B. Get Access
(1)
Put the access platform in position below the APU compartment.
(2)
Open the maintenance door 314AR.
(3)
Release the 22 stud fasteners and remove the catwalk panel from the service panel.
4. Procedure
_________ Subtask 49-16-51-020-053
A. Removal of the Air Intake Actuator
(Ref. Fig. 201/TASK 49-16-51-991-003)
(1)
Disconnect the electrical connector (18).
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Remove the screw (20), the washer (19) and disconnect the bonding jumper (21).
(4)
Remove the clamp (11) and push the bellows (12) down.
(5)
Remove and discard the cotter pins (1) and (17).
(6)
Remove the castle nut (16), the washers (15), (9A) and the bolt (10).
(7)
Remove the castle nut (2), the washers (3) and (4) and the bolt (5).
(8)
Remove the air-intake flap actuator (6).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-51Page 202 201-210, Config-2 Aug 01/05
CES
INTENTIONALLY BLANK
Air-Intake Flap Actuator Figure 201/TASK 49-16-51-991-003- 12 (SHEET 1)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-51Page 204 201-210, Config-2 Aug 01/05
CES
Air-Intake Flap Actuator Figure 201/TASK 49-16-51-991-003- 22 (SHEET 2)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-51Page 205 201-210, Config-2 Aug 01/05
CES TASK 49-16-51-400-003
Installation of the Air-Intake Flap Actuator (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 circuit breaker(s) safety clip(s)
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)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 07-001 ELECTRICAL BONDING COATING (BLUE COLOR) (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-51Page 206 201-210, Config-2 Aug 01/05
CES C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 cotter pin 49-16-04 03 -070 12 bellows 49-16-04 03 -080 17 cotter pin 49-16-04 03 -070
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-16-43-400-001 Installation of the Air Intake Flap (GTCP 36-300) 49-16-51-820-003 Adjustment of the Air-Intake Flap Actuator (131-9(A)) 49-16-51-991-003 Fig. 201
3. Job Set-up
__________
Subtask 49-16-51-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the APU compartment.
(2)
Make sure that the maintenance door 314AR is open.
(3)
Make sure that the catwalk panel is not installed on the service panel.
Subtask 49-16-51-865-064
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-51Page 207 201-210, Config-2 Aug 01/05
CES 4. Procedure
_________
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 機載輔助動力 AIRBORNE AUXILIARY POWER3(47)
