What it covers
For general reports of the rotorcraft tail rotor system reported with insufficient information to file in a more specific tail rotor system. Avoid excessive use of this code if possible.
Service difficulty reports · 95
Reports filed under 6400, newest first.
| 1995 | 1 |
|---|---|
| 1996 | 10 |
| 1997 | 14 |
| 1998 | 8 |
| 1999 | 17 |
| 2001 | 8 |
| 2002 | 3 |
| 2003 | 4 |
| 2004 | 5 |
| 2005 | 2 |
| 2007 | 1 |
| 2008 | 2 |
| 2009 | 3 |
| 2012 | 2 |
| 2013 | 2 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2022 | 3 |
| 2023 | 3 |
| 2024 | 2 |
| 2025 | 1 |
SDR M3XA2025061109002Unknown · vibrationPILOT PERFORMED A PRECAUTIONARY LANDING IN VACANT FIELD IN CARTHAGE, MS FOR IN STRAIGHT AND LEVEL FLIGHT AT 2500 MSL AT 120 KIAS, THERE WAS A HIGH FREQUENCY VIBRATION IN THE ANTI-TORQUE PEDALS. THE VIBRATION REMAINED THROUGH DESCENT TO LANDING.SDR HDNA2024062802Arm · crackedPLAY WAS NOTICED IN TAIL ROTOR SYSTEM DURING A PREFLIGHT INSPECTION. INSPECTION OF SYSTEM FOUND A CRACK IN THE ARM OF THE ACTUATOR AND THE CARDIN JOINT BOLT WORN. AN AD AND ASB HAVE BEEN PREVIOUS COMPLIED WITH NO REOCCURRING INSPECTIONS REQUIRED DUE TO THE FINSDR QMLA2024040920036Blade · failedTWO EC135T2+ TAIL ROTOR BLADES HAVE CRACKED AND/OR SHOWN PITTING VISIBLE TO THE NAKED EYE IN THE BLADE ROOT WITHIN THE LAST 48 HOURS. (DAMAGE IS IN ZONE H ON OUTBOARD SIDE REQUIRING AIRBUS DISPOSITION PER AMM 64-22-00, 6-4) BLADE P/N L642A2002111 S/N'S M31134
See all 95 reports