(Ref. Fig. 401/TASK 71-22-11-991-300) Subtask 71-22-11-020-051
A. Removal of the Aft Engine Mount. NOTE : Removal of the hardware that attach the aft engine mount to the
____
engine is the same at the three engine flanges.
(1) Remove the retaining pin (5) from the bolt (15).
(2) Remove the bolts (30), washers (35), (50). and nuts (55) that attach the retainers (60) and (70) to bracket (40).
(3) Remove the retainers (60) and (70) from engine.
(4) Remove the spanner nuts (65) and (75) from the bolt (10) and the pin (15).
(5) Remove the bolt (10) from the pin (15).
(6) Remove the pin (15), and the brackets (20) and (40) from the engine flange.
(7) Disengage the link assemblies from the engine flanges and remove the engine mount (85) from the engine.
(8) Remove the bushing (25), (45), and the shoulder bushing (80) from the engine flanges.
Subtask 71-22-11-480-052
B. Installation of the AFT ENGINE MOUNT ANTI GOUGE SPLINTS.
(1) Put the top slint assemblies (larger) on the outside of the aft engine mount links.
NOTE : The end of the splint assembly marked TOP must touch the beam
____ assembly. The other end marked BOTTOM must touch the links.
(2) Put the bottom splint (smaller) on the inside of the aft engine mount links.
F 『 EEFF : ALL E Page 40271-22-11
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Aft Engine Mount
Figure 401/TASK 71-22-11-991-300
F 『 EEFF : ALL E Page 40371-22-11
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(3) Attach the SPLINT - ENGINE MOUNT AFT (RSE1224) to the engine mount two places with TY WRAP.
(a) Wind the TY WRAP around the splints and the aft mount where the splint touches the beam assembly.
(b) Wind the TY WRAP around the splints and the aft mount where the splint touches the link.
(c) Make sure that the TY WRAP is wound very tight and that the splints can not move.
F 『 EEFF : ALL E Page 40471-22-11
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TASK 71-22-11-400-041
Installation of the Aft Engine Mount
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific Torque Wrench : range 8.00 to 75.00 lbf.ft
(1.00 to 10.00 m.daN)
No specific Torque Wrench : range 15.00 to 150.00 lbf.ft
(2.00 to 20.00 m.daN) R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN)
RSE1098 1 WRENCH SET - AFT ENGINE MOUNT
RSE1224 2 SPLINT - ENGINE MOUNT AFT
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. CP5063 *
Silicone Lubricant (Ref. 70-30-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-21-11-911-001 Tightening Torques for Standard Threaded Fasteners 71-00-00-000-042 Removal of the Power Plant 71-00-00-400-042 Installation of the Power Plant 71-22-11-991-300 Fig. 401
F 『 EEFF : ALL E Page 40571-22-11
E E May 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
3. Job Set-up
__________
Subtask 71-22-11-860-050
A. Make sure that the engine is removed (Ref. TASK 71-00-00-000-042)
Subtask 71-22-11-080-052
B. Remove the SPLINT - ENGINE MOUNT AFT (RSE1224) from the aft engine mount.
4. Procedure
_________
(Ref. Fig. 401/TASK 71-22-11-991-300)
Subtask 71-22-11-420-051
A. Installation of the Aft Engine Mount. CAUTION : INSTALL THE BUSHING (80) WITH ITS SHOULDER AT THE INTERIOR OF
_______
THE ENGINE RANGE.
NOTE : Installation of the hardware that attach the aft engine mount to 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM 動力裝置 POWER PLANT 2
