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

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Table 2 Master Maintenance Plan Task List (Continued from previous page)
Task number Item Name Task Description Interval Data Module Refer-
ence
*55-30/372 Vertical stabilizer
pitch trim actuator fit-
ting and attachment Eddy current inspec-
tion Threshold
32,500 FH /
42,000 LDG
Repeat
12,500 FH /
15,000 LDG 12-B-55-30-02-00A-
353A-A
55-30/420 Vertical stabilizer for-
ward attachment to
Frame 40 Eddy current inspec-
tion Threshold
32,500 FH /
42,000 LDG
Repeat
12,500 FH /
15,000 LDG 12-B-55-30-03-00A-
353A-A
*55-40/373 Rudder Examine Threshold
32,500 FH /
42,000 LDG
Repeat
12,500 FH /
15,000 LDG / 6 Year 12-B-55-40-00-00A-
310A-A
*55-40/377 Rudder hinges Eddy current inspec-
tion Threshold
32,500 FH /
42,000 LDG
Repeat
12,500 FH /
15,000 LDG 12-B-55-40-05-00A-
353A-A
55-40/410 Rudder trim tab Examine Threshold
32,500 FH /
42,000 LDG
Repeat
12,500 FH /
15,000 LDG / 6 Year 12-B-55-40-04-00A-
310A-A
*56-11/12 Cockpit outer side,
DV windows and cab-
in windows Replace If cracked -
*56-11/13 Cockpit inner and
outer side, DV win-
dows and cabin win-
dows Refer to AMM for lim-
itations If chipped, cracked
(only for inner side
windows), crazing,
scratched, bubbles or
delaminated 12-B-56-00-00-00A-
313A-A
*56-11/14 Windshield LH and
RH Replace If cracked in inner
lamination -
*56-11/15 Windshield LH and
RH Only unpressurized
flight is permitted up
to the next scheduled
inspection providing it
does not cause visual
problems. If cracked in outer
lamination -
56-11/200 Windshield LH and
RH Examine 300 FH / 12 Months 12-B-56-00-00-00A-
313A-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-05-40-00-00A-000B-A
UNCLASSIFIED 2021-12-04 Page 45