曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 1 If the resistance values are in the specified limits:
_
 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
 2 If the resistance values are out of the specified limits:
_
 - disconnect the harness J13 from the fuel flow transmitter and do a check of the transmitter resistance between: . pins 1 and 2 (250 to 350 ohms) . pins 2 and 3 (250 to 350 ohms) . pins 1 and 4 (> 10 megohms) . pin 1 and the ground (> 10 megohms).
 a If the resistance values are in the specified limits:
_
 - replace the harness J13 (Ref. AMM TASK 73-21-50-000-046) and (Ref. AMM TASK 73-21-50-400-046).
 b If the resistance values are out of the specified limits:
_
 - replace the fuel flow transmitter (Ref. AMM TASK 73-31-10-000-002) and (Ref. AMM TASK 73-31-10-400-002).
 D. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 220
 E E Feb 01/05 ERE
ECES  TASK 73-00-00-810-870 Flexible Temperature not Entered

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E

 1. Possible Causes
_______________
 - aircraft wiring
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASM 73-25/06
 3. Fault Confirmation
__________________
 A. Test
 (1) On the MCDU, make sure that the FLEX TEMP value is correctly entered.
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the ECAM warning message FLEX TEMP NOT SET:
 NOTE : Do this procedure on the two engines.
____
 - do a check and repair the aircraft wiring between the MCDU (3CA1) (3CA2)/FCU (2CA)/FMGC (1CA1) (1CA2)/EIU (1KS1) (1KS2) and the ECU (4000KS) (Ref. ASM 73-25/06).
 B. After the subsequent flight, make sure that the fault does not continue.
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 221
 E E Feb 01/05 ERE
ECES

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E

 INTENTIONALLY BLANK

 F 『R E E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 222
 E E Feb 01/05 E E ECES
E TASK 73-00-00-810-871 Autothrust Deactivation in Flight

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E

 1. Possible Causes
_______________
 - aircraft wiring
 2. Job Set-up Information

______________________
 Not Applicable

 3. Fault Confirmation

__________________
 A. Test
 (1) Not applicable, you cannot confirm this fault on the ground.
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the crew observation:
 AUTOTHRUST-deactivation in flight:

 NOTE : Do this procedure on the two engines.
____
 (1) Do a check and repair the aircraft wiring between the FMGC (1CA1) (1CA2), FCU (2CA), EIU (1KS1) (1KS2) and ECU (4000KS).
 B. After the subsequent flight, make sure that the fault does not continue.
 F 『 EEFF : ALL E ∞∞73-00-00∞∞∞∞∞∞∞∞∞∞Page 223
 E E May 01/99 ERE
ECES

 F 『
 E C F M E
 E E
 E 56 E
 E E

 TASK 73-00-00-810-872
R Idle Speed Difference between Engine 1 and Engine 2
 1. Possible Causes
_______________
 - IDG, FRV (Oil temp)

 - SFCC-1(2) (21CV(22CV))

 - EIU-1(2) (1KS1(1KS2))

 - P/BSW-ANTI ICE/ENG 1 (2DN1)

 - P/BSW-ANTI ICE/ENG 2 (2DN2)

 - wing anti-ice valve L

 - wing anti-ice valve R

 - PO/P12/T12

 - BMC-1(2) (1HA1(2))

 - ECU (4000KS)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發動機燃油和控制 1(32)