-
there is no damage
-
there is no corrosion
-
there are no cracks or scores
-the surface protection is in the correct condition.
(2)
Do an inspection of the drive strut, the tab forward link and the tab rear link. Make sure that:
-
there is no damage
-
there is no corrosion
-they are attached correctly.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____
correct repair procedure.
1EFF : 301-399, 1 57-53-00Page B637 1 1 Nov 01/04R 1 1 1CES 1
Outboard Flap - Tab Articulation at Track 4 - Inspection Area
Figure 635/TASK 57-53-00-991-039
5. Close-up
________ Subtask 57-53-00-410-085
A. Close Access
(1)
Remove the spark-proof lamp from the inspection area.
(2)
Install the applicable flap track fairing (Ref. TASK 57-55-11-400-004):
-
for the left wing, install 533AT, 533CB
-
for the right wing, install 633AT, 633CB.
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 57-53-00-865-132
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-075
C. Close Access
(1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-53-00-942-089
D. Removal of Equipment
(1)
Remove the access platform(s).
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
TASK 57-53-00-220-019
Special Detailed Inspection of Outboard Double Slotted Flap, Tab Articulation at Track 4, LH/RH
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Refer to the MPD TASK: 575341-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific spark-proof lamp No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and
4 ASRM 575300 (for corrective action) NTM 575341 PART 9 (for corrective action) 57-53-00-991-040 Fig. 636
3. Job Set-up
__________
Subtask 57-53-00-941-093
A. Safety Precautions
(1)
Put a warning notice on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
(2)
Put the safety barriers in position.
Subtask 57-53-00-860-076
B. Aircraft Maintenance Configuration
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM WINGS 機(jī)翼5(25)
