R **ON A/C ALL
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message: GPWS SYS PB SW (9WZ)/GPWC (1WZ): - on the GPWS section of panel 21VU, make sure that the GPWS/SYS
pushbutton switch (9WZ) is not pushed (the OFF legend is off)
- do a check for ground at pin AB/7D of the GPWC (Ref. ASM 34-48/01).
(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).
(2) If there is ground:
- replace the P/BSW-GPWS/SYS (9WZ) (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 INHIBIT ALL MODE discrete from the GPWC (1WZ) to the GPWS/SYS pushbutton switch (9WZ) (Ref. ASM 34-48/01).
B. Do the test given in Para. 3.
Incorrect Flaps Signal
1. Possible Causes
_______________
- GPWC (1WZ)
- SFCC-1 (21CV)
- P/BSW-GPWS/FLAP MODE (7WZ)
- P/BSW-GPWS/LDG FLAP 3 (13WZ)
- wiring of the GPWS/LDG FLAP 3 pushbutton switch (13WZ)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV)
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 34-48/01
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:
GPWS FLP MODE PB SW (7WZ)/SFCC (21CV)/GPWC (1WZ)
- on the GPWS section of panel 21VU:
. make sure that the GPWS/FLAP MODE pushbutton switch (7WZ) is not
pushed (the OFF legend is off).
. make sure that the GPWS/LDG FLAP 3 pushbutton switch (13WZ) is not
pushed (the ON legend is off).
- on the center pedestal, on the panel 114VU, put the flap and slat control lever in the 0 position
- do a check for ground at pin AB/9C of the GPWC (1WZ).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 215
Aug 01/02R CES
(1) If there is ground:
- 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).
(2) If there is no ground:
- put the flap and slat control lever in the FULL position
- do a check for ground at pin AB/9C of the GPWC (1WZ).
(a) If there is ground:
- replace the GPWC (1WZ) (Ref. AMM TASK 34-48-34-000-001) and (Ref. AMM TASK 34-48-34-400-001).
(b) If there is no ground:
- replace the SFCC-1 (21CV) (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
1_ If the fault continues:
- replace the P/BSW-GPWS/LDG FLAP 3 (13WZ) (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 GPWS/LDG FLAP 3 pushbutton switch (13WZ): . pin A/B3 to GPWC (1WZ) pin AB/9C . pin A/B2 to SFCC1 (21CV) pin AB/8B (Ref. ASM 34-48/01).
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 ∞∞34-48-00∞∞∞∞∞∞∞∞∞∞Page 216
Aug 01/02R
CES Loss of Glide Slope Visual and Aural Warnings and/or Continuous Self-Test Operation
1. Possible Causes
_______________
- GPWC (1WZ)
- P/BSW - GPWS/G/S (4WZ)
- P/BSW - GPWS/G/S (5WZ) 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(70)
