DOC AIRBUS | AMM A320F57-31 MAIN STRUCTURE
- PB.401 MAIN STRUCTURE - DEACTIVATION/REACTIVATION
-
57-31-00-040-001-A
[10]
Deactivation of the Wing-Tip Fence -
57-31-00-440-001-A
[10]
Reactivation of the Wing-Tip Fence
-
57-31-00-040-001-A
[10]
- PB.601 MAIN STRUCTURE - INSPECTION/CHECK
-
57-31-00-220-801-A
[10]
Detailed Inspection of Wing Tip, RIB 27 Lugs -
57-31-00-220-803-A
[10]
Detailed Inspection of Wing Tip, Sharklet, RIB 27A, Bottom Flange Forward -
57-31-00-220-804-A
[10]
Detailed Inspection of Wing Tip, Sharklet, RIB 27A Lugs -
57-31-00-280-801-A
[10]
Special Detailed Inspection (ENDOSCOPE) of Wing Tip, Sharklet Internal Structure from RIB 27A to Spar Splice Brackets Outboard of MID RIB 3
-
57-31-00-220-801-A
[10]
- PB.401 STRUCTURE COMPLETE - WING TIP - REMOVAL/INSTALLATION
-
57-31-21-000-001-A
[10]
Removal of the Wing-Tip Structure -
57-31-21-400-001-A
[10]
Installation of the Wing-Tip Structure
-
57-31-21-000-001-A
[10]
- PB.401 FENCE - WING TIP - REMOVAL/INSTALLATION
-
57-31-22-000-001-A
[10]
Removal of the Wing-Tip Fence -
57-31-22-400-001-A
[10]
Installation of the Wing-Tip Fence
-
57-31-22-000-001-A
[10]
- PB.401 SHARKLET - REMOVAL/INSTALLATION
-
57-31-23-000-801-A
[10]
Removal of the Sharklet -
57-31-23-400-801-A
[10]
Installation of the Sharklet -
57-31-23-000-802-A
[10]
Removal of the Sharklet Access Panels -
57-31-23-400-802-A
[10]
Installation of the Sharklet Access Panels
-
57-31-23-000-801-A
[10]