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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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 AUXI. CENTER TANK - Snapshot Word 3
 BIT DESCRIPTION VALUE -------------------------------------------------------------------------------15 Second pp to indicate program pin ACT 2 True = fitted 14 Second pp to indicate program pin ACT 1 True = fitted 13 First pp to indicate program pin ACT 2 True = fitted 12 First pp to indicate program pin ACT 2 True = fitted -------------------------------------------------------------------------------11 Status of capacitance sensor A2TU2 True = valid 10 Status of diode voltage for A2TU2 True = valid 09 Status of capacitance sensor A2TU2 True = in range 08 LO-Z SC1 in range DRIVER 2 True = in range -------------------------------------------------------------------------------07 LO-Z SC1 in range DRIVER 4 True = in range 06 Status of opp CPU power supply True = healthy 05 Status of diode voltage for A2TU1 True = valid 04 Status of capacitance sensor A2TU1 True = in range -------------------------------------------------------------------------------03 Tank Unit calibration low A2TU2 True = in range 02 Tank Unit calibration low A2TU1 True = in range 01 Tank Unit calibration low A1TU2 True = in range 00 Tank Unit calibration low A1TU1 True = in range
 1EFF : 301-399, 1 28-42-00Page A525 1 1 May 01/05R 1 1 1CES 1


 Subtask 28-42-00-740-105
 T. EVENT 0E (H) : Not Used Subtask 28-42-00-740-106
 U. EVENT 0F (H) : Not Used Subtask 28-42-00-740-107
 V. EVENT 0 (H) : Not Used
 5. Close-up
________ Subtask 28-42-00-860-064
 A. Aircraft Maintenance Configuration
 (1) Put the aircraft back to its initial configuration.
 (a)
 On the MCDU, push the line key adjacent to the RETURN indication until the MCDU Menu page comes into view.

 (b)
 On the MCDU, set the BRT knob to OFF.

 (c)
 If applicable, do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (d)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (e)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 1EFF : 301-399, 1 28-42-00Page A526 1 1 May 01/05R 1 1 1CES 1


 PROBE - FUEL QUANTITY (21QT1,21QT2,22QT1,22QT2,23QT1,23QT2,24QT1,24QT2,25QT1,
_____________________________________________________________________________ 25QT2,26QT1,26QT2,27QT1,27QT2,28QT1,28QT2,29QT1...) - REMOVAL/INSTALLATION
__________________________________________________________________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 TASK 28-42-15-000-001
 Removal of the Wing Tank Fuel-Quantity-Probe (21QT1/2,22QT1/2,23QT1/2,24QT1/2,2 5QT1/2,26QT1/2,27QT1/2,28QT1/2,29QT1/2,30QT1/2,31QT1/2,32QT 1/2,33QT1/2,34QT1/2)
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 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 blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific access platform 4 m (13 ft. 1 in.)

 1EFF : ALL 1 28-42-15Page 401 1 1 Aug 01/05 1 1 1CES 1 B. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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
 28-12-46-000-001  Removal of the Overpressure-Protector Outlet
 28-25-00-650-001  Pressure Defuel
 28-25-00-650-003  To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank
 57-27-11-000-001  Removal of the Access Panel (540AB, 540BB, 540CB,
 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB,
 640DB, 640EB, 640FB, 640GB)
 57-27-11-000-002  Removal of the Access Panel (540HB, 540JB, 540KB,
 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB,
 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB,
 ....)
 
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