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时间:2011-03-28 18:45来源:蓝天飞行翻译 作者:航空
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

 NOTE : If a leakage from the NLG shock absorber has occured, one return____ flight is permitted for repair to be completed, if: - the leak rate from the turning table drain hole is less than 10 drops/min, weight on wheels - the servicing level of the shock absorber is done , less than one hour before a flight

 


 NORMAL EXTENSION AND RETRACTION - FAULT ISOLATION PROCEDURES
____________________________________________________________
 TASK 32-31-00-810-801
 No Data from CFDIU. Interactive Mode Selection & Monitor Sequence Fault
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Possible Causes
_______________
 - LGCIU-1 (5GA1)

 - A/C wiring/interface from the CFDIU ARINC tray to the LGCIU 1 (2) ARINC tray


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 31-32-00-740-002 BITE Test of the Centralized Fault Display Interface
R Unit (CFDIU) AMM 31-32-00-869-001 Procedure for CFDS Switching to Back-up Mode AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2) AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2) ASM 32-31/02
 3. Fault Confirmation
__________________
 A. Test
 (1) This task is for the fault as reported in the "LAST LEG REPORT" by the LGCIU-1 (2) and is valid only if there are "NO" reported CFDIU faults.

 (2) On the A/C, set the MCDU to the interactive mode (MENU MODE) and access the L/G SYSTEM REPORT. The fault confirmation is that the SYSTEM REPORT is not available.


 4. Fault Isolation
_______________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 201
 Nov 01/00 CES B. LGCIU Reset and Initialization.


 (1) At the circuit breakers for LGCIU-1 (2).

 (a) Open the circuit breakers.

 (b) Close the circuit breakers.

 (c) Examine the ECAM for the fault warning.

 (d) If the fault warning on the ECAM clears, set the MCDU to MENU MODE and access the L/G SYSTEM REPORT.

 

 (2) If the SYSTEM REPORT is available, dialog is available and the LGCIU-1 (2) is reset and the ECAM fault warning clears.

 (3) Do GROUND SCANNING and make sure the fault condition is cleared from the ground log.

 (4) If you can not set the SYSTEM REPORT for the LGCIU-1, do the procedure for the CFDIU switching to back-up mode, (Ref. AMM TASK 31-32-00-869-001).


 NOTE : This procedure is not available for the LGCIU-2.
____
 (5) Do the procedure at Para. 4.B.(1), If dialog is not available, replace the LGCIU-1 (5GA1) (Ref. AMM TASK 32-31-71-000-001) (Ref. AMM TASK 32-31-71-400-001)

 (6) Do the procedure at Para 4.B.(1) to reset the LGCIU-1 and to clear the ECAM warning.

 (7) If you cannot set the SYSTEM REPORT for LGCIU-2.

 (a) Remove ground power.

 (b) Swap LGCIU-1 with LGCIU-2.

 (c) Do the procedure for CFDIU switching to back-up mode (Ref. AMM TASK 31-32-00-869-001)

 (d) Do the Para. 4.B.(1)

 

 (8) If the SYSTEM REPORT is not available, replace the LGCIU-2,

 (9) Install the LGCIU-1 in its initial location.


 (10) Repeat Para.4.B.(1) to reset the LGCIU-2 and clear the ECAM warning.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞32-31-00∞∞∞∞∞∞∞∞∞∞Page 202
 Feb 01/98 CES


 (11) If the fault still shows, do the CFDIU BITE (Ref. AMM TASK 31-32-00-740-002)
 (a) If the CFDIU BITE shows a fault condition, do the CFDIU Trouble Shooting (Refer to TSM 31-32-00)

 (b) If the CFDIU shows a "NO" fault condition, do a check of the A/C wiring/interface from the CFDIU ARINC tray to the LGCIU 1 (2) ARINC tray (Ref. ASM 32-31/02)


 5. Close-up
________
 A. Put the aircraft back to its initial configuration.
 
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