(5)
Remove the lockwasher (25) and discard it.
(6)
Remove the sleeve (24) with the extractor PYLON SHAFT EXTRACTOR RIB 4/RIB 10 (98D54003005000). Remove the sleeve at the bottom first.
(7)
Remove the shackles (29). NOTE : Increase the upper force continuously and equally until you
____
can remove the sleeve.
INTENTIONALLY BLANK
R 1 1
54-51-17Page 409
1 1 May 01/03 1 1 1CES 1
R R Forward Pylon-to-Wing Attach Fitting Figure 404/TASK 54-51-17-991-005- 12 (SHEET 1)
1EFF : 1 1 1CES ALL 1 111 54-51-17 Page 410 May 01/03
R R Forward Pylon-to-Wing Attach Fitting Figure 404/TASK 54-51-17-991-005- 22 (SHEET 2)
1EFF : 1 1 1CES ALL 1 111 54-51-17 Page 411 May 01/03
TASK 54-51-17-400-001
Installation of Pylon-to-Wing Forward Attach Fitting at RIB4
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
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)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 cotter pins 36-11-05 07A-160
3 ring-retainer 28-21-06 01 -110
4 ring-retainer 28-21-06 01 -180
11 O-ring 28-21-06 01 -100
14 O-ring 28-21-06 01 -170
15 O-rings 28-21-06 01 -070
25 lockwashers 54-51-17 01 -050
26 nuts 54-51-17 01 -040
28 cotter pins 54-51-17 01 -010
28 cotter pins 54-51-17 01 -010A
28 cotter pins 54-51-17 01 -010B
28 cotter pins 54-51-17 01 -010C
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
07-11-00-586-002 Lowering of the Aircraft for Maintenance Operations 28-00-00-910-001 Fuel Safety Procedures 71-00-00-400-042 Installation of the Power Plant 71-13-11-400-040 Installation of the Fan Cowl Doors 78-32-11-400-040 Installation of the Left or Right Half Door of Thrust
Reverser 54-51-17-991-001 Fig. 401 54-51-17-991-012 Fig. 402 54-51-17-991-003 Fig. 403 54-51-17-991-005 Fig. 404
3. Job Set-up
__________
Subtask 54-51-17-860-052
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engine.
1EFF : ALL 1 54-51-17Page 413 1 1 May 01/03R 1 1 1CES 1
(2)
Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3)
On the overhead 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 1(2).
(4)
Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you do work on the fuel system.
4. Procedure
_________
Subtask 54-51-17-160-050
A. Preparation before Installation
(Ref. Fig. 404/TASK 54-51-17-991-005)
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM NACELLES/PYLONS(54)
