Airbus ABNORMAL/EMERGENCY PROCEDURES 空客非正常/紧急程序(32)

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- Speed below 210, FLAP 150, Speed 'F + 10'
- Speed below 195, FLAP 200, Speed 'F'
- Extend L/G down
- Speed below 180, FLAP 400, Speed VAPP
- Trim the aircraft until VLS and continue to increase pitch attitude until stick shaker activation
- At stick shaker/cricket sound.
- Move throttle full forward.
- Level wings, smoothly adjust pitch to 100 nose up (maybe increased to 17.5 to arrest the rate of descent when ground contact is a factor)
- The PNF switches to FPV and also monitors V/S
- Maintain/adjust pitch as above until crossing VLS then ask for “GO AROUND FLAP”
-  “+ve climb”, “Gear UP”.
- Accelerate and clean up the aircraft as per speed schedule.
- Recovery GREEN DOT speed
- After Take-off check list.

  STALL DURING TURN

 For the recovery, bring the wings level and reduce pitch simultaneously and smoothly move throttles full forward.

 

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A310 ABNORMAL/EMERGENCY PROCEDURES
 REVISION OF JAN 2004: CHANGES

Page 1 of 2

Changes are highlighted by a bold vertical sidebar in the left margin - a summary description of these is given below by page number. Incase of more than one change on the same page, the changes are listed in the sequence they occur.

Some changes have been made in the layout and language of the document to promote better readability and (it is hoped) ease of assimilation. These layout changes HAVE NOT been highlighted by a sidebar nor described here.

Page 2: required callout incase C/L has to be interrupted

Page 3 & 4: section on CRM rewritten

Page 6: previously wrongly printed as RTO – now reads ‘engine failure’

Page 9: note regarding reverser usage and ref to SOP added

Page 12 & 15: 1) words ‘flight path’ previously missing
2) APU to be started during period of relative inactivity after primary   
           ECAM actions/before reaching MSA for level acceleration.

Page 13 & 16: 1) LVL/CH to be selected first, and then ‘green dot’
                   speed so that throttles do not come back thus ensuring climb
                    performance.
                2) ECAM actions are performed till the STATUS pg appears, status pg
　
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