EFF : ALL

25-10-00Page 1
Aug 01/04

 COCKPIT - REPAIRS
_________________
 TASK 25-10-00-330-001 Repair of the Flight-Compartment Ceiling Panels
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-00-00-330-002 Repairs to Nonstructural Components (not in the Cargo Compartments) 25-00-00-330-003 Repairs to Surface Damage of Composite Components
 (not in the Cargo Compartments) 25-13-41-000-001 Removal of the Ceiling Panels 25-13-41-400-001 Installation of the Ceiling Panels 25-10-00-991-001 Fig. 801
 3. Job set up
__________ Subtask 25-10-00-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU LIGHTING/EMER LT/CKPT/DOME 1LE H08 122VU LIGHTING/CKPT/DOME 3LE Y06
 EFF : ALL

25-10-00Page 801

 Subtask 25-10-00-010-050
 B. Removal of the Ceiling Panels
 (1)
 If necessary remove the panel from the aircraft (Ref. TASK 25-13-41-000-001).

 (2)
 List of the ceiling panels.
 (Ref. Fig. 801/TASK 25-10-00-991-001)

 -------------------------------------------------------------------------------
|PANEL | | | IPC | ITEM|IDENT | DESCRIPTION | MATERIAL | CROSS REF. | REMARKS -------------------------------------------------------------------------------
1 |211GC | COVER ASSY | Laminate | 25130103 |Non repairable -------------------------------------------------------------------------------2 |211HC | PANEL ASSY | Sandwich | 25130103 | -------------------------------------------------------------------------------3 |211JC | PANEL ASSY | Sandwich | 25130101 | -------------------------------------------------------------------------------4 |211FC | PANEL ASSY | Sandwich | 25130101 | |212FC | PANEL ASSY | Sandwich | 25130102 |
 -------------------------------------------------------------------------------5 |211EC | DOOR ASSY | Laminate | 25130101 | Non repairable |212EC | DOOR ASSY | Laminate | 25130102 | Non repairable -------------------------------------------------------------------------------
6 |211DC | PANEL ASSY | Joggling | 25130101 | |212DC | PANEL ASSY | Joggling | 25130102 | -------------------------------------------------------------------------------7 |211CC | PANEL ASSY | Joggling | 25130101 | |212CC | PANEL ASSY | Joggling | 25130102 | -------------------------------------------------------------------------------8 |211BC | PANEL ASSY | Sandwich | 25130101 | |212BC | PANEL ASSY | Sandwich | 25130102 | -------------------------------------------------------------------------------9 |211AC | PANEL ASSY | Sandwich | 25130101 | |212AC | PANEL ASSY | Sandwich | 25130102 | -------------------------------------------------------------------------------
EFF : ALL

25-10-00Page 802

 Flight-Compartment Ceiling Panels
 Figure 801/TASK 25-10-00-991-001
 EFF :  ALL  25-10-00 Page 803 
Feb 01/98
 CES 

 4. Procedure
_________ Subtask 25-10-00-330-050
 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. 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. TASK 25-00-00-330-002).
 5. Close up
________ Subtask 25-10-00-410-050
 A. Installation of the Ceiling Panels
 (1) If necessary, install the panel in the aircraft (Ref. TASK 25-13-41-400-001).
 Subtask 25-10-00-865-051
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備1(92)