- Registered owner
- Skywest Airlines Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 10169
- Year built
- 2004
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 29, 2025
- Certificate issued
- November 20, 2018
- Expires
- November 30, 2028
- Mode S code
- AA25A6
From the FAA registry file of October 24, 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 · 76
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1997 | 2 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 3 |
| 2004 | 4 |
| 2005 | 4 |
| 2006 | 3 |
| 2007 | 5 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2017 | 3 |
| 2018 | 2 |
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 7 |
| 2022 | 9 |
| 2023 | 9 |
| 2024 | 5 |
| 2025 | 8 |
| 2026 | 7 |
Airframe · Bombardier CL-600-2C11
AD 2026-15-16Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-08-02StabilizersInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · GE CF34 series
SAIB NE-04-77NTSB investigations
No NTSB investigations matched to N753EVMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2C11 aircraft
FAA incident reports
No FAA accident or incident reports matched to N753EVMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bombardier CL-600-2C11 aircraft
Service difficulty reports · 282
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SWIA202503270019Skin · dentedFOUND VERTICAL DENT ON AFT PART OF R/H FUSELAGE BELOW R/H ENGINE ASSY. DAMAGE LOCATION FOUND TO BE APPROXIMATELY 0.5" INCHES AFT OF THE AFT RIVET LINE OF FRAME 1051.3. DENT SPANS VERTICALLY APPROXIMATELY 6 INCHES AND INTERSECTS STGR 14R AT THE DENT MID-POINT. SDR SWIA20241024Roller · failed inspLH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED CLOSED)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.SDR SWIA202412261024Roller · failed inspLH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED OPEN)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.
See all 282 reportsSTCs that may be installed · 18
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 18 STCs