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

Страница: 467 / 715

Name Identifications/References Qty Reference Remark
Static blank Part T34-020 AR
Supplies
Table 4 Supplies
Name Identifications/References Qty Reference Remark
None
Spares
Table 5 Spares
Name Identifications/References Qty Reference Remark
None
Safety Conditions
Note
To identify the AGE and tools used in this procedure, refer to the List of AGE and Tools, TEM 12-B-00-00-00-00A-
060A-A .
Procedure
1 Remove the protective covers from the left and right pitot heads.
2 Use the Pitot adaptor kit (Pt.No. T34-005) to connect the Pitot static test set (Pt.No. Local supply) pitot
line to the left and right pitot heads.
3 Use the Static adaptor kit (Pt.No. T34-015) to connect the pitot static test set static line to the forward
and rear pressure inlet holes on the left and right static plates.
4 Open access panel 21QZ.
5 Open and install a Safety clip (circuit breaker hold open) (Pt.No. T12-030) on these circuit breakers:
− XPNDR 1 (AVIONIC 1 BUS)
− XPNDR 2 (AVIONIC 2 BUS).
6 Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
7 Set the pitot pressure on the pitot static test set to 150 kts.
8 In the AVIONICS SETUP window, set the BARO CORRECTION to InHg.
9 On the Primary Flight Display (PFD) Controllers, press the BARO rotary control to set 29.92 InHg.
10 On the Electronic Standby Instrument System (ESIS):
− Thales ESIS press the STD button to set 1013 hPa/29.92 InHg
− L3 ESI-1000 ESIS press the S button to set 1013 hPa/29.92 InHg
− L3 EFD-750 ESIS press the knob to set 1013 hPa/29.92 InHg/1013 mb.
11 On the pitot static test set, adjust the static pressure until the PFD and ESIS altitude displays read 0 ft.
(0 m).
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-34-14-00-00A-903B-A
UNCLASSIFIED 2021-12-04 Page 2