- Serial number
- 7876
- Year built
- 2003
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 5, 2004
- Certificate issued
- January 5, 2004
- Expires
- April 30, 2029
- Mode S code
- AD7F3A
- Registered owner
- Skywest Airlines Inc
- Location
- St George, UT
- Owner type
- Corporation
From the FAA registry file of October 20, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.
On this page
Airworthiness directives that may apply · 200
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.
| 1981 | 1 |
|---|---|
| 1982 | 6 |
| 1988 | 1 |
| 1993 | 1 |
| 1994 | 6 |
| 1995 | 4 |
| 1996 | 2 |
| 1997 | 5 |
| 1998 | 4 |
| 1999 | 8 |
| 2000 | 7 |
| 2001 | 9 |
| 2002 | 9 |
| 2003 | 15 |
| 2004 | 14 |
| 2005 | 14 |
| 2006 | 16 |
| 2007 | 12 |
| 2008 | 19 |
| 2009 | 9 |
| 2010 | 16 |
| 2011 | 10 |
| 2012 | 7 |
| 2013 | 8 |
| 2014 | 6 |
| 2015 | 5 |
| 2016 | 7 |
| 2017 | 6 |
| 2018 | 3 |
| 2019 | 6 |
| 2020 | 10 |
| 2021 | 5 |
| 2022 | 8 |
| 2023 | 6 |
| 2024 | 3 |
| 2025 | 6 |
| 2026 | 3 |
Airframe · Bombardier CL-600-2B19
AD 2026-13-02NavigationAD 2026-05-05Flight controlsAD 2026-02-03Flight controlInformation bulletins that may apply · 10
Advisory, not mandatory. Matched the same way as ADs.
Airframe · Bombardier CL-600-2B19
SAIB NM-10-06Oxygen Inspection of Third Crewmember Oxygen HoseSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-07-26Flap failures during cold weather operationsSAIB NE-07-25Thrust reverser access cowlsSAIB NM-07-11Brake System AccumulatorsSAIB NM-05-60SAIB NM-05-55SAIB NM-05-53SAIB NM-05-31Engine · GE CF34 series
SAIB NE-04-77NTSB investigations
No NTSB investigations matched to N969SWMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2B19 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date.
Service difficulty reports · 207
SDR SWIA2026082377263Frame Angle · crackedCRACK FOUND ON THE RT FRAME ANGLE, BS 605, STR 20R. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM 51-42-06, REV 39, SRM 51-42-21, REV 39, AND DWG 601R36026 REV AF.SDR SWIA2026082377249Frame Angle · crackedCRACK ANGLE AT FRAME BS 605, STR 20L. REMOVED AND REPLACED THE FRAME ANGLE AT BS 605, STR 20L IAW SRM 51-42-06, REV 39, SRM 51-42-21, REV 39, AND DWG 601R36026, REV AF. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1003-SKY LEAK CHECKED GOOD.SDR SWIA2026081377251Frame Splice · corrodedFOUND RT SPLICE AT FRAME, BS 605, STR 20R CORRODED. REMOVED AND REPLACED THE FRAME SPLICE IAW DWG 601R36026, REV AF, & SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
See all 207 reports