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

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4.1.3 Open and install a Safety clip - Circuit breaker hold open (Pt.No. T12-030) on this circuit breaker:
− IGNITION (ESSENTIAL BUS)
− STARTER (ESSENTIAL BUS).
4.1.4 Remove the engine cowlings 42AT and 42AB.
4.1.5 Remove and discard the lockwire from the exhaust duct cap Figure 1 [20].
4.1.6 Remove the exhaust duct cap Figure 1 [20] from the union Figure 1 [21].
4.1.7 Disconnect the P3 pipe Figure 1 [24] from the union Figure 1 [22].
4.1.8 Disconnect the P3 pipe Figure 1 [26] and the union Figure 1 [22] from the port Figure 1 [23] and the
EPA tank Figure 1 [25].
4.1.9 Remove the left spark ignitor, refer to AMM 12-B-74-20-00-00A-920A-A.
4.1.10 Install the spray tube Figure 1 [27] finger tight in the left spark ignitor position Figure 1 [28]. Make sure
the RGB tag on the spray tube Figure 1 [27] points toward the reduction gearbox.
4.1.11 Connect the wash rig to the spray tube Figure 1 [27].
4.1.12 Remove the safety clip and close the circuit breaker:
− STARTER (ESSENTIAL BUS).
4.2
CAUTION
OBEY THE STARTER MOTOR OPERATION LIMITS. THIS WILL HELP PREVENT DAMAGE TO
THE STARTER MOTOR.
Procedure
4.2.1 Energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
4.2.2 Do the dry motor of the engine, refer to AMM 12-B-71-00-00-00A-901A-A. When the Ng increases to
5% operate the wash rig to supply the rinse solution to the engine.
4.2.3 Use the chronograph in the cockpit to measure the time of the operation.
4.2.4 Stop the starter motor after 30 seconds.
4.2.5 When the Ng decreases to 5% stop the supply of rinse solution to the engine.
4.2.6 If a water/methyl alcohol solution was used do a dry motor of the engine, refer to AMM 12-B-71-00-00-
00A-901A-A.
4.2.7 De-energize the aircraft electrical system, refer to AMM 12-B-24-00-00-00A-901A-A.
4.3 Close Up
4.3.1 Open and install a Safety clip - Circuit breaker hold open (Pt.No. T12-030) on this circuit breaker:
− STARTER (ESSENTIAL BUS).
4.3.2 Disconnect the wash rig from the spray tube Figure 1 [27].
4.3.3 Remove the spray tube Figure 1 [27] from the engine.
4.3.4 Install the left spark ignitor, refer to AMM 12-B-74-20-00-00A-920A-A.
4.3.5 Connect the P3 pipe Figure 1 [26] and the union Figure 1 [22] to the EPA tank Figure 1 [25] and the
port Figure 1 [23].
4.3.6 Connect the P3 pipe Figure 1 [24] to the union Figure 1 [22].
4.3.7 Install the exhaust duct cap Figure 1 [20] on the union Figure 1 [21].
4.3.8 Torque the exhaust duct cap Figure 1 [20] to between 7,4 and 8,5 Nm (65 and 75 lbf in).
4.3.9 Safety the exhaust duct cap Figure 1 [20] with Lockwire (standard) (Pt.No. P02-007).
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-71-00-00-00A-250A-A
UNCLASSIFIED 2021-12-04 Page 8