「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 248
Feb 01/03R
CES Ground Proximity Warning System Inoperative
1. Possible Causes
_______________
- GPWC (1WZ)
- wiring of the ILS DATA INPUT bus from the GPWC (1WZ) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 34-36-00-740-002 BITE Test of the ILS
AMM 34-36-00-740-003 BITE Test of the MMR
AMM 34-48-34-000-001 Removal of the GPWC (1WZ)
AMM 34-48-34-400-001 Installation of the GPWC (1WZ)
ASM 34-48/01
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
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PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU EIS/GPWS/115VAC 3WZ P07
R **ON A/C 001-049, 051-060, 101-104,
B. Test
(1) Do the BITE test of the ILS (system 1) (Ref. AMM TASK 34-36-00-740-002).
**ON A/C ALL
R Post SB 34-1147 For A/C 001-004,051-060,
R Post SB 34-1189 For A/C 001-049,051-060,101-104,
B. Test
(1) Do the BITE test of the MMR (system 1) (Ref. AMM TASK 34-36-00-740-003).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 249
May 01/05 CES 4. Fault Isolation
_______________
A. If the test gives a maintenance message: R - do the trouble shooting procedure related to the maintenance message.
B. If there is no fault:
- 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 ILS DATA INPUT bus from the GPWC (1WZ) to the first terminal block (Ref. ASM 34-48/01).
C. Do the test given in Para. 3.
Continuous Inhibition of the Flap Condition
1. Possible Causes
_______________
- wiring of the FLAPS discrete from the GPWC (1WZ) to the GPWS/FLAP MODE pushbutton switch (7WZ)
- P/BSW-GPWS/FLAP MODE (7WZ)
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 ASM 34-48/01
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. Do the procedure: - on the GPWS section of panel 21VU, make sure that the GPWS/FLAP MODE pushbutton switch (7WZ) is not pushed (OFF legend is off)
- on the center pedestal, on the panel 114VU, put the flap and slat control lever in the 0 position
- make sure that there is no ground at pin AB/9C of the GPWC (1WZ).
(1) If there is ground:
- do a check for a short to ground at the wiring of the FLAPS discrete from the GPWC (1WZ) to the GPWS/FLAP MODE pushbutton switch (7WZ) : pin A/B1 (Ref. ASM 34-48/01).
(a) If the fault continues:
- replace the P/BSW-GPWS/FLAP MODE (7WZ) (Ref. AMM TASK 33-10-00-000-002) and (Ref. AMM TASK 33-10-00-400-002).
「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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 251
May 01/03R
CES Inhibition of the Flap Condition not Possible
1. Possible Causes
_______________
- wiring of the GPWS/FLAP MODE pushbutton switch (7WZ)
- P/BSW-GPWS/FLAP MODE (7WZ)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 3(81)
