_
- replace the RMI-VOR/DME (11FN) (Ref. AMM TASK 34-57-22-000-001) and (Ref. AMM TASK 34-57-22-400-001).
B. Do the test given in Para. 3.
R **ON A/C 106-149, 201-299, 301-399, 401-499,
TASK 34-57-00-810-815
Loss of the Heading Data on the VOR/ADF/DME RMI
1. Possible Causes
_______________
- RMI-VOR/ADF/DME (21FN)
- SEL SW-ATT HDG (13FP)
- RELAY-HDG SOURCE SEL (19FN)
- wiring of the HDG SOURCE SEL relay (19FN)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 34-14-00-740-001 Interface Test of the IR
AMM 34-57-22-000-002 Removal of the VOR/ADF/DME RMI (21FN)
AMM 34-57-22-400-002 Installation of the VOR/ADF/DME RMI (21FN)
ASM 34-57/01
3. Fault Confirmation
__________________
A. Test
(1) Do the Interface test of the IR (Ref. AMM TASK 34-14-00-740-001).
4. Fault Isolation
_______________
A. If during the test, with the ATT HDG selector switch at CAPT 3, the HDG data do not come into view on the VOR/ADF/DME RMI (21FN):
- do a check for a maintenance message in the BITE test of the IR system.
(1) If the BITE test gives a maintenance message:
- Do the trouble shooting procedure related to the maintenance message.
(2) If the BITE test does not give a maintenance message:
- replace the SEL SW-ATT HDG (13FP)
(a) If the fault continues:
- replace the RELAY-HDG SOURCE SEL (19FN). 1 If the fault continues:
_
- do a check of the wiring of the HDG SOURCE SEL relay (19FN): . pins A/A and A/Z to the ground points
「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 : 106-149, 201-299, 301-399, 401-499, ∞∞34-57-00∞∞∞∞∞∞∞∞∞∞Page 227
Aug 01/05 CES . pin A/X to the ATT HDG selector switch (13FP): pin A/1 . pin A/2 to VOR/ADF/DME RMI (21FN): pin A/16. (Ref. ASM 34-57/01).
a If there is no continuity:
_
- repair the above wiring.
b If there is continuity:
_
- replace the RMI-VOR/ADF/DME (21FN) (Ref. AMM TASK 34-57-22-000-002) and (Ref. AMM TASK 34-57-22-400-002).
B. Do the test given in Para. 3.
_________________________________________________
TASK 34-58-00-810-801
Loss of the GPSSU1 Input on the ADIRU1
1. Possible Causes
_______________
- MMR-1 (40RT1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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):
- read the POST FLIGHT REPORT for other GPSSU1 (1SN1) maintenance messages (ATA 34-58-31 source IR2, IR3).
NOTE : In this case the GPSSU1 message is for the GPS part of the MMR1.
____
(1) If there is a minimum of one maintenance message:
- replace the MMR-1 (40RT1) (Ref. AMM TASK 34-36-31-000-002) and (Ref. AMM TASK 34-36-31-400-002).
「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 201
May 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 202 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 3(169)
