S 865-088

 (2)  
Put all the fuel measuring sticks for each fuel tank to their usual position (AMM 28-44-00/201).

 S 865-089

 (3)  
Service the shock struts (AMM 12-15-01/301 and AMM 12-15-02/301).

 S 865-030
 WARNING: DO THE ACITVATION PROCEDURE FOR THE LEADING EDGE SLAT.
_______ ACCIDENTAL SLAT OPERATION COULD CAUSE INJURY TO PERSONS.
 (4)  
Do the activation procedure for the leading edge slat
 (AMM 27-81-00/201).

 (5)  
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 865-090
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-21-00
 ALL  ú ú 01 Page 520 ú May 28/01

A

757 MAINTENANCE MANUAL
 FUELING ADAPTER AND VALVE - REMOVAL/INSTALLATION
________________________________________________
 1.  General_______
 A.  Two fueling adapters attach to the front spar just aft of leading edge slat No. 8 on the right wing. The fueling adapters are found through the fueling control panel door. There is a poppet assembly installed in each fueling adapter.
 B.  This procedure contains four tasks. The first task removes the fueling adapter. The second task installs the fueling adapter. The third task removes the poppet assembly. The fourth task installs the poppet assembly.
 TASK 28-21-01-004-022
 2.  Remove the Fueling Adapter (Fig. 401)__________________________
 A.  References
 (1)  
AMM 06-44-00/201, Wings (Major Zones 500 and 600) Access Doors and Panels

 (2)
AMM 24-22-00/201, Electric Power Control

 (3)
AMM 27-81-00/201, Leading Edge Slat System

 (4)
AMM 28-26-00/201, Defueling

 B.  
Equipment

 (1)
Container - Fuel Resistant, 2 Gallon (7.57 Liters)

 C.  
Access

 (1)  
Location Zone
 621 Leading Edge to Front Spar (Right)

 (2)  
Access Panel
 621GB Fueling Station Door (Right)

 D.  
Procedure

 (1)
Make sure the airplane is grounded to an approved ground.

 (2)
Remove electrical power from the airplane (AMM 24-22-00/201).

 S 214-064
 S 914-065
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 燃油 CHAPTER 28 - FUEL 2(64)