What it covers
For reports of the structure including exterior skin and truss framework of tail booms on rotorcraft. Includes attach fittings, etc., for tail boom and stabilizer surfaces. Typical parts are bulkhead, bracket, frame, frame tube, plate, etc.
Service difficulty reports · 965
Reports filed under 5302, newest first.
| 1995 | 25 |
|---|---|
| 1996 | 38 |
| 1997 | 27 |
| 1998 | 20 |
| 1999 | 49 |
| 2000 | 22 |
| 2001 | 53 |
| 2002 | 39 |
| 2003 | 42 |
| 2004 | 25 |
| 2005 | 18 |
| 2006 | 36 |
| 2007 | 31 |
| 2008 | 45 |
| 2009 | 43 |
| 2010 | 34 |
| 2011 | 72 |
| 2012 | 52 |
| 2013 | 27 |
| 2014 | 38 |
| 2015 | 31 |
| 2016 | 28 |
| 2017 | 24 |
| 2018 | 22 |
| 2019 | 32 |
| 2020 | 16 |
| 2021 | 10 |
| 2022 | 20 |
| 2023 | 11 |
| 2024 | 19 |
| 2025 | 13 |
| 2026 | 3 |
SDR 2026FA0000299Tail Boom · corrodedDURING THE PERFORMANCE OF THE GENERAL VISUAL INSPECTION AS SPECIFIED IN THE CONDITIONS OF PSE/TQ/2025/215289 REPAIR DEFERRAL LETTER, EVIDENCE OF PROPAGATION AND WORSENING CONDITIONS WAS DETERMINED OF THE CORROSION AT STA 8700, BL0.0 LOWER STRUCTURE OF 9Y-ELL TSDR 2A6R2026040675204Skin · crackedDURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.SDR 2A6R2026031675203Stator · corrodedDURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM .020 TO .030 DEEP. PER AIRBUS TE-2026-EC130-00406, THE STATOR ASSEMBLY WAS REMOVED AND REPLACED. FOR MORE INFORMATION
See all 965 reports