Failure of the Pressure Transducer of the R Static Pressure ADM or of the L Static Pressure ADM

TASK 34-11-00-810-902-A
Failure of the Pressure Transducer of the R Static Pressure ADM or of the L Static Pressure ADM

1. Possible Causes

2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
AMM 34-11-16-000-001	Removal of the Static Probe
AMM 34-11-16-400-002	Installation of the Static Probe

3. Fault Confirmation
Subtask 34-11-00-700-060-A ** ON A/C NOT FOR ALL

A. Test
Not applicable, you cannot confirm this fault on the ground.

4. Fault Isolation
Subtask 34-11-00-810-232-A ** ON A/C NOT FOR ALL

A. If the POST FLIGHT REPORT gives the maintenance message ADM4/5 (19FP4/5):

(1) If one static probe is damaged:

replace the defective static probe AMM 34-11-16-000-001 and AMM 34-11-16-400-002.

(2) If the static probes are not damaged:

do a check and repair the aircraft wiring between ADIRU1 pins AA/8D, 8E and ADM4 pins A/G, H
do a check and repair the aircraft wiring between ADIRU1 pins AA/9D, 9E and ADM5 pins A/G, H.

[Rev.8 from Aug 2018] 2026.04.04 04:32:19 UTC