(2)
AMM 71-00-00/501, Power Plant
(3)
AMM 78-31-00/201, Thrust Reverser System
(4)
AMM 80-11-01/401, Starter
(5)
WDM 73-21-15, 73-21-25, 73-21-35, 73-21-45, 77-12-21, 77-12-22, 77-12-23, 77-12-24
(6)
SSM 73-21-01, 77-12-02
E.
Access
(1)
Location Zone 412 Engine 1 - Main Gearbox Aft Face 6 o'clock 422 Engine 2 - Main Gearbox Aft Face 6 o'clock 432 Engine 3 - Main Gearbox Aft Face 6 o'clock 442 Engine 4 - Main Gearbox Aft Face 6 o'clock
(2)
Access Panel 415 and 416 Thrust Reverser Halves - Engine 1 425 and 426 Thrust Reverser Halves - Engine 2 435 and 436 Thrust Reverser Halves - Engine 3 445 and 446 Thrust Reverser Halves - Engine 4
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-05
ALL ú ú N01 Page 418 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F. Install the Stator
S 034-071-N00
(1)
Remove the protection caps.
S 644-060-N00
(2)
Lubricate the new packing (15) with the petrolatum.
S 434-036-N00
(3)
Install the new packing (15) on the stator (17).
S 424-037-N00
(4)
With the bolt holes in the stator (17) aligned with the bolt holes in the EEC alternator drive pad, carefully install the stator (17) on the rotor (3).
S 644-059-N00
(5)
Lubricate the threads of the bolts (11) with the antigalling compound.
S 434-057-N00
(6)
ENGINES PRE-PW-SB 72-375;
Do these steps:
(a)
Put the heat shield (12) above the stator (17).
(b)
Attach the stator (17) and the heat shield (12) to the EEC alternator drive pad with the bolts (11) and washer (19).
(c)
Tighten the bolts (11) to 62-72 pound-inches (7.0-8.1 newton-meters).
S 434-056-N00
(7)
ENGINES POST-PW-SB 72-375;
Do these steps:
(a)
Attach the stator (17) to the EEC alternator drive pad with the bolts (11) and washer (19).
(b)
Tighten the bolts (11) to 62-72 pound-inches (7.0-8.1 newton-meters).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-05
ALL ú ú N01 Page 419 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(c) Use a 0.003 inch (0.076 mm) feeler guage to make sure the clearance between the EEC alternator (17) and the EEC Alternator Drive Pad is satisfactory. 1) If the feeler guage can go in the clearance, you must do a
check of the torque of the bolts (11).
2) If the bolts (11) are at the maximum torque and the EEC alternator stator (17) is not installed correctly, remove and install the stator (17) again.
3) Use the feeler guage again to make sure the clearance is satisfactory.
S 434-039-N00
(8)
Connect the cooling air tube (14) on the right side of the stator (17) with the clamp (13).
S 434-040-N00
(9)
Put the retaining plate (21) behind the cable end flanges of the stator (17).
(a)
Make sure the spacers point forward.
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本文链接地址：747-400 AMM 飞机维护手册 发动机燃油和控制 2(29)
