(3)
Remove and discard the cotter pins (1) and (7).
(4)
Remove the castle nuts (2) and (6), the washers (3) and (8) and the bolts (4) and (9).
(5)
Remove the tie-rods (5), (10) and (11) from the vibration isolator 4035KM (12).
(6)
Remove the vibration isolator (12) from the APU mount-bracket (14).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-12-51Page 406 201-210, Config-2 Aug 01/05
CES (7) If necessary remove the tie-rods (5), (10) and (11).
(a)
Remove the nuts (19) and (23), the washers (21) and (25) the screws (22) and (26).
(b)
Remove the clamps (27) and (28).
(c)
Disconnect the bonding straps (20).
(d)
Remove and discard the cotter pins (18).
(e)
Remove the castle nuts (17), the washers (16) and the bolts (15).
(f)
Remove the tie-rod from the bracket.
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
TASK 49-12-51-400-003
Installation of the FWD LH Tie -Rods and Vibration Isolator 4035KM (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 0.20 to 3.60 m.daN
(2.00
to 26.00 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)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-12-51Page 408 201-210, Config-2 Aug 01/05
CES C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
1 cotter pins 49-12-04 02 -110 1 cotter pins 49-12-04 02A-110 7 cotter pins 49-12-04 02 -120 7 cotter pins 49-12-04 02A-120 18 cotter pin 49-12-04 02 -110 18 cotter pin 49-12-04 02A-110
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
**ON A/C 001-049, 101-105, 201-203,
49-12-51-991-003 Fig. 401
R **ON A/C 107-107, 151-199, 204-210,
49-12-51-991-003-A Fig. 401A
R EFF : 001-049, 101-105, 107-107, 151-199, 49-12-51Page 409 201-210, Config-2 Aug 01/05
CES
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
3. Job Set-up
__________
Subtask 49-12-51-860-058
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.
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 机载辅助动力 AIRBORNE AUXILIARY POWER2(84)
