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时间:2011-03-22 07:03来源:蓝天飞行翻译 作者:admin
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R  DAMAGE TO EQUIPMENT. 
R  (1) Remove and discard the cable ties (1) to release the electrical cable 
R  (8) from the probe (10). 
R  (2) Loosen the terminal screw (7) on the terminal block (2). 
R  (3) Loosen the screws (3), (4) and (5) on the terminal block (2). 
R  (4) Identify and remove the electrical connectors of the cable (8). 
R  (5) Put blanking caps on the disconnected electrical connectors. 
R  (6) Remove the bolts (9) and (12). 
R  (7) Remove the probe (10). 
R  (8) Remove the bracket (11) from the probe (10).

 

 1EFF : 301-399, 1 28-42-15Page 446 1 1 May 01/04 1 1 1CES 1


 TASK 28-42-15-400-004

 Installation of the Center (Transfer) Tank Fuel-Quantity Probe (35QT, 36QT,
 37QT, 38QT, 51QT)
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING

_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific safety barriers R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 11-026  GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
cable ties  28-42-05 03C-060
 1EFF : 301-399, 1 28-42-15Page 447 1 1 May 01/05 1 1 1CES 1 D. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003  Pressure Refuel with Automatic Control
 20-28-00-912-002  Electrical Bonding of Components With Conductive
 Bolts and Screws in the Tanks
 28-10-00-910-001  Safety Procedures When You Do Work in a Fuel Tank
 28-10-00-910-002  Access to the Fuel Tanks and the Work Areas
 28-25-00-650-001  Pressure Defuel
 28-25-00-650-003  To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank
 28-25-00-869-001  Fuel Transfer
 28-42-00-740-001  Status Report (BITE)
 32-12-00-010-001  Open the Main Gear Doors for Access
 32-12-00-410-001  Close the Main Gear Doors after Access
 57-17-11-000-001  Removal of the Covers 147AZ (148AZ)
 57-17-11-400-001  Installation of the Covers 147AZ (148AZ)
 28-42-15-991-008  Fig. 408
 3. Job Set-up__________
 Subtask 28-42-15-941-064
 A. Safety Precautions

 WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
 (1) You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.
 (2) Make sure that the safety barriers are in position. Subtask 28-42-15-860-053
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the applicable fuel tank is defueled (Ref. TASK 28-25-00-650-001).

 (2)
 Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. TASK 28-25-00-650-003).

 (3)
 Make sure that the applicable MLG door(s) are open (Ref. TASK 32-12-00-010-001).


 1EFF : 301-399, 1 28-42-15Page 448 1 1 May 01/05R 1 1 1CES 1


 (4)
 Make sure that the GROUND LOCK SLEEVE is installed on the applicable MLG door actuator.

 (5)
 Make sure that the access platform is below the applicable access panel 147AZ (148AZ).

 (6)
 Make sure that the applicable access panel 147AZ (148AZ) is removed (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-17-11-000-001).
 
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