What it covers
For reports of the fittings on the fuselage used for the attachment of the stabilizers
Service difficulty reports · 571
Reports filed under 5342, newest first.
| 1995 | 11 |
|---|---|
| 1996 | 9 |
| 1997 | 4 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 21 |
| 2001 | 28 |
| 2002 | 24 |
| 2003 | 12 |
| 2004 | 11 |
| 2005 | 8 |
| 2006 | 9 |
| 2007 | 8 |
| 2008 | 6 |
| 2009 | 12 |
| 2010 | 13 |
| 2011 | 34 |
| 2012 | 14 |
| 2013 | 21 |
| 2014 | 24 |
| 2015 | 7 |
| 2016 | 13 |
| 2017 | 12 |
| 2018 | 8 |
| 2019 | 7 |
| 2020 | 19 |
| 2021 | 44 |
| 2022 | 25 |
| 2023 | 6 |
| 2024 | 11 |
| 2025 | 74 |
| 2026 | 69 |
SDR REXA2026101601945Drag Angle · crackedDURING (ET) HFEC INSPECTION ON DRAG ANGLE IAW NRC 252, A CRACK WAS FOUND ON THE AFT DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) AT VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026101601944Drag Angle · crackedCRACKED FWD DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) ON THE VERTICAL STABILIZER TO FUSELAGE. THE FWD DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026101601943Drag Angle · crackedCRACKED AFT DRAG ANGLE BTWN 55.62% STR DATUM TO 61.56% STR DATUM ON THE VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
See all 571 reports