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时间:2011-03-27 22:23来源:蓝天飞行翻译 作者:航空
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AMM  05-51-29-200-001 Inspection after Abnormal Movement of the Pax/Crew Door
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After an abnormal pax/crew door movement:
 (1) Do the procedure: Inspection after Abnormal Pax/Crew Door Movement (Ref. AMM TASK 05-51-29-200-001).


 Significant MLG Vibration at Touch-Down
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  05-51-31-200-001 Inspection after Significant MLG Vibration at Touch-Down
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After significant MLG Vibration at touch-Down:
 (1) Do the procedure: Inspection after Significant MLG Vibration at touch down (Ref. AMM TASK 05-51-31-200-001).


 landing Gear extension at more than the Geardown Limiting speed
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  05-51-12-200-001 Inspection after Landing Gear Extension at more than the Geardown Limiting Speed
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After landing gear extension at more than the geardown limiting speed:
 (1) Do the procedure: Inspection after Landing Gear Extension at more than the Geardown Limiting Speed (Ref. AMM TASK 05-51-12-200-001).


 Flap/Slat Extension at more than the Flap/Slat Limiting Speed
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  05-51-13-200-001 Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After flap/slat extension at more than the flap/slat limiting speed:
 (1) Do the procedure: Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed (Ref. AMM TASK 05-51-13-200-001).


 In Flight Excessive Load factor due to Turbulence or Maneuver or in Excess of VMO/MMO
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  05-51-17-200-001 Inspection after in Flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMO
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After in flight excessive load factor due to turbulence or maneuver or in excess of VMO/MMO:
 (1) Do the procedure: Inspection after In flight Excessive Load Factor due to Turbulence or Maneuver or in Excess of VMO/MMO (Ref. AMM TASK 05-51-17-200-001).


 Engine Failure
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 05-51-26-200-001 INSPECTION AFTER ENGINE FAILURE
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. After engine failure:
 (1) Do the procedure: Inspection after Engine Failure (Ref. AMM TASK 05-51-26-200-001).


 Overweight Taxiing
 1. Possible Causes

_______________

 2. Job Set-up Information


______________________
 
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