What it covers
The system components and parts, including the computer which sense, transmit and provide warning when operating air speed limits are exceeded. Typical parts are transducer, stall warning detector, switch, vane, horn, lamp, warning unit computer, module, etc.
Service difficulty reports · 39
Reports filed under 3415, newest first.
| 1997 | 1 |
|---|---|
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 6 |
| 2003 | 3 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 4 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2019 | 3 |
| 2022 | 3 |
| 2025 | 3 |
SDR HNAA2025123100870Control Panel · malfunctionedUNABLE TO SET BARO FOR ADC 1 REGARDLESS OF REVERSIONARY PANEL SETTING. FACT 30DEC25 18:49 PHL R/R PFD 100 IAW AMM 34-22-01 OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.SDR QXEA2025102400330Module · malfunctionedFLIGHT 2268. IN CRUISE FLIGHT @ FLT 360 MASTER CAUTION & CAUTION MSG ON EICAS "ADS 1 FAIL." AUTO REVERSION TO ADS 3. MSG EXTINGUISHED AFTER AUTO REVERSION TO ADS 3. THIS OCCURED SIMULTANEOUSLY AS CAUTION MSG AUTOBRAKE FAIL. MSG EXTINGQUISHED. RETURNED TO FIELDSDR QXEA2025052900229Probe · fodFLIGHT 2016. REJECTED TAKEOFF AT APPROX. 100 KTS IAS DUE TO IAS MISMATCH FLAG ON AIRSPEED DIFFERENCE WAS APPROX. 10-15 KTS BETWEEN AIRSPEED INDICATORS CO PILOT IAS SHOWED APPROX. 80 KNOTS AT THE "80" CALL, PILOT SIDE SHOWED APPROX. 70 KNOTS. RETURNED TO GATE.
See all 39 reports