(7)
 Remove the vibration isolator (10) from the APU mount-bracket (11).

 (8)
 If necessary remove the tie-rods (12) and/or (13).

 (a)
 Remove the nuts (14), the washers (17) and the screws (16).

 (b)
 Disconnect the bonding straps (15).

 (c)
 Remove and discard the cotter pins (20).

 (d)
 Remove the castle nuts (19), the washers (18) and the bolts (21).

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-53Page 403 201-210, Config-2 Aug 01/05
 CES

 AFT Tie-Rods and Vibration Isolator
 Figure 401/TASK 49-12-53-991-003

 CES

 (e) Remove the tie-rods (12) and/or (13).

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-53Page 405 201-210, Config-2 Aug 01/05
 CES  TASK 49-12-53-400-003

 Installation of the AFT Tie-Rods and Vibration Isolator 4055KM (131-9(A))
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific fiber-bristled brush No specific access platform 3.5 m (11 ft. 6 in.) No specific Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00
 to 75.00 lbf.ft) 98A49107504001 1 PROTECTOR - THREADS, APU MOUNTING BOLTS

 B.
 Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116
 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-027 USA MIL-L-81309
 RUST INHIBITOR(FOR CORROSION USE 15-004)
 (Ref. 20-31-00) Material No. 11-001 USA MIL-D-16791 TYPE I
 DETERGENT (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 cotter pin 49-12-04 04 -100 5 cotter pin 49-12-04 04 -110 20 cotter pin 49-12-04 04 -100

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-53Page 406 201-210, Config-2 Aug 01/05
 CES  D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
24-42-00-861-001  Energize the Ground Service Network from the External
 Power
 24-42-00-862-001  De-energize the Ground Service Network Supplied from
 the External Power
 29-00-00-864-001  Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action
 29-14-00-614-002  Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 49-00-00-080-003  Removal of the APU Hoist Tool (131-9(A))
 52-41-00-010-001  Open the APU Doors for Access
 52-41-00-410-001  Close the APU Doors after Access
 52-41-21-000-001  Removal of the APU Access Door 315AL
 52-41-22-000-001  Removal of the APU Access Door 316AR and the related
 Door Mechanism
 49-12-53-991-003  Fig. 401
 3. Job Set-up__________
 Subtask 49-12-53-860-057

 A. Aircraft Maintenance Configuration
 (1)
 Energize the ground service network (Ref. TASK 24-42-00-861-001).

 (2)
 On the panel 25VU make sure that the APU MASTER SW p/bsw is OFF.

 (3)
 Make sure that the warning notices is on panel 25VU to tell persons not to start the APU.

 (4)
 Make sure that hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).

 (5)
 Make sure that the access platform is in position below the access doors 315AL and 316AR.

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-12-53Page 407 201-210, Config-2 Aug 01/05
 CES

 (6) Make sure that the APU access doors 315AL, 316AR are open (Ref. TASK 52-41-00-010-001) or removed (Ref. TASK 52-41-21-000-001) and (Ref. TASK 52-41-22-000-001).
　
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