R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
TASK 24-22-00-810-817
GEN1 does not come on line
1. Possible Causes
_______________
- IDG1 (4000XU)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-21-51-400-040 Installation of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine 1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the Engine 1(2)
AMM 31-60-00-860-001 EIS Start Procedure
AMM 71-00-00-710-003 Engine Automatic Start
AMM 71-00-00-710-028 Engine Shutdown
3. Fault Confirmation
__________________
A. Job Set up
(1) On the ELEC panel 35VU, push the GEN1 pushbutton switch (3XU1).
(2) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
(3) Start the engine 1 (Ref. AMM TASK 71-00-00-710-003).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 253
201-299, 301-399, Aug 01/05 CES B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel, push
the ELEC key (on the lower ECAM
DU, the ELEC page comes into
view).
On the lower ECAM DU:
- the GEN1 does not supply the AC1 busbar. On the upper ECAM DU:
- GEN1 OFF message does not come into view with the GEN1 pushbutton switch pushed (ON configuration).
4. Fault Isolation
_______________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
A. If the test confirms the fault:
(1) Do a check of the resistance of the IDG1 MPU coil between pin B/1 and pin B/2 (17.5 Ohms plus or minus 3.5 Ohms at 25 deg.C 77 deg. F.).
(2) If the resistance values are out of the specified limits:
- replace the IDG1 (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. Do the test given in para. 3.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Stop the engine 1 (Ref. AMM TASK 71-00-00-710-028).
(2) Put the aircraft back to its initial configuration.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 254
201-299, 301-399, Aug 01/05 CES
TASK 24-22-00-810-818 GEN2 does not come on line
1. Possible Causes
_______________
- IDG2 (4000XU)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-21-51-400-040 Installation of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine 1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the Engine 1(2) AMM 31-60-00-860-001 EIS Start Procedure AMM 71-00-00-710-003 Engine Automatic Start AMM 71-00-00-710-043 Normal Engine Automatic Start Procedure
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本文链接地址：A320 Trouble Shooting Manual 排故手册 电源 2(149)
