Pylon-to-Engine Attach Fitting Figure 608/TASK 54-51-00-991-005
1EFF : 1 1R 1CES ALL 1 11 1 54-51-00 Page 641 Aug 01/99
(2) Make sure that there is no:
R R R (a) Corrosion damage: - If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200-P.Block001) for types of corrosion, inspection, removal and corrosion protection.
R R R (b) Other damage (cracks, scratches, stress, marks dents, bumps,...): - If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100-P.Block001) for damage classification and associated corrective action.
5. Close-up________
Subtask 54-51-00-440-057
A. Aircraft Maintenance Configuration
(1) Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
Subtask 54-51-00-410-056
B. Close Access
R (1) Close the thrust reverser doors (Ref. TASK 78-36-00-410-040). FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
R (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-040). FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
(3) Make sure that the work area is clean and clear of tool(s) and other items.
(4) Remove the access platform(s).
(5) Remove the warning notice(s).
TASK 54-51-00-200-006
R Detailed Inspection of Pylon to Wing Attach Fitting Lugs at RIB 4
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.
1. Reason for the Job
__________________
Refer to the MPD TASK: 545114-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice R No specific access platform 2.5 m (8 ft. 2 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
78-30-00-081-041 78-30-00-481-041 SRM 511100-P.Block001 SRM 512200-P.Block001 54-51-00-991-006 Make the Thrust Reverser Serviceable after MaintenanceMake the Thrust Reverser Unserviceable for MaintenanceFig. 609
3. Job Set-up__________
Subtask 54-51-00-941-057
A. Safety Precautions
R (1) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overheat maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-056
B. Get Access
R (1) Put an access platform in position.
R (a) At the zone 410 for the left pylon.
R (b) At the zone 420 for the right pylon.
(2) Remove the access panels: 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 NACELLES/PYLONS(30)
