(2)
Do this task: Pressure Defueling (AMM 28-26-00/201).
(3)
Drain the fuel tank sumps (AMM 12-11-03/301).
S 942-266
(4)
Make sure the airplane is correctly grounded to an approved and identified ground (AMM 20-41-00/201).
S 652-264
S 652-265
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-11-00
ALL ú ú 01 Page 228 ú May 20/98
A
757
MAINTENANCE MANUAL
S 492-267
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE TRAILING EDGE FLAPS.
_______ ACCIDENTAL OPERATION OF THE TRAILING EDGE FLAPS COULD CAUSE INJURY TO PERSONS.
(5) Do the deactivation procedure for the trailing edge flaps (AMM 27-51-00/201).
S 492-268
WARNING: DO THE DEACTIVATION PROCEDURE OF THE LEADING EDGE SLAT
_______ (AMM 27-81-00/201). IF THE LEADING EDGE SLAT OPERATES ACCIDENTALLY, IT CAN CAUSE INJURY.
(6)
Do the deactivation procedure of the leading edge slats (AMM 27-81-00/201).
S 492-269
(7)
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
S 492-270
WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO INSTALL THE DOOR
_______ LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(8)
Open the doors for the landing gear and install the door locks (AMM 32-00-15/201).
S 942-271
(9)
Put ropes around the airplane to identify the hazardous location areas (Figure 201), and attach these signs with words you can see clearly written on both sides:
(a)
DANGER - OPEN FUEL TANKS - NO SMOKING
(b)
AUTHORIZED PERSONNEL ONLY
S 862-272
(10)
Make sure the fuel pump switch lights on the overhead panel, P5, are in the off position, and attach DO-NOT-OPERATE tags.
S 862-275
(11)
Open these circuit breakers on the main power distribution panel, P6, and attach DO-NOT-CLOSE tags:
(a)
6F15, L FUEL OVRD PUMP
(b) 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊 燃油 CHAPTER 28 - FUEL 1(42)
