What it covers
The system components and parts from the cockpit control to the stabilizer, except the actuator which controls position of the horizontal stabilizer for pitch trim (usually found on high performance turbine powered aircraft). Also for stabilator control systems on aircraft utilizing a single horizontal tail surface for both the stabilizer and elevator. Does not include structure in JASC code 5511. Typical parts are cable, bellcrank, pulley, control valve, indicator, etc.
Service difficulty reports · 2,126
Reports filed under 2740, newest first.
| 1995 | 35 |
|---|---|
| 1996 | 39 |
| 1997 | 38 |
| 1998 | 57 |
| 1999 | 46 |
| 2000 | 102 |
| 2001 | 89 |
| 2002 | 74 |
| 2003 | 103 |
| 2004 | 125 |
| 2005 | 146 |
| 2006 | 173 |
| 2007 | 58 |
| 2008 | 54 |
| 2009 | 58 |
| 2010 | 62 |
| 2011 | 92 |
| 2012 | 67 |
| 2013 | 47 |
| 2014 | 66 |
| 2015 | 46 |
| 2016 | 49 |
| 2017 | 38 |
| 2018 | 63 |
| 2019 | 51 |
| 2020 | 37 |
| 2021 | 67 |
| 2022 | 54 |
| 2023 | 61 |
| 2024 | 59 |
| 2025 | 40 |
| 2026 | 30 |
SDR UIEA2026101500987Limit Switch · failedREJECTED T/O AT 60KTS DUE TO EICAS MESSAGE. UNSCHEDULED STAB TRIM MESSAGE ALSO APPEARED TWICE DURING TAXI OUT(<P>RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR EXPERIENCED AN INTERNAL SHORT. R&R R/H STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER MODULE PER ASDR AALA202610081174Motor · inoperativeAIRCRAFT WAS GROUNDED: -- EMERGENCY DECLARED. DECESION WAS MADE TO RETURN TO DFW. AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT -- ELECTRIC STAB TRIM FAILED AFTER TAKEOFF. ALSO SPEED TRIM FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED STAB TRIM MOTOR PER AMM 27SDR AALA202609251867Stabilizer · jammedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVEERTED TO PIT DUE TO THE FLIGHT CREW REPORTING FLIGHT CONTROL STABILIZER JAM AFTER TAKEOFF - THE AIRCRAFT LANDED SAFELY AT PIT AND TAXIED TO THE GATE UNDER ITS OWN POWER. (OPEN)
See all 2,126 reports