Pilatus PC-12/47E MSN-1001-UP, Maintenance Manual

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Procedure
1 General
The aircraft can be temporarily parked in a hangar or outside in low wind speeds. If the aircraft is
outside and the wind speeds are high, moor the aircraft, refer to AMM 12-B-10-20-00-00A-901A-A.
If the aircraft is not to be used for a long time, do the storage of the aircraft, refer to AMM 12-B-10-10-
01-00A-901A-A.
2 Parking - Maintenance Practices
Note
Two versions of cover sets are available. The original version supplied with the aircraft is shown in
Fig. 1
. The alternative version is shown in
Fig. 2
.
Note
Before you install or remove covers/pins, make sure that they are serviceable and complete.
Note
If the aircraft is parked in sunlight, the Sun screens (Optional) (Pt.No. T10-005) can be put in position
behind the flight compartment windows to protect the interior from heat and UV damage.
2.1 Put the aircraft on a level surface. If the aircraft is not in a hangar, point the aircraft into the usual wind
direction, refer to AMM 12-B-09-10-00-00A-901A-A.
2.2 Put the parking brake to ON.
2.3 Put the Wheel chocks (Pt.No. T10-010) at the front and the rear of the nose wheel and each main
wheel.
2.4 If the aircraft is parked outside and heavy snowfall is expected, install the Hand towbar/Tail
stand Figure 1 [11] (Figure 2 [9]) to support the rear fuselage.
Note
The towbar/tail stand is stowed in the rear fuselage of the aircraft.
2.5 Ground the aircraft.
2.6 Close the DV window, the passenger/crew door and the cargo door.
Note
Keep the DV window open if the aircraft is parked in a hangar.
2.7 Make sure that all access panels are correctly installed and closed.
2.8 For aircraft with the original cover set delivered with the aircraft, install them as follows:
− Cover, engine air-intake Figure 1 [1]
− Cover, oil-cooler intake LH and Cover, oil-cooler intake RH Figure 1 [2]
− Cover, ECS intake Figure 1 [4]
− Cover, generator intake Figure 1 [3]
− Cover, engine exhaust Figure 1 [5]
− Cover, protective, AOA sensor Figure 1 [7]
− Cover, pitot tube Figure 1 [8]
− Propeller restraint assembly Figure 1 [6]
− Install the Lock pin emergency exit Figure 1 [9] in the inner handle of the emergency exit
Figure 1 [10].
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719,
1721-1999
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All 12-B-10-10-00-00A-901A-A
UNCLASSIFIED 2021-12-04 Page 4