Slats Command Sensor Unit Failure

TASK 27-81-00-810-820-A
Slats Command Sensor Unit Failure

1. Possible Causes

CSU [51CV]

2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TSM TASK 27-51-00-810-828-A	Flaps Command Sensor Unit Failure

3. Fault Confirmation
Subtask 27-81-00-710-057-A

A. Procedure.
(1) This fault has locked the wing tip brakes of the slat and flap system, no fault confirmation is necessary.
(a) Do the fault isolation.

4. Fault Isolation
Subtask 27-81-00-810-069-A

A. Procedure.
(1) The cause of this fault is CSU [51CV] do (Ref. TSM TASK 27-51-00-810-828)

[Rev.8 from Aug 2018] 2026.04.04 04:27:48 UTC