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
______________________
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 時(shí)間限制/維護(hù)檢查(8)
