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时间:2011-03-28 22:53来源:蓝天飞行翻译 作者:航空
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 - make sure that there is continuity between pins A/J,K,N,P and that there is an open circuit between pins A/L,M.


 a If the pin programming is incorrect:
_
 - repair the aircraft wiring

 - connect the electrical connector of the ADM (19FP4)

 - install the ADIRU2.


 b If the pin programming is correct:
_
 - disconnect the electrical connector of the ADM (19FP5)

 - make sure that there is continuity between pins A/J,K,M,P and that there is an open circuit between pins A/L,N.

 - If the pin programming is incorrect: repair the aircraft wiring connect the electrical connector of the ADM (19FP5)


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 204-299, 301-399, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page B202
 401-499, Aug 01/05 CES install the ADIRU2.


 - If the pin programming is correct: replace the ADM (19FP1) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001). . If the fault continues: replace the ADM (19FP4).
 * If the fault continues: replace the ADM (19FP5).
 **ON A/C ALL
 B. Do the test given in Para. 3.


 Failure of the ADR3-SDI Pin-Programming
 1. Possible Causes
_______________
 - ADIRU-3 (1FP3)

 - ADM-L TOTAL PRESSURE (19FP1)

 - ADM-R STATIC PRESSURE (19FP4)

 - ADM-L STATIC PRESSURE (19FP5)

 - aircraft wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-11-17-000-001 Removal of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-11-17-400-001 Installation of the Air Data Module
 (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-13-00-740-002 INTERFACE TEST of the ADR ASM 34-12/03 ASM 34-13/03
 3. Fault Confirmation
__________________
 A. Test Do the Interface test of the ADR (system 3) (Ref. AMM TASK 34-13-00-740-002).
 4. Fault Isolation
_______________
R **ON A/C 001-049, 101-105, 151-199, 201-203,
 A. If the test gives the maintenance message WRG: SDI PIN PROG:
 - remove the ADIRU-3 (1FP3), (Ref. AMM TASK 34-12-34-000-001)

 - do a check of pins AB/1A,5A,6A on the rack connector.

 - compare the state of the pins with the SDI PIN PROGRAMMING given in the ASM (Ref. ASM 34-12/03).


 (1) If the pin programming is incorrect:
 - repair the aircraft wiring: defective pins

 - install the ADIRU3 (Ref. AMM TASK 34-12-34-400-001).


 「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 ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page B204
 May 01/05 CES (2) If the pin programming is correct:


 - swap the ADIRU3 and the ADIRU1.
 (a) If the fault stops:

 - replace the ADIRU that you installed on side 2.

 (b) If the fault continues:

 - get access to the ADM-L TOTAL PRESSURE (19FP1) (Ref. AMM TASK 34-11-17-000-001) (Para. 2.B.)

 - disconnect the electrical connector of the ADM (19FP1)

 - make sure that there is continuity between pins A/J,K and that there is an open circuit between pins A/L,M,N,P.

 


 1 If the pin programming is incorrect:
_
 - repair the aircraft wiring (Ref. ASM 34-13/03)

 - connect the electrical connector of the ADM (19FP1)

 - install the ADIRU3.


 2 If the pin programming is correct:
_
 - get access to the ADM-R STATIC PRESSURE (19FP4) ADM-L STATIC PRESSURE (19FP5), (Ref. AMM TASK 34-11-17-000-001) (Para. 2.B.)

 - disconnect the electrical connector of the ADM (19FP4)

 - make sure that there is continuity between pins A/J,K,N,P and that there is an open circuit between pins A/L,M.


 a If the pin programming is incorrect:
_
 - repair the aircraft wiring

 - connect the electrical connector of the ADM (19FP4)

 - install the ADIRU3.


 b If the pin programming is correct:
_
 - disconnect the electrical connector of the ADM (19FP5)

 - make sure that there is continuity between pins A/J,K,M,P and that there is an open circuit between pins A/L,N.
 
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