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25-10-00Page 1
Aug 01/04
COCKPIT - REPAIRS
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TASK 25-10-00-330-001 Repair of the Flight-Compartment Ceiling Panels
1.
Reason for the Job
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Self Explanatory
2.
Job Set-up Information
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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
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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 | -------------------------------------------------------------------------------
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Flight-Compartment Ceiling Panels
Figure 801/TASK 25-10-00-991-001
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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
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