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时间:2011-03-28 09:44来源:蓝天飞行翻译 作者:航空
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R (1) Read the Class 3 Faults of the GAPCU from the CFDS (Ref. AMM TASK 24-R 41-00-740-002).
R 4. Fault Isolation
_______________
R CAUTION : BEFORE YOU START THE CHECK OF IDG WIRING THAT INCLUDES CONNECTORS,
_______ R EXAMINE EACH CONNECTOR TO MAKE SURE THAT THERE IS NO OIL IN IT. R IF YOU FIND OIL, CLEAN THE CONNECTOR AND CONNECT IT AGAIN. R IF THE FAILURE CONTINUES, DO THE TROUBLE SHOOTING PROCEDURE AS R GIVEN BELOW.
 「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 : 106-149, 229-299, 303-399, 401-499, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 249
 Aug 01/05 CES


R A. If the Class 3 Faults gives the maintenance message IDG1 (E1-4000XU) OIL R OUT TEMP/ GCU1 (1XU1):
R NOTE : This CFDS message can come into view when the temperature of the
____ R IDG 1 oil is more than 151 deg.C but less than 185 deg.C. R If this CFDS message comes into view with other chapter-24 CFDS R messages, do the trouble shooting for all these messages. R If there is no other message, do the trouble shooting that R follows:
R (1) Do the trouble shooting for chapter-73 CFDS messages that come into
R view with the CFDS message IDG1 (E1-4000XU) OIL OUT TEMP/ GCU1
R (1XU1).

R (2) If there is no chapter-73 CFDS message or if the fault continues
R after the trouble shooting:
R - do the check of the Differential Pressure Indicator (DPI) of the
R IDG 1 (Ref. AMM TASK 24-21-00-210-046).

R (a) If the DPI is extended:
R - replace the engine 1 IDG (4000XU) (Ref. AMM TASK 24-21-51-000-R 040) and (Ref. AMM TASK 24-21-51-400-040).

R (b) If the DPI is not extended:
R - do a check of the IDG 1 oil level (Ref. AMM TASK 24-21-00-210-R 046).

R  1_  If the oil level is not correct:
R  - replace the IDG 1 charge and scavenge filters (Ref. AMM TASK 
R  24-21-00-920-040) 
R  - add oil (Ref. AMM TASK 12-13-24-612-041). 

R 2_ If the oil level is correct:
R - do a check of the resistance of the oil inlet and outlet
R temperature-sensors of the IDG 1 (Ref. ASM 24-21/01)
R between:

R . pins B/7 and B/8 (100 ohms plus or minus 10 ohms at the R ambient temperature of the IDG case)

R . pins B/8 and B/9 (100 ohms plus or minus 10 ohms at the R ambient temperature of the IDG case).


R a_ If the resistance values are out of the specified limits:
R - replace the engine 1 IDG (4000XU) (Ref. AMM TASK 24-21-R 51-000-040) and (Ref. AMM TASK 24-21-51-400-040).

R b_ If the resistance values are in the specified limits:
R - do a check of the wiring of the oil outlet
R temperature-sensor (Ref. ASM 24-21/01) for an open
R circuit or a short to ground between:

R . pin B/7 of the IDG 1 and pin A/9C of the GCU 1

R . pin B/8 of the IDG 1 and pin A/9D of the GCU 1

R . pin B/9 of the IDG 1 and pin A/10C of the GCU 1.


 「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 : 106-149, 229-299, 303-399, 401-499, ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 250
 Aug 01/05 CES


R  * If the wiring is not correct: 
R  - repair or replace as necessary. 
R  * If the wiring is correct: 
R  - replace the GCU-1 (1XU1) (Ref. AMM TASK 24-22-34-000-
R  001) and (Ref. AMM TASK 24-22-34-400-001). 
R  ** If the fault continues: 
R  - replace the engine 1 IDG (4000XU) (Ref. AMM TASK 24-21-
R  51-000-040) and (Ref. AMM TASK 24-21-51-400-040). 
R  B. When you replace a component or repair the wiring: 
R  - do the subsequent flight before you do the check of the Class 3 Faults 
R  of the GAPCU from the CFDS. 
R  If the test continues to give the fault message, continue the trouble 
R  shooting procedure.


R TASK 24-00-00-810-822


R Failure of the Oil Temperature Sensors of the IDG 2 without Overtemperature R Detection
R 1. Possible Causes
_______________
R - IDG (4000XU) R - GCU-2 (1XU2) R - wiring
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 12-13-24-612-041 R R AMM 24-21-00-210-046 R R AMM 24-21-00-920-040 R R AMM 24-21-51-000-040 R R AMM 24-21-51-400-040 R R AMM 24-22-34-000-001 R AMM 24-22-34-400-001 R AMM 24-41-00-740-002 R ASM 24-21/01
R 3. Fault Confirmation
__________________
 
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