- replace the P/BSW-TERR ON ND, CAPT (30WZ1) (Ref. AMM TASK 33-10-00-000-002) and (Ref. AMM TASK 33-10-00-400-002).
(a) If the fault continues:
- do a check and repair the wiring of the TERRAIN POP-UP CAPT discrete between the GPWC (1WZ) and the TERR ON ND, CAPT pushbutton switch (30WZ1): for pin AA/1A of the GPWC (Ref. ASM 34-48/02).
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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 264
May 01/05R
CES Permanent Display of Terrain Data on F/O ND
1. Possible Causes
_______________
- GPWC (1WZ)
- P/BSW-TERR ON ND, F/O (30WZ2)
- wiring of the TERRAIN POP-UP F/O discrete between the GPWC (1WZ) and the TERR ON ND, F/O pushbutton switch (30WZ2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 33-10-00-000-002 Removal of the Bulbs and the Body of a Pushbutton Switch in the Cockpit AMM 33-10-00-400-002 Installation of the Bulbs and the Body of a
Pushbutton Switch in the Cockpit AMM 34-48-00-740-002 BITE Test of the Enhanced GPWC AMM 34-48-34-000-001 Removal of the GPWC (1WZ) AMM 34-48-34-400-001 Installation of the GPWC (1WZ) ASM 34-48/02
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the Enhanced GPWS (Ref. AMM TASK 34-48-00-740-002).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message: FO TERR ON ND PB SW (30WZ2)/GPWC (1WZ) - on the LDG GEAR CTL & IND PNL (402VU), make sure that the TERR ON ND,
F/O pushbutton switch (30WZ2) is not pushed (the ON legend is off)
- do a check for ground at pin AA/1B of the GPWC (Ref. ASM 34-48/02).
(1) If there is no ground:
- replace the GPWC (1WZ) (Ref. AMM TASK 34-48-34-000-001) and (Ref. AMM TASK 34-48-34-400-001).
「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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 265
May 01/05R
CES (2) If there is ground:
- replace the P/BSW-TERR ON ND, F/O (30WZ2) (Ref. AMM TASK 33-10-00-000-002) and (Ref. AMM TASK 33-10-00-400-002).
(a) If the fault continues:
- do a check and repair the wiring of the TERRAIN POP-UP F/O discrete between the GPWC (1WZ) and the TERR ON ND, F/O pushbutton switch (30WZ2): for pin AA/1B of the GPWC (Ref. ASM 34-48/02).
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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 266
May 01/05R
CES Loss of the Control Data Input 1 Bus of the GPWC
1. Possible Causes
_______________
- GPWC (1WZ)
- wiring of the FCU 1 DATA INPUT bus from the GPWC to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-48-00-740-002 BITE Test of the Enhanced GPWC AMM 34-48-34-000-001 Removal of the GPWC (1WZ) AMM 34-48-34-400-001 Installation of the GPWC (1WZ) ASM 34-48/02
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the Enhanced GPWS (Ref. AMM TASK 34-48-00-740-002).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message:
FCU (3CA) BUS CP-L/GPWC (1WZ)
- replace the GPWC (1WZ) (Ref. AMM TASK 34-48-34-000-001) and (Ref. AMM TASK 34-48-34-400-001).
(1) If the fault continues:
- do a check and repair the wiring of the FCU 1 DATA INPUT bus from the GPWC to the first terminal block: for pins AB/12A, 12B of the GPWC (Ref. ASM 34-48/02).
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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 267
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 3(86)
