What it covers
For reports pertaining to the structure of the movable surface hinged to the rudder surface for directional trim. Typical parts are skin, hinge fitting, spar, rib. The actuating mechanism is filed in JASC code 2720.
Service difficulty reports · 196
Reports filed under 5543, newest first.
| 1995 | 22 |
|---|---|
| 1996 | 14 |
| 1997 | 14 |
| 1998 | 9 |
| 1999 | 12 |
| 2000 | 10 |
| 2001 | 4 |
| 2002 | 4 |
| 2003 | 5 |
| 2004 | 4 |
| 2005 | 6 |
| 2006 | 4 |
| 2007 | 3 |
| 2008 | 4 |
| 2009 | 10 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 1 |
| 2013 | 3 |
| 2014 | 6 |
| 2015 | 10 |
| 2016 | 16 |
| 2017 | 9 |
| 2018 | 6 |
| 2019 | 6 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 4 |
| 2024 | 2 |
| 2026 | 1 |
SDR 2026F00150Trim Tab · delaminatedTHE SUBJECT RUDDER TABS ARE TYPICALLY FOUND WITH DAMAGE AND DELAMINATION ON OUTER SKIN, WITH POTENTIAL FOR UNDERLYING CORE DAMAGE. THE SKINS ARE MADE FROM 0.012 2024-T81. BOEING 717-200 SRM 51-70-02 DOES NOT PROVIDE REPAIR INSTRUCTIONS FOR FULL REPLACEMENT OF SDR DALA2025103107967Tab · corrodedCORROSION ON SKIN LT & RT SIDE AT RUDDER TAB. REPLACED BY SERVICIABLE RUDDER CONTROL TAB (0266679).SDR DALA2024030503004Tab · dentedSEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB. SUMMARY OF NRC 00081: SEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB WERE MEASURED AND FOUND WITH NO DISBONDS AND ARE WITHIN LIMITS PER B717-200 SRM 55-41-01-1A PROCEDURE I ALLOWABLE DAMAGE I PAR 3,A,(4),(C), AND
See all 196 reports