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

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3.3 With the passenger/crew door Figure 1 [1] in the open position turn the inner door handle Figure 1 [4]
to the closed position.
3.4 Identify the type of shoot bolt Figure 1 [7] installed, measure the distance from the center of the shoot
bolt to the start of the chamfer. If the distance is 2 mm (0.08 in) new shoot bolts are installed. If the
distance is 3,4 mm (0.13 in) old shoot bolts are installed.
3.5 Replace old shoot bolts (Ref. Figure 1 [7]).
3.6 Measure the length Figure 1 [8] from the end of the shoot bolts Figure 1 [7] to the door Figure 1 [1]
frame (do not measure to the bush around the shoot bolt). The measurements must be between the
limits in Table 6.
Table 6 Shoot Bolt Measurements
Shoot Bolt Shoot Bolt Measurements
Lower Shoot Bolt (nearest to the door
hinge) Between 35,5 and 36,5 mm (1.40 and 1.44 in)
Center Shoot Bolt Between 30,5 and 31,5 mm (1.20 and 1.24 in)
Upper Shoot Bolt Between 26,5 and 27,5 mm (1.04 and 1.08 in)
3.7 If the measurements are not correct, adjust the shoot bolts as follows:
3.7.1 Remove the passenger/crew door trim panels as necessary, refer to AMM 12-B-25-21-03-00A-920A-A
or 12-B-25-22-03-00A-920A-A.
3.7.2 Remove and discard the cotter pin Figure 1 [9] from the shoot bolt Figure 1 [7].
3.7.3 Remove the shoot bolts Figure 1 [7] from the fork ends Figure 1 [11].
3.7.4 Remove the nuts Figure 1 [10], bolts Figure 1 [13] and washers Figure 1 [14] from the fork ends
Figure 1 [11].
3.7.5 Remove the indicators Figure 1 [15] from the covers Figure 1 [16].
3.7.6 Remove the fork ends Figure 1 [11] from the connecting rods Figure 1 [12]. Discard the fork ends
Figure 1 [11].
3.7.7 Position the new fork ends Figure 1 [11] on the connecting rods Figure 1 [12] and loosely install the
bolts Figure 1 [13], washers Figure 1 [14] and nuts Figure 1 [10].
3.7.8 If required, apply a thin layer of Lubricating paste (Pt.No. P04-029) to the new shoot bolts Figure 1 [7].
3.7.9 Install the shoot bolts Figure 1 [7] removed at Step 3.7.3 on the fork ends Figure 1 [11].
3.7.10 Turn the door handle Figure 1 [4] to the closed position.
3.7.11 Adjust the length Figure 1 [8] that the shoot bolts Figure 1 [7] come out of the door Figure 1 [1] to the
limits in Table 6:
3.7.12 Turn the door handle Figure 1 [4] to the open position.
3.7.13 Use a 2 mm drill to drill the cotter pin holes in the fork ends Figure 1 [11] using the hole in the shoot
bolts Figure 1 [7] as a guide. Remove all unwanted material from inside the door Figure 1 [1].
3.7.14 Install a new Cotter pin Figure 1 [9] through the shoot bolts Figure 1 [7] and fork ends Figure 1 [11].
3.7.15 Remove the nuts Figure 1 [10], bolts Figure 1 [13] and washers Figure 1 [14] from the fork ends
Figure 1 [11].
3.7.16 Position the indicator Figure 1 [15] in the cover Figure 1 [16] and on the fork end Figure 1 [11]. Install
the bolts Figure 1 [13], washers Figure 1 [14] and nuts Figure 1 [10].
3.8 Examine the inboard side of the striker plates Figure 1 [5] for signs of touch marks, or monitor the
shoot bolt Figure 1 [7] motion from the inner side of the aircraft when the door is closed. If touch marks
are found, replace the striker plates, refer to 12-B-52-10-07-00A-920B-A.
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-52-10-00-00A-903B-A
UNCLASSIFIED 2021-12-04 Page 4