(5) Do the functional test of the ADM for the CAPT (F/O) circuit (Ref. AMM TASK 34-11-00-720-001).
(a) If one pressure value is different, replace the defective ADM (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
(b) If the pressure values are the same, replace the AOA sensor 1(2) (3FP1(2)) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(6) If the fault continues:
- Do a check to make sure that there are no impacts on the fuselage around the AOA sensors, the static probes and the ADMs (Ref. SRM 530011P.BLOCK101).
B. If the test shows a different altitude value from the ADR3 (compared to the ADR1 and the ADR2):
- do a visual check of the static probes.
R (1) If one static probe is damaged, replace it (Ref. AMM TASK 34-11-16-R 000-001) and (Ref. AMM TASK 34-11-16-400-002).
(2) Make sure that the small wing of the AOA sensor 3 (3FP3) is not damaged and that the mechanism moves freely.
R (a) If the AOA sensor 3 (3FP3) is damaged, replace it (Ref. AMM TASK R 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(b) If the AOA sensor 3 (3FP3) is not damaged:
- do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002)
- connect the ARINC Reader to the test connector 199VC on the panel 187VU (Ref. ASM 34-13/01)
- manually turn the AOA sensor 3 (3FP3) to the down position
- manually turn the AOA sensor 3 (3FP3) to the up position
- compare the AOA values (between -35 deg. and -34.5 deg. for the down position and between +84.5 deg. and +85 deg. for the up position) read on label 221:
ADIRU 3 199VC 3FP3 pins y, z
1 If one value is different:
_
- replace the AOA sensor 3 (3FP3) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(3) Do the draining and flushing of the standby static and the standby total pressure line of the Air Data Module (19FP8) (Ref. AMM TASK 34-10-00-170-003).
(4) Do the leak test of the standby circuits (Ref. AMM TASK 34-21-00-790-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-203, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page B241
May 01/05 CES
(5) Do the functional test of the ADM for the standby circuit (Ref. AMM TASK 34-11-00-720-001).
(a) If one pressure value is different, replace the defective ADM (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
(b) If the pressure values are the same, replace the AOA sensor 3 (3FP3) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(6) If the fault continues:
- Do a check to make sure that there are no impacts on the fuselage around the AOA sensor 3, the ADMs and the static probes (Ref. SRM 530011P.BLOCK101).
R **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
A. If the test shows a different altitude value from the ADR1 (compared to the ADR2 and ADR3) or from the ADR2 (compared to the ADR1 and ADR3):
- do a visual check of the static probes.
(1) If one static probe is damaged, replace it (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).
(2) Make sure that the small wing of the AOA sensor 1(2) is not damaged and that the mechanism moves freely.
(a) If one AOA sensor is damaged, replace it (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(3) Do the flushing of the static pressure line of the Air Data Module (ADM 19FP4 and 19FP5 or 19FP6 and 19FP7) (Ref. AMM TASK 34-10-00-170-002).
(4) Do the leak test of the main Air Data System (Ref. AMM TASK 34-13-00-790-002).
(5) Do the functional test of the ADM for the CAPT (F/O) circuit (Ref. AMM TASK 34-11-00-720-001).
(a) If one pressure value is different, replace the defective ADM (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
(b) If the pressure values are the same, replace the AOA sensor 1(2) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
「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 ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page B242
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 2(8)
