What it covers
The system components and parts, including the computer which sense, transmit and provide aural, visual and stick shaker warning of an aircraft in an impending flight stall condition. Typical parts are transducer, stall warning detector, switch, vane, horn, lamp, stick shaker, heater element, warning unit computer, module, etc.
Service difficulty reports · 1,641
Reports filed under 3418, newest first.
| 1995 | 65 |
|---|---|
| 1996 | 75 |
| 1997 | 68 |
| 1998 | 65 |
| 1999 | 44 |
| 2000 | 189 |
| 2001 | 126 |
| 2002 | 73 |
| 2003 | 89 |
| 2004 | 131 |
| 2005 | 94 |
| 2006 | 112 |
| 2007 | 65 |
| 2008 | 22 |
| 2009 | 20 |
| 2010 | 37 |
| 2011 | 30 |
| 2012 | 24 |
| 2013 | 28 |
| 2014 | 21 |
| 2015 | 31 |
| 2016 | 25 |
| 2017 | 16 |
| 2018 | 23 |
| 2019 | 28 |
| 2020 | 31 |
| 2021 | 19 |
| 2022 | 12 |
| 2023 | 17 |
| 2024 | 24 |
| 2025 | 18 |
| 2026 | 19 |
SDR TAMF20260913061Aoa · out of limitsAIRCRAFT EXPERIENCED AN ECAM NAV AOA EXCEEDED MESSAGE ASSOCIATED WITH TURBULENCE. AIRBUS CONFIRMED LOADS EXCEEDING THE AIRCRAFT DESIGN ENVELOPE. REQUIRED INSPECTIONS WERE PERFORMED AND AIRBUS AUTHORIZED AIRCRAFT RELEASE THROUGH RDAF 81873879/017/2026 ISSUE ASDR SWIA2026081276841Aoa · faultedIMMEDIATELY AFTER TAKEOFF GOT A STICK SHAKER WITH CONTINUOUS IGNITION WITH STALL LIGHT FLASHING. FOS SIDE AIRSPEED TAPE HAD RED BARBER POLE FROM BOTTOM HIGHER THAN NORMAL. ALSO GOT AUDIO WARBLER. NEVER GOT STICK PUSHER. DURING FLIGHT HIGH AIRSPEED BARBER PSDR DALA2026080404491Aoa · failedATO- APPROX 30KTS DUE TO STICK PUSHER FAIL AND DISARM SPOILERS ANNUNCIATION WITH ASSOCIATED MASTER CAUTION. REPLACED NR 2 AOA SENSOR. ALL OPS CHECK GOOD. (6787252) AIRCRAFT WAS GROUNDED.
See all 1,641 reports