What it covers
The structural aspects of the fixed vertical surface attached to the fuselage including the dorsal fin.
Service difficulty reports · 2,534
Reports filed under 5530, newest first.
| 1995 | 157 |
|---|---|
| 1996 | 137 |
| 1997 | 136 |
| 1998 | 134 |
| 1999 | 120 |
| 2000 | 150 |
| 2001 | 76 |
| 2002 | 45 |
| 2003 | 41 |
| 2004 | 29 |
| 2005 | 39 |
| 2006 | 53 |
| 2007 | 29 |
| 2008 | 33 |
| 2009 | 38 |
| 2010 | 41 |
| 2011 | 35 |
| 2012 | 44 |
| 2013 | 49 |
| 2014 | 72 |
| 2015 | 77 |
| 2016 | 82 |
| 2017 | 80 |
| 2018 | 57 |
| 2019 | 70 |
| 2020 | 153 |
| 2021 | 120 |
| 2022 | 123 |
| 2023 | 125 |
| 2024 | 100 |
| 2025 | 60 |
| 2026 | 29 |
SDR 2026FA0000836Fairing · separatedUPPER VERTICAL TIP CAP FAIRING SEPARATED IN FLIGHT, SUBSEQUENTLY DAMAGING UPPER PORTION OF RUDDER, UPPER VERTICAL SKIN, ELEVATOR PUSH RODS AND ELEVATOR HORNS.SDR CALA2026092119598Tape · peelingSPEED TAPE HAS PEELED BACK ON VERTICAL STAB. FOUND VERTICLE STAB ANTENNA EROSION COATING PEELING. ACCOMPLISHED PART 1 OF ECRA 5530-01432. INSPECT INTERM REPAIR AT INTERVALS NOT TO EXCEED 2 DAYS AND PERFORM A PERMANENT REPAIR WITHIN 10 DAYS DUE TO VERTICAL SSDR IPXA2026090711902Panel · debondedTHE LT FWD TORQUE BOX PANEL HAS 2EA DELAMINATED, DISBONDED AREAS NEAR FSS 245.653 AND FSS 171.39. REMOVED ALL FASTENERS FROM LT FWD TORQUE BOX PANEL, EXCEPT MOST BOTTOM ROW, & BOTTOM AFT ROW, IAW SRM 51-40-02. INSTALLED NEW TORQUE BOX PANEL ON LT FWD IAW SR
See all 2,534 reports