C. Open the right fan-cowl door (Ref. TASK 71-13-00-010-040):
-
FOR 1000EM1
438AR
-
FOR 1000EM2
448AR
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 24-21-00-720-051
D. Reset of the IDG 1(2) disconnect system
CAUTION : MAKE SURE THE ENGINE IS STOPPED BEFORE YOU PULL THE DISCONNECT
_______ RESET RING. IF NOT YOU WILL CAUSE DAMAGE TO THE JAW TEETH.
(1) Slowly pull out the disconnect reset ring to the full limit of travel. Monitor the hand force that is necessary: this force must not to be too high. The disconnect mechanism must move freely without hard points.
NOTE : The disconnect solenoid will make a click that you can feel in
____ the disconnect reset ring when the reset ring comes near the full travel limit.
(2)
Let the disconnect reset ring go slowly back to the initial position.
(3)
Again, slowly pull out the disconnect reset ring to the full limit of travel. Monitor the hand force that is necessary. This force will be much less than in (1). Also there will be no indication of the reset of the disconnect mechanism.
(4)
On the ELEC control panel 35VU, push the GEN 1(2) pushbutton switch (the FAULT legend comes on).
(5)
When you do the first engine start, make sure that the related electrical- generation system operates correctly.
NOTE : If you start the engine after the test, you must do a GCU
____ reset. To do this, release then push the related GEN pushbutton switch.
NOTE : If you do not get a correct reset of the IDG disconnect
____ mechanism after you obeyed the instructions given in step (1), you must remove and replace the IDG.
R **ON A/C 401-499,
R Subtask 24-21-00-720-051-A
R D. Reset of the IDG 1(2) Disconnect System
R (Ref. Fig. 501/TASK 24-21-00-991-922)
R CAUTION : MAKE SURE THE ENGINE IS STOPPED BEFORE YOU PULL THE DISCONNECT_______
R RESET RING. IF NOT YOU WILL CAUSE DAMAGE TO THE JAW TEETH.
R (1) Remove the screw (3) and desengage the loop clamp (2).
R (2) Slowly pull out the disconnect reset ring (1) to the full limit of
R travel. Monitor the hand force that is necessary: this force must not
R be too high. The disconnect mechanism must move freely without hard
R points.
R NOTE : The disconnect solenoid will make a click that you can feel in____
R the disconnect reset ring when the reset ring comes near the
R full travel limit.
R (3) Let the disconnect reset ring (1) go slowly back to the initial
R position.
R (4) Again, slowly pull out the disconnect reset ring (1) to the full
R limit of travel.
R Monitor the hand force that is necessary. If the reset of the
R disconnect mechanism is correct, this force will be much less than in
R step (2). Also there will be no indication of the reset of the
R disconnect mechanism.
R (5) Install the loop clamp (2) on the disconnect reset ring (1) and
R secure the loop clamp with the screw (3). TORQUE the screw to between
R 20 and 22 lbf.in (0.22 and 0.24 m.daN).
R (6) On the ELEC control panel 35VU, push the GEN 1(2) pushbutton switch
R (the FAULT legend comes on).
R (7) When you do the first engine start, make sure that the related
R electrical generation system operates correctly.
R NOTE : If you start the engine after the test, you must do a GCU____
R reset. To do this, release then push the related GEN
R pushbutton switch.
R 1EFF : 401-499, 1 24-21-00Page 512 1 1 Aug 01/05 1 1 1CES 1
R R R NOTE : If you do not get a correct reset of the IDG disconnect____ mechanism after you obeyed the instructions given in step (2), you must remove and replace the IDG.
R **ON A/C ALL
5. Close-up________
Subtask 24-21-00-410-063
A. Close Access
(1) Close the right fan cowl door (Ref. TASK 71-13-00-410-040): - FOR 1000EM1 438AR - FOR 1000EM2 448AR
Subtask 24-21-00-860-052
B. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
TASK 24-21-00-730-040
System Test of the IDG Frequency (P/N 740119)
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 ELECTRICAL POWER 電源1(61)
