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

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Procedure
1 General
This data module is referenced from the AMM Airworthiness Limitations data module 12-B-04-00-00-
00A-000A-A.
2 Inspections
Do these supplemental structural inspections to increase the life of the airframe above more than
25000 flying hours or 30000 landings:
Table 6 Supplemental Inspections
SUPPLEMENTAL INSPECTIONS
Task number Inspection/Reference Threshold (whichev-
er comes first)
Repeated Interval (whichever
comes first)
Flying
Hours
Landings
Flying
Hours
Landings Years
27-00/402 Bonding leads to all flight control surfaces
Examine 32,500 42,000 12,500 15,000
6
32-20/403 NLG
Overhaul
CMM 02100
Parts kit P/N 500.60.12.029 25,000 30,000 8,300 10,000
6
32-50/404 NLG steering mechanism
Examine
12-B-32-50-00-00A-310A-A 32,500 42,000 8,300 10,000
6
52-10/405 Passenger/crew door piano hinge
Eddy current inspection
12-B-52-00-01-00A-353A-A 32,500 42,000 12,500 15,000
52-10/406 Passenger/crew door skin
Eddy current inspection
12-B-52-10-01-00A-353A-A 25,000 30,000 12,500 15,000
6
52-30/407 Cargo door piano hinge
Eddy current inspection
12-B-52-30-00-01A-353A-A 32,500 42,000 12,500 15,000
52-30/408 Cargo door skin
Eddy current inspection
12-B-52-30-01-00A-353A-A 25,000 30,000 12,500 15,000
6
53-00/419 Frame 40
Eddy current inspection
12-B-53-30-02-00A-353A-A
or
12-B-55-30-03-00A-353A-A 32,500 42,000 12,500 15,000
55-30/420 Vertical stabilizer forward attachment to
Frame 40
Eddy current inspection
12-B-55-30-03-00A-353A-A 32,500 42,000 12,500 15,000
55-40/410 Rudder trim tab
Examine
12-B-55-40-04-00A-310A-A 32,500 42,000 12,500 15,000
6
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-05-10-30-00A-280A-A
UNCLASSIFIED 2021-12-04 Page 3