(2)
AMM 28-11-01/401, Main Tank Access Door
(3)
AMM 28-22-07/401, Fuel Line and Fittings
(4)
AMM 28-26-00/201, Defueling
B.
Access
(1)
Location Zones
541 Main Tank - Rib No. 5 to No. 17 (Left)
641 Main Tank - Rib No. 5 to No. 17 (Right)
(2)
Access Panels
541AB Main Tank Access Door (Left)
641AB Main Tank Access Door (Right)
C.
Procedure
S 654-037
(1)
Defuel the applicable left or right main fuel tank
(AMM 28-26-00/201).
S 654-038
(2)
Drain and purge the applicable left or right main fuel tank (AMM 28-11-00/201).
S 014-001
(3)
Remove the applicable left or right main tank access door, 541AB or 641AB (AMM 28-11-01/401).
S 944-039
WARNING: OBEY THE FUEL TANK ENTRY PRECAUTIONS (AMM 28-11-00/201).
_______ FAILURE TO OBEY THE FUEL TANK ENTRY PRECAUTIONS COULD CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(4) Obey the fuel tank entry precautions (AMM 28-11-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-04
ALL ú ú 01 Page 401 ú May 28/99
A
757
MAINTENANCE MANUAL
BYPASS VALVE
SEE A
END RIB OF
THE FUEL TANK
MOUNTING BRACKET
SUCTION SCREW
FEED LINE WASHER, NUT (EXAMPLE)
COUPLING
BYPASS VALVE
FWD OUTBD
FLANGE
SUCTION FEED LINE
FILTER SCREEN
MOUNTING
FASTENER
BRACKET
(EXAMPLE)
BYPASS VALVE
(LEFT SIDE SHOWN, RIGHT SIDE OPPOSITE)
A
Bypass Valve of the Fuel Boost Pump Installation
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-04
ALL ú ú 02 Page 402 ú May 28/99
A
757
MAINTENANCE MANUAL
S 014-040
(5) Go into the fuel tank.
S 014-002
(6) Find the bypass valve.
S 024-041
(7) To remove the bypass valve, do the steps that follow: (a) Remove the fasteners from the mounting brackets that attach the suction feed line to the end rib of the fuel tank.
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 3(63)