(2) Put the aft engine mount (85) on the engine and engage the link assemblies with the engine flanges.
R (3) Apply Silicone Lubricant (Material No. CP5063) to the bolt (10) and the pin (15).
(4) Install the pin (15), and the brackets (20) and (40) on the engine flange.
(5) Put the bolt (10) into the pin (15).
(6) Install the spanner CAUTION : USE OF THE SPANNER WRENCHES AS A TORQUE WRENCH ADAPTER WILL
_______ CHANGE THE TORQUE VALUE WHICH IS REALLY APPLIED. THE EFFECTIVE LENGHT OF THE SPANNER WRENCHES ARE: RSE1098-1 : 6-INCHES (152.4 MM) RSE1098-5 : 8-INCHES (203.2 MM)
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NOTE : To find the correct TORQUE value when spanner wrenches are
____ used refer to the formula in standard practices (Ref. TASK 20-21-11-911-001).
(a) Install the spanner nut (75) on the pin (15).
(7) TORQUE the spanner nut (75) to 80 lbf.ft (10.84 m.daN) minimum. Use WRENCH SET - AFT ENGINE MOUNT (RSE1098-5) to adapt torque wrench to the spanner nut.
(8) Install the spanner nut (65) on the bolt (10).
(9) TORQUE the spanner nut (65) to 35 lbf.ft (4.74 m.daN) minimum. Use WRENCH SET - AFT ENGINE MOUNT (RSE1098-1) to adapt the torque wrench to the spanner nut.
(10) Put the retainers (70) and (60) against the bracket (40) to make sure the bolt holes are aligned.
(11) If the holes are not aligned, increase the torque on the spanner nuts
(65) and (75) to align the holes.
NOTE : Do not torque the nut (75) more than to 95 lbf.ft (12.88
____ m.daN) or the nut (65) more than to 42 lbf.ft (5.69 m.daN)
(12) If the holes are aligned, install the bolts (30), the washers (35) , (50), and the nuts (55).
NOTE : Make sure that you put the countersunk washers under the bolt
____
heads.
(13) TORQUE nuts (55) to between 24 and 27 lbf.in (0.27 and 0.30 m.daN).
(14) Install the retaining pin (5) through the pin (15).
5. Close-up
________ Subtask 71-22-11-410-050
A. Install the engine (Ref. TASK 71-00-00-400-042)
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Removal of the Aft Engine Mount Without Engine Removal
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific rubber mat No specific warning notice No specific access platform 1 m (3 ft. 3 in.) S487ETT2 1 ENGINE TROLLEY S686CR56-5 1 ENGINE CRADLE 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 98D71203500000 1 BOOTSTRAP SYSTEM
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 71-22-11-991-300 Fig. 401 71-22-11-991-302 Fig. 402 71-22-11-991-303 Fig. 403 71-22-11-991-304 Fig. 404
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3. Job Set-up
__________ Subtask 71-22-11-941-055
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.
(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) Make sure that the slats are retracted and install TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap and slat control lever. 中國(guó)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(cè) AMM 動(dòng)力裝置 POWER PLANT 2(2)
