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

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3 Close Up
Note
If a new wing is installed, do a check of the alignment and symmetry, refer to AMM
12-B-05-50-06-00A-
282A-A .
3.1 Install the Cable tie (Pt.No. P09-008) Figure 7 [3] on the hydraulic pipe Figure 7 [4] between the
hydraulic power pack and the nitrogen tank.
3.2 Remove the caps and install the two forward de-ice pipes Figure 7 [1] and Figure 7 [2] between the
wing and the fuselage.
3.3 Install the left wing tip, refer to AMM 12-B-57-33-00-00A-920A-A.
3.4 Remove the jack and trestle from the right wing.
3.5 Remove the rigging pin Figure 3 [16] from the left aileron bellcrank Figure 3 [13].
3.6 Connect the aircraft batteries:
− Lead acid batteries, refer to AMM 12-B-24-30-07-00A-920A-A
− Ni-Cad batteries, refer to AMM 12-B-24-30-07-00A-920B-A
− Heated Ni-Cad batteries, refer to AMM 12-B-24-30-07-00A-920C-A.
3.7 Do the servicing of the hydraulic system, refer to AMM 12-B-29-00-00-00A-902A-A.
3.8 Do the functional test of the landing gear extension and retraction system, refer to AMM 12-B-32-30-
00-00A-903A-A.
3.9 Bleed the brake system, refer to AMM 12-B-32-40-00-00A-902A-A.
3.10 Do the functional test of the airfoil de-ice system, refer to AMM 12-B-30-10-00-00A-903A-A or 12-B-
30-10-00-00A-903B-A.
3.11 Do the check of the stick pusher system, refer to AMM 12-B-22-20-00-00A-903A-A.
3.12 Do a pitot system leak test, refer to AMM 12-B-34-11-00-00A-903A-A.
3.13 Do the functional test of the flap system, refer to AMM 12-B-27-50-00-00A-903A-A.
3.14 Do the functional test of the ailerons, refer to AMM 12-B-27-10-00-00A-903A-A.
3.15 Lower the aircraft from jacks, refer to AMM 12-B-07-10-00-00A-901A-A.
3.16 Remove the bolts Figure 8 [10], washers Figure 8 [9] and nuts Figure 8 [8] from the two fuselage
jacking points Figure 8 [11]. Put the straps Figure 8 [12] in position on the jack points Figure 8 [11] and
install the four bolts Figure 8 [10], washers Figure 8 [9] and nuts Figure 8 [8].
3.17 Do the test of fuel balancing system, refer to AMM 12-B-28-21-00-00A-903A-A.
3.18 Examine all the fuel and hydraulic pipes, that were removed and disconnected, for leaks. No leaks are
permitted.
3.19 Install the fuel pipe covers Figure 4 [7] with the screws Figure 4 [6] and washers Figure 4 [5] in the left
landing gear compartment.
3.20 Position the electrical cable and secure with the Cable tie (Pt.No. P09-008).
3.21 Connect the electrical connector P148.
3.22 Install the panel 12AB with the screws.
3.23 Do the exterior lights operational test for the landing, navigation, strobe, recognition and red beacon (if
installed), refer to AMM 12-B-33-40-00-00A-903A-A.
3.24 Do the operational test of the probes de-ice system, refer to AMM 12-B-30-30-20-00A-903A-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-57-00-00-00A-720A-A
UNCLASSIFIED 2021-12-04 Page 18