STRUT.
(1)
Make sure you remove all unwanted materials from the strut cavities.
S 412-184
(2)
Install these access panels (AMM 54-62-00/201):
(a)
Access panel 462AL/472AL on the left side of the strut at NSTA 164.
(b)
Access panel 462EL/472EL on the left side of the strut at NSTA 217.
(c)
Access panel 462CL/472CL on the left side of the strut at NSTA 186.
S 442-185
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ LE FLAP SAFETY LOCK. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT DO THE STEPS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3) Do this task: "Safety Locks Removal and Extended Leading Edge Flaps Activation" (AMM 27-81-00/201).
S 412-187 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(4) Close the left and right thrust reversers (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
54-53-00
ALL ú ú 01N Page 240 ú Jun 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 412-365
(5)
Close the left and right core cowl panels (AMM 71-11-06/201).
S 412-188
(6)
Close the left and right fan cowl panels (AMM 71-11-04/201).
S 442-366
(7)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
TASK 54-53-00-702-189
9. Inboard Strut, Aft Tube - Leak Check (T2)
_________________________________________
A. General
(1) This task gives instuctions on how to do a leak check (T2) of the aft drain tube on the inboard engine strut.
B. Equipment
(1)
Water source - low pressure, can spray up to 2 quarts (1.9 liters) per minute
(2)
Container - 5 gallon (19 liter) capacity, can collect and measure water to within 1 fluid ounce (30 ml) (measure can be done in smaller containers)
(3)
Funnel - long necked
C. References
(1)
AMM 08-00-00/201, Leveling and Weighing
(2)
AMM 27-81-00/201, Leading Edge Flaps
(3)
AMM 51-31-01/201, Seals and Sealing
(4)
AMM 54-62-00/201, Nacelle Strut Access Panels
(5)
AMM 71-11-04/201, Fan Cowl Panels
(6)
AMM 71-11-06/201, Core Cowl Panels
(7)
AMM 78-31-00/201, Thrust Reverser System
D. Access
(1)
Location Zone
461 Nacelle Strut 2 - Forward Fairing
462 Nacelle Strut 2 - Torque Box
471 Nacelle Strut 3 - Forward Fairing
472 Nacelle Strut 3 - Torque Box
(2)
Access Panel 462GL Lower Midspar Pressure Relief Door Panel - Engine 2 511CT Wing Leading Edge Cover - Engine 2 472GL Lower Midspar Pressure Relief Door Panel - Engine 3 611CT Wing Leading Edge Cover - Engine 3
E. Prepare for the Leak Check
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
54-53-00
ALL ú ú 01N Page 241 ú Jun 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 042-344
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 NACELLES/PYLONS(70)
