Repair of the Flight-Compartment Rear Panels

TASK 25-10-00-330-003-A
Repair of the Flight-Compartment Rear Panels

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TASK 25-00-00-330-002-A	Repairs of Non-structural Components (not in the Cargo Compartments)
TASK 25-00-00-330-003-A	Repairs of Surface Damage of Composite Components (not in the Cargo Compartments)
Flight-Compartment Rear Panels

3. Job Set-up
Subtask 25-10-00-010-052-A

A. Removal of the Rear Panels
(1) If necessary, remove the panel from the aircraft.
(2) List of the rear/panels.

Flight-Compartment Rear Panels

ITEM	PANEL IDENT	DESCRIPTION	MATERIAL	IPC CROSS REF.
1	212JW	PANEL-UPPER	Foam	25130119
2	212HW	PANEL ASSY-SIDE	Sandwich	25130119
3		PANEL ASSY	Laminate	25130112
4		PANEL ASSY-SIDE	Sandwich	25130122
5		PANEL-FRONT	Sandwich	25130122
6		PANEL ASSY-SIDE	Sandwich	25130122
7		PANEL ASSY	Sandwich	25130113
8	212KW	PANEL ASSY	Sandwich	25130112

4. Procedure
Subtask 25-10-00-330-052-A

A. Damage to the Lining Panel
(1) Superficial Damage
(a) If the damage diameter is less than or equal to 50 mm (1.9685 in.) and if the honeycomb core is not damaged, do the repair of the panel (Ref. AMM TASK 25-00-00-330-003).
(2) Significant Damage
(a) If the honeycomb core is damaged and/or if the damage diameter is more than 50 mm (1.9685 in.) or if the honeycomb structure is debonded, do the repair of the panel (Ref. AMM TASK 25-00-00-330-002).

5. Close-up
Subtask 25-10-00-410-052-A

A. Installation of the Rear Panels
(1) If necessary, install the panels in the aircraft.

[Rev.10 from 2021] 2026.03.31 23:27:41 UTC