S 416-002
(13)
Install the pneumatic ducts removed for access (AMM 30-11-01/401).
S 866-002
WARNING: DO THE ACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS
_______ (AMM 27-81-00/201). THE SLATS CAN MOVE QUICKLY AND CAUSE INJURY TO PERSONS.
(14)
Do the activation procedure for the leading edge slats (AMM 27-81-00/201).
(15)
Remove electrical power if it is not necessary (AMM 24-22-00/201).
S 866-003
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-11-07
ALL ú ú 01 Page 605 ú Jun 20/96
A
757 MAINTENANCE MANUAL
CENTER TANK PURGE DOOR - REMOVAL/INSTALLATION
_____________________________________________
1. General_______
A. The center tank purge door is installed on the rear spar of the center fuel tank, approximately 2 feet to the right of the airplane centerline. The center tank purge door is used to close the venturi port, when not in use. The venturi port is used for purging the fuel tank.
B. This procedure contains two tasks. The first task removes the center tank purge door. The second task installs the center tank purge tank.
TASK 28-11-08-004-015
2. Remove the Center Tank Purge Door (Fig. 401)_________________________________
A. Equipment
(1)
Lanyard - commercially available
B.
References
(1)
AMM 06-41-00/201, Fuselage (Major Zones 100 and 200) Access Doors and Panels
(2)
AMM 28-11-00/201, Fuel Tanks
(3)
AMM 28-11-02/401, Center Tank Access Door
(4)
AMM 28-26-00/201, Defueling
(5)
AMM 32-00-15/201, Landing Gear Door Locks
(6)
AMM 32-00-20/201, Landing Gear Downlocks
C.
Access
(1)
Location Zone
134 Wing Center Section (Right)
(2)
Access Panels
134AZ Center Tank Access Door (Right)
134BZ Baffle Door
134CZ Baffle Door
134DZ Baffle Door
D.
Procedure
(1)
Defuel the center fuel tank (AMM 28-26-00/201).
S 214-016
(2)
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
S 654-020
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 2(14)