(2) Connect the four electrical connectors (12). Tighten electrical connector fingertight plus one-eight turn using soft nose pliers.
Subtask 76-11-19-080-052
D. Remove the rigging pin (13) from the artificial feel unit. Subtask 76-11-19-865-060
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 21CE1, 21CE2, 21CE3, 22CE
Subtask 76-11-19-861-051
F. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002) Subtask 76-11-19-869-058
G. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (upper ECAM DU only) (Ref. TASK 31-60-00-860-001).
(2) On the panel 50VU, make sure that the ENG FADEC GND PWR 1 and 2 pushbutton switches are released (ON LEGENDS COME ON).
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Subtask 76-11-19-865-059
H. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 8KS1
49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41 FOR 8KS2 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 121VU ENGINE/ENG2/FADEC B 4KS2 Q40
Subtask 76-11-19-710-052
J. Do this test
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 404/TASK 76-11-19-991-911)
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 404A/TASK 76-11-19-991-911-A)
**ON A/C ALL
(1) Open circuit breakers 2KS1, 2KS2
(2) Move the throttle control lever ENG1(2) and make sure that the small white circle on N1 indication follows the throttle control lever position.
(3) Close circuits breakers 2KS1, 2KS2
(4) Open circuit breakers 4KS1, 4KS2
(5) Move throttle control lever ENG1(2) and make sure that the small white circle on N1 indication follows the throttle control lever position.
(6) Close circuit breakers 4KS1, 4KS2.
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R Upper Display Unit of the Ecam System N1 Indication R Figure 404/TASK 76-11-19-991-911
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Upper Display Unit of the Ecam System N1 Indication Figure 404A/TASK 76-11-19-991-911-A
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(7) Move throttle control lever ENG1(2) and make sure that the small white circle on N1 indication follows the throttle control lever position. Make sure that no warning message shows on the upper ECAM DU.
(8) Do the BITE test of the EFCS (Ref. TASK 27-96-00-740-001) and make sure that no message related to the throttle control unit 8KS1(2) is shown.
5. Close-up
________ Subtask 76-11-19-869-059
A. Put the aircraft back to its initial configuration.
(1) On the panel 50VU, release the ENG FADEC GND PWR 1 and 2 pushbutton switches (ON legends goes off).
(2) Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
Subtask 76-11-19-862-051
B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 76-11-19-410-051
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the access door 811
(3) Remove the access platform(s).
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TASK 76-11-41-000-042
Removal of the Throttle Control Lever Assembly
1. Reason for the Job
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本文鏈接地址：A320飛機維護手冊 AMM ENGINE CONTROLS 發動機控制(14)
