- Serial number
- 7881
- 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
- AD854A
- 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 N970SWMatched 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 · 205
SDR SWIA2026072276668Psu · faultedON MLG UP SELECTION, RECEIVED A/SKID INOP CAUTION FOLLOWED BY PARK BRAKE SOV CAUTION. NOTED AN AIRFRAME VIBRATION. MLG LEVER SELECTED IAW SOP, UP BUT FOUND MLG INDS TO BE DOWN & 3 GREEN. ON SELECTING MLG DOWN, CAUTION MESSAGES EXTINGUISHED & LANDED UNEVENTFSDR SWIA2026041877227Skin · crackedONE-OFF CRACK TO AFT LOWER WING PLANK, DWG 601R10046, 0300 THK AT CRACK LOCATION AFT EDGE AT WS 45 CRACK IS 0600 LONG AND STARTS FROM AFT EDGE OF AFT LOWER WING PLANK AT WS 450 FLIGHT 6080 . COMPLIED WITH PERMANENT REPAIR FOR CRACK DAMAGE AT LT AFT LOWER WINSDR SWIA2026041676737Skin · cracked1-OFF CRACK TO AFT LOWER WING PLANK AFT EDGE AT WS 45. CRACK IS 0.600? LONG AND STARTS FROM AFT EDGE OF AFT LOWER WING PLANK AT WS 45. COMPLIED WITH PERMANENT REPAIR FOR CRACK DAMAGE AT LHS AFT LOWER WING PLANK, AFT EDGE AT WS 45.00 IAW ALL STEPS OF REO 601R-
See all 205 reports