(5) Remove filler plugs from the hoist points on the air intake cowl. Keep the plugs for the installation after the air intake cowl is removed.
F 『 EEFF : ALL E Page 40271-11-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Air Intake Cowl
Figure 401/TASK 71-11-00-991-300
F 『 EEFF : ALL E Page 40371-11-00
E E Feb 01/98 E E ECES E Subtask 71-11-00-480-050
F 『
E C F M E
E E
E 56-5B E
E E
B. Installation of the Tooling
(1) Install the universal attach pads (20) in the hoist points of the air intake cowl (25).
(2) Attach the SLING - AIR INTAKE COWL (RSE1112) (15) to the universal attach pads (20).
(3) Lift the sling until it supports the air intake cowl (25) weight. Subtask 71-11-00-020-050
C. Disengagement of the Air Intake Cowl
(1) Remove the bolts (50), washers (5) and (55), spacers (60), and nuts
(10) that attach the air intake cowl (25) to the engine flange.
(2) Pull the air intake cowl (25) forward to disengage the index pin from the engine flange.
Subtask 71-11-00-480-056
D. Installation of the Air Intake Cowl on the Dolly
(1) Put the air intake cowl (25) on the DOLLY - AIR INTAKE COWL (RSE1116).
(2) Attach the air intake cowl to the dolly with the bolts (50), washers
(5) and (55), spacers (60), and the nuts (10). Subtask 71-11-00-080-050
E. Remove the SLING - AIR INTAKE COWL (RSE1112) (15) and the universal
attach pads (20) from the air intake cowl (25).
Subtask 71-11-00-420-056
F. Installation of the Filler Plugs
(1) Install the filler plugs on the hoist points of the air intake cowl (25).
(2) Put protective covers on the preformed hose, the swirl nozzle duct assembly, the ECU, and the ECU cooling air duct.
F 『 EEFF : ALL E Page 40471-11-00
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TASK 71-11-00-400-041 Installation of the Air Intake Cowl CAUTION : ADJUST THE FAN COWL DOORS WHEN A NEW AIR INTAKE COWL IS INSTALLED. IF
_______ THE FAN COWL DOORS ARE NOT CORRECTLY ADJUSTED THE DOORS CAN OPEN IN FLIGHT.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific universal attach pads No specific warning notice No specific access platform 1 m (3 ft. 3 in.) No specific Torque Wrench : range 96.00 to 900.00 lbf.in
(1.00 to 10.00 m.daN) RSE1112 1 SLING - AIR INTAKE COWL
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP-2306
Material No. CP1039
R Material No. CP1041
R
R Material No. CP2011
R
R Material No. CP2559
R
R Material No. CP2560
R
R Material No. CP2566
R
F
EEFF : ALL
E
E
ECES
*
tape (Ref. 70-30-00)
*
acetone (Ref. 70-30-00)
*
isopropyl alcohol (Ref. 70-30-00)
*
stoddard solvent (Ref. 70-30-00)
*
ardrox 552 (Ref. 70-30-00)
*
turco ind 79 (Ref. 70-30-00)
*
mag-chem teksol (Ref. 70-30-00)
『
E 71-11-00Page 405
E May 01/05EE F 『 EEFF : ALL E Page 40671-11-00
F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R Material No. Material No. CP2584 CP2656 * degreasol 99 R (Ref. 70-30-00) * mag-chem skysol (Ref. 70-30-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 动力装置 POWER PLANT 1(92)
