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时间:2011-03-28 22:58来源:蓝天飞行翻译 作者:航空
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R  pins A/29, 30 to pins AB/14D, 15D for the PRIMARY GPS DATA IN 
R  bus and pins A/13, 14 to pins AB/14J, 15J for the PRIMARY GPS 
R  TIME MARK bus (Ref. ASM 34-58/01).
 B. Do the test given in para. 3.


R


 TASK 34-58-00-810-812
 Loss of the GPSSU2 Data on the ADIRU3
 1. Possible Causes
_______________ R - GPSSU-2 (1SN2)
 - ADIRU-3 (1FP3) R - wiring from the GPSSU2 to the ADIRU3
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R  AMM 34-12-34-000-001 AMM 34-12-34-400-001 AMM 34-14-00-740-001 AMM 34-58-31-000-001 AMM 34-58-31-400-001 ASM 34-58/01 Removal of the ADIRU (1FP1, 1FP2, 1FP3)Installation of the ADIRU (1FP1, 1FP2, 1FP3)Interface Test of the IR Removal of the GPSSU (1SN1,1SN2) Installation of the GPSSU (1SN1,1SN2) 
3. Fault Confirmation__________________ 
R
 A. Test

 (1) Do the Interface test of the IR (system 3) (Ref. AMM TASK 34-14-00-
740-001). R
 4. Fault Isolation
_______________
R A. If the test gives the maintenance message GPSSU2 (1SN2)/ADIRU3 (1FP3):
R - replace the GPSSU-2 (1SN2) (Ref. AMM TASK 34-58-31-000-001) and (Ref.
R AMM TASK 34-58-31-400-001).

R (1) If the fault continues:
R - replace the ADIRU-3 (1FP3) (Ref. AMM TASK 34-12-34-000-001) and
R (Ref. AMM TASK 34-12-34-400-001).

R (a) If the fault continues:
R - do a check and repair the wiring from the GPSSU2 to the ADIRU3:
R pins A/29, 30 to pins AB/7C, 8C for the SECONDARY GPS DATA IN
R bus and pins A/13, 14 to pins AB/1C, 2C for the SECONDARY GPS
R TIME MARK bus (Ref. ASM 34-58/01).

 「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 ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 223
 Feb 01/05 CES


 B. Do the test given in para. 3.

 「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 ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 224
 Feb 01/05R
 CES  Loss of GPS Data on the ADIRU1


 1. Possible Causes
_______________
 - MMR-1 (40RT1)

 - MMR-2 (40RT2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-32-00-869-002 Procedure for Class 3 Faults Reading
 AMM 34-14-00-740-001 Interface Test of the IR
 AMM 34-36-31-000-002 Removal of the Multi Mode Receiver (40RT1, 40RT2)
 AMM 34-36-31-400-002 Installation of the Multi Mode Receiver (40RT1,

 40RT2)
 3. Fault Confirmation
__________________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. Test
 (1) Do the Interface test of the IR (system 1) (Ref. AMM TASK 34-14-00-740-001).
 **ON A/C ALL
 4. Fault Isolation
_______________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. If the test gives the maintenance message GPSSU1 (1SN1) + GPSSU2 (1SN2):
 - read the CFDIU CLASS 3 FAULTS for ATA 341400 and SOURCE IR1 (Ref. AMM TASK 31-32-00-869-002).
 NOTE : In this case the GPSSU message is for the GPS part of the related
____
 MMR.

 「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 ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 225
 May 01/05 CES


R  (1) If the CLASS 3 FAULTS report gives one or two of these maintenance 
R  messages GPSSU1 (1SN1)/ADIRU1 (1FP1) and GPSSU2 (1SN2)/ADIRU1 (1FP1), 
R  you can find the related trouble shooting procedure in the applicable 
R  Page Block 101. 
R  (2) If the CLASS 3 FAULTS report does not give one or two of these 
R  maintenance messages GPSSU1 (1SN1)/ADIRU1 (1FP1) and GPSSU2 
R  (1SN2)/ADIRU1 (1FP1): 
R  - replace the MMR-1 (40RT1) and MMR-2 (40RT2) (Ref. AMM TASK 34-36-
R  31-000-002) and (Ref. AMM TASK 34-36-31-400-002). 
R  B. Do the test given in para. 3.

 

 TASK 34-58-00-810-826
 
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