F 『 EEFF : ALL E Page 40576-11-19
E E Feb 01/98 E E ECES E E 56-5B E
F 『
E C F M E
E E
E E TASK 76-11-19-400-042
Installation of the Throttle Control Unit (8KS1, 8KS2)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.5 m (4 ft. 11 in.) 98DNSA20206080 1 RIGGING PIN
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2188 * Loctite 675 (Ref. 70-30-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 cotter pin 76-11-01 02 -010 8 cotter pins 76-11-01 03 -010
F 『 EEFF : ALL E Page 40676-11-19
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
76-11-00-820-044 Adjustment of the Mechanical Linkage
76-11-19-991-908 Fig. 401
76-11-19-991-909 Fig. 402
76-11-19-991-910 Fig. 403
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
76-11-19-991-911 Fig. 404
R **ON A/C 106-149, 303-399, 401-499,
76-11-19-991-911-A Fig. 404A
**ON A/C ALL
3. Job Set-up
__________
Subtask 76-11-19-860-052
A. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position.
(2) Make sure that the throttle control levers are set to idle (0 degree TLA).
(3) On the panel 50VU, make sure that the ENG FADEC GND PWR 1 and 2 pushbutton switches are released (on legends come on).
F 『 EEFF : ALL E Page 40776-11-19
E E Aug 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
Subtask 76-11-19-010-054
B. Make sure that the access door 811 is open.
Subtask 76-11-19-865-058
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
Subtask 76-11-19-869-057
D. Inspection of the bolt
(1) Make sure that the bush (3) is correctly bonded to the bolt (2).
(2) If necessary, bond the bush (3) to the bolt (2) with Loctite 675 (Material No. CP2188)
4. Procedure
_________ (Ref. Fig. 401/TASK 76-11-19-991-908, 402/TASK 76-11-19-991-909, 403/TASK 76-11-19-991-910) Subtask 76-11-19-420-051
A. Installation of the Throttle Control Unit.
(1) Remove all the blanking caps from the connectors.
(2) Install the throttle control unit 8KS1 (8KS2) (11) on its support.
(3) Install the three bolts (1) with the washers (10) and the nuts (9). Tighten the bolts (1).
(4) Install the three new cotter pins (8)
(5) Engage the rod (4) in the fork of the throttle control unit (11).
F 『 EEFF : ALL E Page 40876-11-19
E E May 01/05 ERE ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(6) Attach the rod to the fork with the bolt (2) on which the bush (3), the washer (7) and the nut (6) are assembled. Tighten the bolt.
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 ENGINE CONTROLS 發動機控制(13)
