(3)
Do a visual check of the inspection area for damage or discontinuities.
(4)
Make sure that there is no:
(a)
Corrosion damage:
-If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block 001) for types of corrosion, inspection, removal and corrosion protection.
(b)
Other damage (cracks, scratches, stress, marks, dents, bumps...):
-If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
R Engine Forward Mount-Fitting and Spigot Fitting - Inspection Areas Figure 602/TASK 54-51-00-991-057
1EFF : ALL 1 54-51-00Page 606 1 1 Aug 01/03 1 1 1CES 1
4. Procedure
_________
Subtask 54-51-00-250-051
A. Inspection (Ref. Fig. 602/TASK 54-51-00-991-057)
(1) Do a special detailed inspection of the internal structure of the forward mount fitting and the spigot fitting (Ref. NTM 545101,P.Block-601).
R R NOTE : Do the full procedure for one hole, then do it again for each____ hole.
(2) Make a report of damage after NDT inspection:
(a) Corrosion damage: - If you find damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block 001) for types of corrosion, inspection, removal and corrosion protection.
(b) Other damage (cracks, scratches, stress, marks, dents, bumps...): - If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
5. Close-up________
R Subtask 54-51-00-420-065
R A. Installation of the Components
R R (1) Install the bolt (1) with SPECIAL MATERIALS (Material No. 05-047), the washer (2) and the nut (3).
R R NOTE : Do the full procedure for one hole and then, do it again for____ each hole.
R R (2) TORQUE the nut (3) to between 14 and 16 m.daN (103.24 and 117.99 lbf.ft).
Subtask 54-51-00-440-051
R B. Aircraft Maintenance Configuration
(1) Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
Subtask 54-51-00-410-050
R C. Close Access
(1)
Close the thrust reverser doors (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
(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 54-51-00-200-002
R Special Detailed Inspection of Engine Forward Mount Fitting, End of Lower Arms, R Aft of RIB 1, Forward and Aft Attachment Bolt Holes
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: 545102-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 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)
中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM NACELLES/PYLONS(22)
