2.9
For aircraft with the superseded cover set, install them as follows:
−
Cover assembly, engine air-intake Figure 2 [1]
−
Cover assembly, air intakes (oil cooler, ECS and generator intakes) Figure 2 [7]
−
Cover assembly, exhaust LH and Cover assembly, exhaust RH Figure 2 [2]
−
Cover assembly, AOA sensor LH and Cover assembly, AOA sensor RH Figure 2 [4]
−
Cover assembly, pitot tube Figure 2 [8]
−
Cover assembly, propeller Figure 2 [3]
−
Install the Lock pin emergency exit Figure 2 [6] in the inner handle of the emergency exit
Figure 2 [5].
2.10
Engage the flying controls gust lock in the flight compartment, refer to AMM 12-B-27-70-00-00A-040A-
A.
2.11
Lock the passenger/crew and cargo doors.
2.12
Lock the service door 31AB.
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 5