Form ASI-PC6-Engine Installation
Reissued: 2
Revision: 1
Date: July 2020
Page 2 of 26
NO.
DESCRIPTION
TASK NO. MECH. ENG.
RII
E.
Engine Driven Fuel Pump (Ref. Fig. 410)
1. Remove the blank from the opening.
2. Install a new gasket (8).
3. Install the fuel pump (7), washers (5) and nuts (6).
4. Torque the nuts (6) to between 8,5 and 9,6 Nm (75 and 85 lbf in.).
N/A
F.
Gas Generator and Propeller Tachometer Generators (Ref. Fig. 410)
1. Remove the blank from the opening.
2. Install a new gasket (2).
3. Install the generator (1), washers (3) and nuts (4).
4. Torque the nuts (4) to between 8,5 and 9,6 Nm (75 and 85 lbf in.).
N/A
G.
Torque Indicating System (Ref. Fig. 411, Sheets 1 and 2)
1. Install a new O-ring (1).
2. Install the adapter (8).
3. Remove the bottom RH nut (6) from the propeller tachometer
generator.
4. Install the P-clip (4) and torque transducer (3).
5. Install the nut (6).
6. Torque the nut (6) to between 8,5 and 9,6 Nm (75 and 85 lbf in.).
7. Install the torque pressure pipe (2).
8. Install the case reference pressure hose (7).
N/A
H.
Propeller Overspeed Governor (Ref. Fig. 412)
1. Install a new gasket (4) on the replacement engine.
2. Install the governor with the washers (1) and nuts (2).
3. Torque the nuts (2) to between 19,2 and 21,5 Nm (170 and 190 lbf in.).
N/A
I.
Drain Line Adapter, QAD Adapter (if applicable) and Starter-Generator (Ref. Fig. 413)
1. Install the drain adapter (7).
2. Install a new gasket (1).
3. If applicable, install the QAD adapter (2) with the washers (3) and nuts
(4).
4. Install the starter-generator (Ref. 24-31-11) but connect the electrical
cables after you install the engine (Ref. Para. 7.H.(1))
24-31-11
N/A
J.
Harness (Ref. Fig. 414)
1. If applicable, install the propeller de-icer unit (Ref. 30-60-01, Page
Block 401).
2. If necessary, replace the heat insulating tape installed on the harness
between the engine flanges A and C.
3. Put the harness assembly in position on the engine.
4. Install the P-clips to secure the harness.
5. Remove the identity marks and connect the ITT indication leads to the
T5 terminal block.
6. If applicable, remove the identity marks and connect the propeller de-
icer leads to the de-icer unit terminal block.
7. Connect the electrical plugs at the:
i. chip detector.
ii. propeller tachometer generator.
iii. torque pressure transducer.
8. Remove the two thrust bearing cover attaching nuts.
9. Install the low pitch warning switch mounting bracket and warning
switch on to the mounting studs.
10. Install the warning switch linkage block on to mounting stud on the
propeller reversing lever.
11. Install the washer and nut to secure the warning switch linkage block,
then tighten the nut with your hand. Make sure that the block is free to
turn on the stud.
12. Safety the nut with a new cotter pin.
30-60-01
N/A
Содержание PILATUS PORTER PC6
Страница 2: ...MAINTENANCE PROGRAM PILATUS PC 6 DOCUMENT NUMBER SAP 27 REISSUE 2 REVISION 1 JULY 2020...
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Страница 122: ...Form ASI PC6 Engine Removal Reissued 2 Revision 1 Date July 2020 Page 6 of 25...
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Страница 144: ...Form ASI PC6 Propeller Installation Reissued 2 Revision 1 Date July 2020 Page 3 of 7...
Страница 145: ...Form ASI PC6 Propeller Installation Reissued 2 Revision 1 Date July 2020 Page 4 of 7...
Страница 151: ...Form ASI PC6 Propeller Removal Reissued 2 Revision 0 Date October 2019 Page 3 of 7...
Страница 152: ...Form ASI PC6 Propeller Removal Reissued 2 Revision 0 Date October 2019 Page 4 of 7...
Страница 178: ...Form ASI PC6 Alignment Symmetry Inspection Reissued 2 Revision 1 Date July 2020 Page 4 of 4 Table 2...
Страница 216: ...Form No ASI MD 65 Revision 3 July 2020 Page 5 of 7 Figure 201 Identification and Location of Fuel Manifold Adapters...
Страница 218: ...Form No ASI MD 65 Revision 3 July 2020 Page 7 of 7 Figure 203 Fuel Manifold Installation Clearance Checks...
Страница 231: ...Form No ASI MD 71 Revision 3 July 2020 Page 2 of 4 FIGURE 1...
Страница 232: ...Form No ASI MD 71 Revision 3 July 2020 Page 3 of 4 FIGURE 2...
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Страница 244: ...Form No ASI MD 90 Revision 3 July 2020 Page 4 of 8...
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