What it covers
The units mechanically connected to flight control cables, etc., for making minor corrections in aircraft attitude or direction.
Service difficulty reports · 128
Reports filed under 2216, newest first.
| 1995 | 6 |
|---|---|
| 1996 | 4 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 3 |
| 2000 | 5 |
| 2001 | 8 |
| 2002 | 3 |
| 2003 | 8 |
| 2004 | 12 |
| 2005 | 19 |
| 2006 | 20 |
| 2007 | 4 |
| 2008 | 2 |
| 2009 | 4 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 6 |
| 2013 | 3 |
| 2014 | 4 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 1 |
| 2021 | 1 |
| 2022 | 3 |
| 2025 | 1 |
SDR 6CBA2025121625001Adapter · faultyDURING A ROUTINE FLIGHT FROM KPSM TO KBTV, THE CREW EXPERIENCED DURING CLIMB THE YAW DAMP WOULD NOT ENGAGE. ON THE THIRD ATTEMPT TO ENGAGE THE YAW DAMP, AP FAIL CAS MESSAGE FOLLOWED 2 SECONDS LATER BY A RED TRIM RUNAWAY CAS. AN EMERGENCY WAS DECLARED AND THE SDR 3WTR20221013Bolt · corrodedWHILE COMPLYING WITH EMBRAER SB 505-22-0004 R3, THE SUBJECT CLUTCH RETAINING BOLT WAS FOUND TO BE SEVERELY CORRODED. THE PURPOSE OF THE SERVICE BULLETIN IS TO INSPECT AND REPLACE THIS BOLT BUT THE CORROSION FOUND ON THIS BOLT WAS THROUGH APPROXIMATELY 50% OF TSDR 9JLA2022071938701Trim System · failedTHE FLIGHT CREW REPORTED THE PITCH TRIM DID NOT WORK WITH AUTO-PILOT ELECTRIC PITCH TRIM ON BOTH THE LEFT AND RIGHT SIDE BELOW 200KTS ON DESCENT. OPERATIONS WERE CONTINUED UNDER MEL 27-31-01. THE BASE MAINTENANCE TEAM DETERMINED THE ELEVATOR ELECTRIC TRIM MOTO
See all 128 reports