: ...PILOT S OPERATING HANDBOOK SECTION 7 DESCRIPTION Edition 0 October 31 2013 Rev 1 Page 7 6 3 Figure 7 6 1 2 2 POWERPLANT ...