first terminal block (Ref. ASM 34-51/01).
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 ∞∞34-51-00∞∞∞∞∞∞∞∞∞∞Page 222
Feb 01/05R
CES Loss of the DME 1 Data on the ND
1. Possible Causes
_______________
- INTRG-DME, 1 (2SD1)
- ANTENNA-DME, 1 (3SD1)
- wiring from the DME antenna 1 (3SD1) to the DME interrogator 1 (2SD1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 34-51-00-720-001 Functional Test of the DME
AMM 34-51-00-740-002 BITE Test of the DME
AMM 34-51-11-000-002 Removal of the DME Antenna (3SD1, 3SD2)
AMM 34-51-11-400-002 Installation of the DME Antenna (3SD1, 3SD2)
AMM 34-51-33-000-001 Removal of the DME Interrogator (2SD1,2SD2)
AMM 34-51-33-400-001 Installation of the DME Interrogator (2SD1,2SD2)
ASM 34-51/01
3. Fault Confirmation
__________________
A. Test
(1) Do the functional test of the DME (Ref. AMM TASK 34-51-00-720-001).
4. Fault Isolation
_______________
A. If the DME 1 data do not come into view on the ND:
- do the BITE test of the DME (Ref. AMM TASK 34-51-00-740-002).
(1) If the test gives a maintenance message: R - Do the trouble shooting procedure related to the maintenance R message. R
(2) If the test does not give a maintenance message:
- replace the INTRG-DME, 1 (2SD1) (Ref. AMM TASK 34-51-33-000-001) and (Ref. AMM TASK 34-51-33-400-001).
(a) If the fault continues:
- replace the ANTENNA-DME, 1 (3SD1) (Ref. AMM TASK 34-51-11-000-002) and (Ref. AMM TASK 34-51-11-400-002).
1 If the fault continues:
_
- do a check and repair the wiring from the DME antenna 1 (3SD1) to the DME interrogator 1 (2SD1) (Ref. ASM 34-51/01).
B. Do the test given in Para. 3.
Loss of the DME 2 Tuning Data
1. Possible Causes
_______________
- FMGC-2 (1CA2)
- RMP-COM/NAV FREQ SEL, 2 (1RG2)
- INTRG-DME, 2 (2SD2)
- wiring of the FMGC OWN CB 1 bus from the FMGC 2 (1CA2) to the first
terminal block
- wiring of the DATA FROM FMGC bus from the COM/NAV FREQ SEL RMP 2 (1RG2) to the first terminal block
- wiring of the NAV DATA OUTPUT bus from the COM/NAV FREQ SEL RMP 2 (1RG2) to the first terminal block
- wiring of the FREQ FUNCT SELECT DATA INP A bus from the DME interrogator 2 (2SD2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-83-34-000-001 Removal of the FMGC (1CA1,1CA2)
AMM 22-83-34-400-001 Installation of the FMGC (1CA1,1CA2)
AMM 23-13-13-000-001 Removal of the Radio Management Panel (CRMP) (1RG1,
1RG2, 1RG3) AMM 23-13-13-400-001 Installation of the Radio Management Panel (CRMP)
(1RG1, 1RG2, 1RG3) AMM 34-14-00-740-001 Interface Test of the IR AMM 34-51-00-740-002 BITE Test of the DME AMM 34-51-33-000-001 Removal of the DME Interrogator (2SD1,2SD2) AMM 34-51-33-400-001 Installation of the DME Interrogator (2SD1,2SD2) AMM 34-55-00-740-002 BITE Test of the VOR/MKR ASM 22-86/02 ASM 23-13/01 ASM 34-51/01
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the DME (Ref. AMM TASK 34-51-00-740-002).
「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 ∞∞34-51-00∞∞∞∞∞∞∞∞∞∞Page 225
Feb 01/05R
CES
4. Fault Isolation
_______________
A. If the test gives the maintenance message FMGC2(1CA2)/RMP2(1RG2)/DME2(2SD2): - on the center pedestal, on the RMP 2, push the NAV and the VOR
pushbutton switches (the green LED on these pushbutton switches comes on)
- do the BITE test of the DME (Ref. AMM TASK 34-51-00-740-002).
(1) If the test does not give the maintenance message
FMGC2(1CA2)/RMP2(1RG2)/ DME2(2SD2):
- do the Interface test of the IR (system 1) (Ref. AMM TASK 34-14-00-740-001). 中國航空網 m.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(97)
