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时间:2011-03-28 22:53来源:蓝天飞行翻译 作者:航空
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 - replace the SENSOR-ANGLE OF ATTACK, 2 (3FP2).
 **ON A/C 001-049, 101-105, 151-199, 201-228,
 Post SB 34-1240 For A/C 001-049,101-105,151-199,201-228,
 A. If the LOG-BOOK gives the maintenance message AOA SENSOR2 (3FP2)/ADIRU2 (1FP2):
 - do a visual check of the angle of attack sensor 2 (3FP2).
 (1) If the angle of attack sensor 2 (3FP2) is damaged:

 - replace the SENSOR-ANGLE OF ATTACK, 2 (3FP2) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).

 (2) If the angle of attack sensor 2 (3FP2) is not damaged:


 - no other action is neccesary.
 (a) After the subsequent flight, if the fault continues:
 - replace the SENSOR-ANGLE OF ATTACK, 2 (3FP2).
 B. If the maintenance message AOA SENSOR2 (3FP2)/ADIRU2 (1FP2) is shown in the Ground Scanning, after the test of the angle of attack warning:
 - no maintenance action is necessary.
 NOTE : At the end of the test, on the ADIRS CDU, set the OFF/NAV/ATT
____ selector switch related to the ADIRU2 to OFF for some seconds then to NAV to cancel the messages (fast re-alignment is not sufficient)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-228, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A256
 301-399, 401-499, Aug 01/05 CES


R **ON A/C 001-049, 101-105, 151-199, 201-228, 301-399, 401-499,
 TASK 34-11-00-810-894
 Deterioration of the Angle of Attack Sensor 3
 1. Possible Causes

_______________

 2. Job Set-up Information

______________________
 Not Applicable


 3. Fault Confirmation


__________________ R **ON A/C 001-049, 101-105, 151-199, 201-228, 301-399, 401-499, Post SB 34-1240 For A/C 211-228,
 A. Test
 Not applicable, you cannot confirm this fault on the ground.

R **ON A/C 001-049, 101-105, 151-199, 201-228, 301-399, 401-499,
 4. Fault Isolation
_______________ R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399, 401-499,
 A. If the LOG-BOOK gives the maintenance message AOA SNSR3 (3FP3)/ADIRU3 (1FP3):
 - no other action is necessary.
 **ON A/C 001-049, 101-105, 151-199, 201-228,
 Post SB 34-1240 For A/C 001-049,101-105,151-199,201-228,

 A. If the LOG-BOOK gives the maintenance message AOA SENSOR3 (3FP3)/ADIRU3 (1FP3):
 - no other action is necessary.
 B. If the maintenance message AOA SENSOR3 (3FP3)/ADIRU3 (1FP3) is shown in the Ground Scanning, after the test of the angle of attack warning:
 - no maintenance action is necessary.
 NOTE : At the end of the test, on the ADIRS CDU, set the OFF/NAV/ATT

____ selector switch related to the ADIRU3 to OFF for some seconds then to NAV to cancel the messages (fast re-alignment is not sufficient)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-228, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A257
 301-399, 401-499, Aug 01/05 CES TASK 34-11-00-810-895


 Loss of the Air Data Display on the CAPT PFD with the AIR DATA Selector Switch at CAPT/3
 1. Possible Causes
_______________
 - SEL SW-AIR DATA (15FP)

 - wiring of the AIR DATA selector switch (15FP)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-868 Loss of the Attitude Data on the CAPT PFD with the
 ATT HDG Selector Switch at CAPT/3
 AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3)
 AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 ASM 31-68/04

 3. Fault Confirmation
__________________
 A. Test
 Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. If the air data indications go out of view on the CAPT PFD with the AIR DATA selector switch at CAPT/3:
 - remove the DMC1 and DMC3 (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).

 - do a check for a ground signal at the pin AB/4E of the DMC1 and DMC3.


 (1) If there is no ground signal:

 - replace the SEL SW-AIR DATA (15FP).
 (a) If the fault continues:
 - do a check and repair the wiring of the AIR DATA selector switch (15FP): pin A/5 to the ground point pin A/6 to the first terminal block (Ref. ASM 31-68/04).
 
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