• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-22 07:03来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  27QT2, 28QT1, 28QT2, 29QT1, 29QT2, 30QT1, 30QT2, 59QT1, 59QT2, 60QT1, 
R  60QT2, 61QT1, 61QT2, 34QT1, 34QT2 
R  (Ref. Fig. 407/TASK 28-42-15-991-006) 
R  (a) Put the probe (11) in the correct position and loosely install 
R  the bolts (1) and the washers (2). 
R  (b) Measure the clearance between the structure and the top and 
R  bottom of the probe (11). Make sure that the clearance is a 
R  minimum of 7.0 mm (0.2755 in.). 
R  NOTE : When a probe is installed, a minimum clearance of 7.0 mm____ 
R  (0.2755 in.) is recommended. (A clearance of less than 7.0 
R  mm (0.2755 in.) but more than 5.0 mm (0.1968 in.) is 
R  acceptable, if local installation does not allow 
R  recommened clearance) 
R  (c) To prevent possible static discharge, make sure that the fuel 
R  probe is not less than 5.0 mm (0.1968 in.) from: 
R  - the nearest structure 
R  - rib and tank wall 
R  - pipework 
R  - brackets and p-clips 
R  - fasteners and other metal parts. 
R  (d) TORQUE the bolts (1) to between 0.45 and 0.56 m.daN (39.82 and 
R  49.55 lbf.in). 
R  (e) Remove the blanking caps from the electrical connectors. 
R  (f) Identify and connect the electrical connectors of the cable (10) 
R  with the screws (5), (6) and (7). 
R  (g) TORQUE the screws (5), (6) and (7) as follows: 
R  - the screw (5) to between 0.102 and 0.124 m.daN (9.02 and 10.97 
R  lbf.in) 
R  - the screw (6) to between 0.203 and 0.226 m.daN (17.96 and 19.99 
R  lbf.in)

 

R  - the screw (7) to between 0.316 and 0.362 m.daN (27.96 and 32.03 
R  lbf.in). 
R  (h) Put the cable (10) in position under the clamp block (8) and 
R  TORQUE the clamp screw (9) to between 0.023 and 0.045 m.daN (2.03 
R  and 3.98 lbf.in). 
R  (i) Install the cable ties (2), as necessary, to attach the cable 
R  (10) to the probe (11). 
R  Subtask 28-42-15-865-064 
R  C. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  1QT, 2QT, 8QT. 
R  Subtask 28-42-15-740-054 
R  D. Test 
R  (1) Do a status report (BITE) of the FQI system (Ref. TASK 28-42-00-740-
R  001). 
R  5. Close-up________ 
R  Subtask 28-42-15-410-056 
R  A. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Make sure that all of the bonding straps are correctly installed and 
R  attached (Ref. TASK 20-28-00-912-002), before you install the 
R  fuel-tank access panels. 
R  (3) Remove the HOOK-COVER (RIB 2 SURGE DOORS) and carefully close the 
R  spring-loaded surge door 540AZ (640AZ). 
R  (4) Remove the HOOK-COVER (RIB2-SURGE DOORS) and carefully close the 
R  spring-loaded surge door 540BZ (640BZ). 
R  (5) Install the applicable access panels (Ref. TASK 57-27-11-400-001) or 
R  (Ref. TASK 57-27-11-400-002): 
R  - FOR 21QT1, 23QT1, 25QT1, 26QT1, 54QT1, 56QT1 
R  - install 540AB: 
R  - FOR 28QT1, 27QT1

 

R  - install 540BB: 
R  - FOR 29QT1 
R  - install 540DB: 
R  - FOR 30QT1 
R  - install 540FB: 
R  - FOR 34QT1 
R  - install 540QB: 
R  - FOR 59QT1 
R  - install 540HB: 
R  - FOR 21QT2, 23QT2, 25QT2, 26QT2, 54QT2, 56QT2 
R  - install 650AB: 
R  - FOR 28QT2, 27QT1 
R  - install 640BB: 
R  - FOR 29QT2 
R  - install 640DB: 
R  - FOR 30QT2 
R  - install 640FB: 
R  - FOR 34QT2 
R  - install 640QB: 
R  - FOR 59QT1 
R  - install 640HB. 
R  Subtask 28-42-15-650-052 
R  B. Fuel Configuration 
R  (1) Refuel, defuel or transfer fuel as necessary (Ref. TASK 12-11-28-650-
R  003), (Ref. TASK 28-25-00-650-001) or (Ref. TASK 28-25-00-869-001). 
R  Subtask 28-42-15-942-054 
R  C. Removal of Equipment 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM FUEL 燃油5(68)