A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备1(71)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Wall Panel and Partition Panel
 25-00-00-340-020  Patches and Filler Repair Method (Damage Through) -
All Cargo Compartment Linings with Honeycomb Core
 25-00-00-340-021  Speed Patch Repair Method (Damage not Through) - All
 Cargo Compartment Linings with Honeycomb Core
 25-00-00-340-022  Speed Patches and Filler Repair Method (Damage
 Through) - All Cargo Compartment Linings with
 Honeycomb Core, but not Ceiling Panels
 25-00-00-340-023  Patches, Filler and Rivets Repair Method (Damage
 Through) - All Cargo Compartment Linings with
 Honeycomb Core
 25-00-00-340-025  Speed Patches and Filler Repair Method (Damage not
 Through) - All Cargo Compartment Linings with
 Honeycomb Core
 25-00-00-340-026  Stainless Steel-Patch Repair Method (Damage not
 Through) - All Cargo Compartment Linings with
 Honeycomb Core
 25-00-00-340-028  Speed Patch and Filler to the Edge Repair Method
 (Damage Not Through from the Edge) - All Cargo
 Compartment Linings with Honeycomb Core
 25-00-00-340-029  Protection of Cargo Compartment Linings with S-Glass
 Patch - All Cargo Compartment Linings with Honeycomb
 Core
 25-54-11-000-001  Removal of the FWD Cargo-Compartment Partition FR24
 25-54-11-400-001  Installation of the FWD Cargo-Compartment Partition
 FR24
 25-54-12-000-001  Removal of the FWD Cargo Compartment Partition FR34
 25-54-12-000-002  Removal of the Ceiling Panels in the FWD Cargo
 Compartment
 25-54-12-000-003  Removal of the Sidewall Panels in the FWD Cargo
 Compartment
 25-54-12-400-001  Installation of the FWD Cargo Compartment Partition
 FR34
 25-54-12-400-002  Installation of the Ceiling Panels in the FWD Cargo
 Compartment

R
 CES  -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

25-54-12-400-003
25-55-11-000-001 25-55-11-000-002
25-55-11-000-003
25-55-11-400-001
25-55-11-400-002
25-55-11-400-003
25-55-12-000-001 25-55-12-000-002
25-55-12-000-003
25-55-12-400-001
25-55-12-400-002
25-55-12-400-003
52-30-00-860-001
52-30-00-860-002
53-43-11-000-001 53-43-11-400-001 AMM 11-35-25 P.Block 001 AMM 11-36-25 P.Block 001 ASRM 53-02-00-208 ASRM 532300 ASRM 534300 25-00-00-991-048 25-00-00-991-033 25-00-00-991-034 25-00-00-991-035 25-00-00-991-027 Installation of the Sidewall Panels in the FWD Cargo CompartmentRemoval of the AFT Cargo-Compartment Partition FR47Removal of the Ceiling Panels in the AFT Cargo Compartment - FR47/FR59Removal of the Sidewall Panels in the AFT Cargo Compartment - FR47/FR59Installation of the AFT Cargo-Compartment Partition FR47Installation of the Ceiling Panels in the AFT Cargo Compartment -FR47/FR59Installation of the Sidewall Panels in the AFT Cargo Compartment - FR47/FR59Removal of the AFT Cargo Compartment Partition FR65Removal of the Ceiling Panels in the AFT Cargo Compartment - FR59/FR65Removal of the Sidewall Panels in the AFT Cargo Compartment - FR59/FR65Installation of the AFT Cargo Compartment Partition FR65Installation of the Ceiling Panels in the AFT Cargo Compartment - FR59/FR65Installation of the Sidewall Panels in the AFT Cargo Compartment - FR59/FR65Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpClose the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpRemoval of the Support StrutsInstallation of the Support Struts
Fig. 818Fig. 819Fig. 820Fig. 821Fig. 822
 EFF : ALL 25-00-00Page A804

Aug 01/05
R
 CES  3. Job Set-up

__________ Subtask 25-00-00-861-082
 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 Subtask 25-00-00-010-083
 B. Get Access
 (1)
 Open the related cargo compartment door (Ref. TASK 52-30-00-860-001).

 (2)
 Put the ACCESS PLATFORM 2M (6 FT) in position.

 4. Procedure
_________ Subtask 25-00-00-910-052
 A. General Information NOTE : The repair of decompression panel flanges and floor panel are not
____
 includet in this procedure.

 (1)
 For the repair of the decompression panel flange (Ref. TASK 25-00-00-340-003)

 (2)
 For the protection procedure of the cargo compartment linings (S-glass protection patch on the view side):

 (Ref. Fig. 818/TASK 25-00-00-991-048)
　
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