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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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