What it covers
The single component used for both engine starting and direct current generation on turbine engines. Typical parts are bearing, shaft, brush, fan, retainer ring, armature, brush, housing, end bell, terminal, etc.
Service difficulty reports · 2,052
Reports filed under 2435, newest first.
| 1995 | 137 |
|---|---|
| 1996 | 131 |
| 1997 | 95 |
| 1998 | 181 |
| 1999 | 185 |
| 2000 | 74 |
| 2001 | 105 |
| 2002 | 118 |
| 2003 | 156 |
| 2004 | 85 |
| 2005 | 75 |
| 2006 | 46 |
| 2007 | 51 |
| 2008 | 63 |
| 2009 | 53 |
| 2010 | 37 |
| 2011 | 63 |
| 2012 | 43 |
| 2013 | 54 |
| 2014 | 39 |
| 2015 | 40 |
| 2016 | 18 |
| 2017 | 20 |
| 2018 | 36 |
| 2019 | 28 |
| 2020 | 12 |
| 2021 | 28 |
| 2022 | 16 |
| 2023 | 18 |
| 2024 | 21 |
| 2025 | 19 |
| 2026 | 5 |
SDR DALA2026081404663Starter Gen · burnedAPU KICKED OFF WHILE SITTING AT THE GATE, STRONG ODOR ( ELECTRICAL ODOR) BUT NO FAIL INDICATION OR APU LIGHTS. APU CONTINUED TO RUN BUT NO POWER. INSPECTED PER AMM 05-42. FOUND STARTER-GENERATOR CABLE COVER SEVERLY BURNING. REMOVED & REPLACED APU STARTER-GENSDR XU5A2026080600173Starter Gen · inoperativeTHE AIRCRAFT A LOSS OF LOAD INDICATION ON THE NR 2 GENERATOR FOLLOWED BY A BAT DISCHARGE CAUTION LIGHT. UPON INSPECTION OF THE AIRCRAFT IT WAS DETERMINED THAT THE NR 2 GENERATOR HAD FAILED IN A MANNER THAT ALSO CAUSED THE BUSS TIE SYS TO FUNCTION IMPROPERLY RESDR EE0A202605310001Starter Gen · failedRT ENGINE FAILD TO RATATE ON START. REPLACED RT STARTER GENERATOR.
See all 2,052 reports