S 024-010-N00
WARNING: BEFORE YOU OPEN THE OIL TANK CAP, PERMIT A MINIMUM OF FIVE
_______ MINUTES AFTER THE ENGINE SHUTDOWN TO LET THE PRESSURE IN THE OIL TANK BLEED OFF. A FAST FLOW OF HOT OIL CAN OCCUR AND CAUSE INJURY TO YOU.
DO NOT KEEP THE OIL ON YOUR SKIN FOR A LONG TIME. IF YOU DO NOT CLEAN THE OIL OFF, THE OIL CAN CAUSE INJURY.
(2) Remove the bolts (4) which attach the last chance oil strainer (3).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-21-16
ALL ú ú N01 Page 411 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 024-048-N00
(3)
Use the PWA 85518 puller to remove the last chance oil strainer (3) from the housing.
S 034-011-N00
(4)
Remove the packing (5).
(a)
Discard the packing (5).
S 034-012-N00
(5) Install the protection caps.
TASK 79-21-16-004-013-N00
5. Remove the No. 4 Bearing Last Chance Oil Strainer (Fig. 401)
_________________________________________________
A. Standard Tools and Equipment
(1)
Container - 1 U.S. gallon (4 liter) capacity,
used to catch the oil
B.
References
(1)
AMM 71-11-04/201, Fan Cowl Panels
(2)
AMM 71-11-06/201, Core Cowl Panels
(3)
AMM 78-31-00/201, Thrust Reverser System
(4)
IPC 79-21-51 Fig. 05
C.
Access
(1)
Location Zone 412 Engine 1 - Turbine Exhaust Case 10:30 o'clock 422 Engine 2 - Turbine Exhaust Case 10:30 o'clock 432 Engine 3 - Turbine Exhaust Case 10:30 o'clock 442 Engine 4 - Turbine Exhaust Case 10:30 o'clock
(2)
Access Panel
415 Left Thrust Reverser Half - Engine 1
425 Left Thrust Reverser Half - Engine 2
435 Left Thrust Reverser Half - Engine 3
445 Left Thrust Reverser Half - Engine 4
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-21-16
ALL ú ú N01 Page 412 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D. Prepare to Remove the Last chance Oil Strainer
S 014-049-N00
(1) Open the left fan cowl panel (AMM 71-11-04/201).
S 044-067-N00
WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(2)
Do this procedure: Thrust Reverser Deactivation for Ground
Maintenance (AMM 78-31-00/201).
S 014-050-N00
(3)
Open the left core cowl panel (AMM 71-11-06/201).
S 044-068-N00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00 WHEN YOU OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(4)
Open the left thrust reverser (AMM 78-31-00/201).
E.
Remove the Last Chance Oil Strainer
S 494-015-N00
(1)
Put the container below the last chance oil strainer (13) to collect the remaining oil.
S 034-016-N00
(2)
Remove the hose clamps (9) which attach the heat shield (11) at the top connection of the oil pressure tube (6) for the No. 4 bearing.
(3)
Remove the heat shield (11) from the engine.
S 034-051-N00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-21-16
ALL ú ú N01 Page 413 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 滑油 OIL(90)