Left-Wing Leading-Edge Pressure-Relief Panel Open

TASK 36-14-00-810-807-A
Left-Wing Leading-Edge Pressure-Relief Panel Open

1. Possible Causes

2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TSM TASK 36-22-00-810-801-A	Air Leak in the Left Wing
AMM 57-41-37-350-001	Repair to the Leading Edge Pressure-Relief Panel After it has Operated
AMM 57-41-37-350-002	Repair to the Leading Edge Pressure-Relief Panel After it has Operated
AMM 57-41-37-350-003	Repair to the Leading Edge Pressure-Relief Panel After it has Operated
AMM 57-41-37-350-004	Repair to the Leading Edge Pressure-Relief Panel After it has Operated
AMM 57-41-37-350-005	Repair to the Leading Edge Pressure-Relief Panel After it has Operated

3. Fault Confirmation
Subtask 36-14-00-700-056-A ** ON A/C NOT FOR ALL

A. Not applicable. No confirmation test is necessary.

4. Fault Isolation
Subtask 36-14-00-810-056-A ** ON A/C NOT FOR ALL

A. Maintenance Procedure
(1) Do these steps:
(a) Do the applicable procedure for the repair of the leading edge pressure-relief panel AMM 57-41-37-350-001 or AMM 57-41-37-350-002 or AMM 57-41-37-350-003 or AMM 57-41-37-350-004 or AMM 57-41-37-350-005.
(b) Do the procedure for an air leak in the left wing (Ref. TSM TASK 36-22-00-810-801).
(c) After the subsequent flight, make sure the fault does not continue.

5. Close-up
Subtask 36-14-00-860-061-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.

[Rev.8 from Aug 2018] 2026.04.04 04:34:01 UTC