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

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Name Identifications/References Qty Reference Remark
Static adaptor kit Part T34-015 AR
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 Preparation
1.1 Remove the protective covers from the left and right pitot heads.
1.2 Connect the Pitot static test set (Pt.No. Local supply) pitot line to the left and right pitot heads.
1.3 Connect the pitot static test set static line to the forward and rear pressure inlet holes on the left and
right static plates.
1.4 Open and install a Safety clip (circuit breaker hold open) (Pt.No. T12-030) on the circuit breakers:
− XPNDR 1 (AVIONIC 1 BUS)
− XPNDR 2 (AVIONIC 2 BUS)
− RAD ALT 1 (AVIONICS 1 BUS).
2 Procedure
2.1 Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
2.2 Do a leak test of the left and right pitot and static systems, refer to AMM 12-B-34-11-00-00A-903A-A.
2.3 Make sure that the Primary Flight Display (PFD) SAT display shows approximately the current OAT
value.
2.4 Set the pitot pressure on the pitot static test set to 50 kts.
2.5 On the maintenance panel, set the AIR/GND switch to AIR.
2.6 On the Primary Flight Display (PFD) Controllers, press the BARO rotary control to set Standard
Pressure (STD).
2.7 On the Electronic Standby Instrument System (ESIS):
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-34-16-00-00A-903A-A
UNCLASSIFIED 2021-12-04 Page 2