Stall warnings in high capacity aircraft: The Australian context 2008 ...
Stall warnings in high capacity aircraft: The Australian context 2008 ...
Stall warnings in high capacity aircraft: The Australian context 2008 ...
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ATSB – AR-2012-172<br />
Other notable precursors to genu<strong>in</strong>e stall <strong>warn<strong>in</strong>gs</strong> were:<br />
• Turbulence/gusts/w<strong>in</strong>dshear AND<br />
- operation at low airspeeds (26 occurrences)<br />
- bank angle greater than 20° (21 occurrences)<br />
- an operational deviation, such as a weather diversion (19 occurrences)<br />
- retract<strong>in</strong>g flaps or lead<strong>in</strong>g edge devices (10 occurrences)<br />
- rapid bank angle rate of change (10 occurrences)<br />
- pitch angle greater than 10° (10 occurrences).<br />
• Autopilot-<strong>in</strong>itiated flight path correction AND<br />
- operation at low airspeeds (12 occurrences)<br />
- rapid pitch angle rate of change (8 occurrences)<br />
- rapid changes <strong>in</strong> airspeed (6 occurrences).<br />
• Operation at low airspeeds AND<br />
- bank angle greater than 20° (9 occurrences)<br />
- rapid pitch angle rate of change (8 occurrences)<br />
- operational deviation or crew distraction (8 occurrences)<br />
- pitch angle greater than 10° (8 occurrences).<br />
• Rapid changes <strong>in</strong> airspeed AND<br />
- rapid pitch angle rate of change (9 occurrences).<br />
• Operational deviation or crew distraction AND<br />
- rapid pitch angle rate of change (8 occurrences)<br />
- bank angle greater than 20° (9 occurrences).<br />
• Bank angle greater than 20° AND<br />
- retract<strong>in</strong>g flaps or lead<strong>in</strong>g edge devices (7 occurrences)<br />
- rapid pitch angle rate of change (6 occurrences).<br />
Of those four stall <strong>warn<strong>in</strong>gs</strong> that were classified as serious <strong>in</strong>cidents between <strong>2008</strong> and 2012,<br />
three occurred at airspeeds close to V Ref , and two <strong>in</strong>volved a rapid pitch angle rate of change.<br />
Irrespective of what conditions led to the stall warn<strong>in</strong>g, appropriate actions by flight crews to<br />
manage the situation commonly were:<br />
• immediately reduce the angle of attack, either by releas<strong>in</strong>g back pressure on the control<br />
column, or by mov<strong>in</strong>g the elevator control forward<br />
• roll w<strong>in</strong>gs level if <strong>in</strong> a turn<br />
• check eng<strong>in</strong>e power sett<strong>in</strong>gs, RPM, and speeds<br />
• check standby <strong>in</strong>struments<br />
• advise air traffic control and, when the stall warn<strong>in</strong>g occurred <strong>in</strong> severe turbulence, advise<br />
cab<strong>in</strong> crew of the situation (generally <strong>in</strong>volv<strong>in</strong>g a passenger announcement to rema<strong>in</strong> seated<br />
and secured, and a limit<strong>in</strong>g of cab<strong>in</strong> service)<br />
• if the stall warn<strong>in</strong>g was suspected to be spurious, make a note <strong>in</strong> the <strong>aircraft</strong>’s defect log for<br />
follow-up.<br />
While there have been different approaches to stall recovery tra<strong>in</strong><strong>in</strong>g <strong>in</strong> the past, the important<br />
response when confronted with a stall or a stall warn<strong>in</strong>g is to immediately reduce angle of attack.<br />
<strong>The</strong> United States Federal Aviation Adm<strong>in</strong>istration (FAA) advises all pilots and operators to use<br />
evaluation criteria for stall recovery that do not mandate a predeterm<strong>in</strong>ed value for altitude loss,<br />
and <strong>in</strong>stead consider the multitude of external and <strong>in</strong>ternal variables that can affect the recovery<br />
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