Pilatus PC-12/47E MSN-1001-UP, Руководство по обслуживанию

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Support equipment
Table 3 Support equipment
Name Identifications/References Qty Reference Remark
Safety clip (circuit breaker hold
open) Part T12-030 As re-
quired
Supplies
Table 4 Supplies
Name Identifications/References Qty Reference Remark
Grease Part P04-028 As re-
quired
Spares
Table 5 Spares
Name Identifications/References Qty Reference Remark
Cotter pin CSN/ISN 32-10-00-03A-015/00A 2 EA
Safety Conditions
None
Procedure
1 General
This procedure is applicable to the left and right main landing gear doors.
2 Removal
2.1 Obey the safety precautions given in AMM 12-B-32-00-00-00A-901B-A.
2.2 Lift the aircraft clear of the ground on jacks, refer to AMM 12-B-07-10-00-00A-901A-A.
2.3 Open and install a Safety clip (circuit breaker hold open) (Pt.No. T12-030) on this circuit breaker:
− LDG GEAR PWR (RH POWER JUNCTION BOX).
2.4 Remove the nut Figure 1 [13], washer Figure 1 [12], bush Figure 1 [9] and bolt Figure 1 [8] and
disconnect the rod Figure 1 [14] from the fitting Figure 1 [10].
2.5 If needed, remove the bush Figure 1 [11].
2.6 Remove and discard the cotter pins Figure 1 [5] and Figure 1 [16].
2.7 Remove the nuts Figure 1 [4] and Figure 1 [17] and washers Figure 1 [3] and Figure 1 [18].
2.8 Disconnect the bonding lead Figure 1 [19] from the bolt Figure 1 [21].
2.9 Hold the main-gear door Figure 1 [6] and remove the bolts Figure 1 [1] and Figure 1 [21]. Remove the
main-gear door Figure 1 [6] from the structure.
2.10 If needed, remove the bushes Figure 1 [2], Figure 1 [7], Figure 1 [15] and Figure 1 [20].
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-32-10-02-00A-920B-A
UNCLASSIFIED 2021-12-04 Page 2