• 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


 -
FOR 30QT1
 remove 540FB


 -
FOR 31QT1
 remove 540GB


 -
FOR 32QT1
 remove 540HB


 -
FOR 33QT1
 remove 540LB


 -
FOR 34QT1
 remove 540QB


 -
FOR 21QT2, 22QT2, 23QT2, 24QT2, 25QT2, 26QT2
 remove 640AB


 -
FOR 27QT2, 28QT2

 


R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-15Page 409 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 remove 640BB


 -
FOR 29QT2
 remove 640DB


 -
FOR 30QT2
 remove 640FB


 -
FOR 31QT2
 remove 640GB


 -
FOR 32QT2
 remove 640HB


 -
FOR 33QT2
 remove 640LB


 -
FOR 34QT2
 remove 640QB.

 

 4. Procedure
_________
 (Ref. Fig. 402/TASK 28-42-15-991-002)
 Subtask 28-42-15-420-056
 A. Preparation for Installation
 (1)
 Clean the component interfaces and the adjacent areas with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Make sure that the parts retained from the removed component are clean and in the correct condition.


 Subtask 28-42-15-420-050
 B. Installation of the Fuel-Quantity-Probes
 (1) For the probe (6):
 (a)
 Put the probe (6) in position and install the bolts (5) and (8) and the washers (4).

 (b)
 TORQUE the bolts (5) and (8) to between 40 and 50 lbf.in (0.45 and 0.56 m.daN).


R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-15Page 410 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


 (2)
 For the probe (9):

 (a)
 Put the support tube (1) on top of the probe (9).

 (b)
 Put the probe (9) in position and install the bolts (8) and the washers (4).

 (c)
 Put the support tube (1) in position and install the bolts (2).

 (d)
 TORQUE the bolts (2) and (8) to between 40 and 50 lbf.in (0.45 and 0.56 m.daN).

 

 (3)
 For all the probes (6) and (9):


 CAUTION : REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU
_______ CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
 (a) Measure the clearance between the structure and the top and bottom of the probe (6) or (9). Make sure that the clearance is a minimum of 7.0 mm (0.2755 in.).
 NOTE : When a probe is installed, a minimum clearance of 7.0 mm
____ (0.2755 in.) is recommened. (A clearance of less than 7.0 mm (0.2755 in.) but more than 5.0 mm (0.1968 in.) is acceptable, if local installation does not allow the recommended clearance)
 (b) To prevent possible static discharge, make sure that the fuel probe is not less than 5.0 mm (0.1968 in.) from:
 -the nearest structure
 -rib and tank wall
 -pipework
 -brackets and p-clips
 -fasteners and other metal parts.
 (c)
 Remove the blanking caps and connect the electrical cables (10) to the probe (6) or (9).

 (d)
 Use the cable tie (3) and the cable tie (7) to attach the electrical cables (10) to the probe (6) or (9). Use the applicable tool, set to the minimum tension, to tighten the cable ties (3) and (7).


R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-15Page 411 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 28-42-15-865-053


 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QT, 2QT, 8QT.
 Subtask 28-42-15-740-050
 D. Test
 (1) Do a status report (BITE) of the FQI system (Ref. TASK 28-42-00-740-001).
 5. Close-up
________ Subtask 28-42-15-410-050
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access panel(s) that you removed (Ref. TASK 57-27-11-400-001) or (Ref. TASK 57-27-11-400-002), or for 540HB(640HB), (Ref. TASK 28-12-46-400-001).


 Subtask 28-42-15-650-050
 B. Fuel Configuration
 (1) Refuel, defuel or transfer fuel as necessary (Ref. TASK 12-11-28-650-003), (Ref. TASK 28-25-00-650-001) or (Ref. TASK 28-25-00-869-001).
 Subtask 28-42-15-942-050
 C. Removal of Equipment
 (1)
 Remove the safety barriers.
 
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(59)