# N905J: 2003 Bombardier CL-600-2D24, registration cancelled 2025-06-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 23, 2025
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2D24](https://openairdocs.org/model/bombardier-cl-600-2d24) (registry code 1390016)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 15005
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 22, 2003
- Certificate issued: March 11, 2025
- Last registry action: March 11, 2025
- Mode S code: AC8287
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%20George)
- Owner type: Corporation
- Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N905J
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=905J
- Page: https://openairdocs.org/deregistered/N905J-2025-06-23

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2D24: https://openairdocs.org/model/bombardier-cl-600-2d24.md

## Service difficulty reports (334, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR MASA2023102000013](https://openairdocs.org/sdr/MASA2023102000013), Oct 20, 2023: UNKNOWN. UNKNOWN. AFT CEILING EMERG LIGHT INOP- MEL/SPLICED BROKEN WIRE ON AFT CEILING EMERG LIGHT -
- [SDR MASA2023102000134](https://openairdocs.org/sdr/MASA2023102000134), Oct 20, 2023: LIGHT. BURNED OUT. AFT CEILING EMERG LIGHT INOP. PLACED ON MEL
- [SDR MASA2023100400028](https://openairdocs.org/sdr/MASA2023100400028), Oct 4, 2023: UNKNOWN. UNKNOWN. LH FUEL QTY/TOTAL FUEL QTY DASHES IN FLT- R2 LT #2 AND #6 FUEL PROBES
- [SDR MASA2023100200026](https://openairdocs.org/sdr/MASA2023100200026), Oct 2, 2023: UNKNOWN. UNKNOWN. FWD EMERGENCY MISSING LIGHT BULB- RELAMPED
- [SDR MASA2023011200003](https://openairdocs.org/sdr/MASA2023011200003), Jan 12, 2023: BULB. BURNED OUT. ROW 18 CEILING EMER FLOOD LIGHT INOP. MXC DEFERRED WITH CREW.
- [SDR MASA2022120600268](https://openairdocs.org/sdr/MASA2022120600268), Dec 9, 2022: BULB. INOPERATIVE. ROW 13 A FLR LVL EXIT SIGN (1) BULB INOP. REPLACED BULB
- [SDR MASA2022082900220](https://openairdocs.org/sdr/MASA2022082900220), Aug 29, 2022: NONE. NONE. FLAP FAIL CAUTION (EMERGENCY DECLARED). RESET SFECU AND CLEARED INHIBITS, OPS CHECK GOOD.
- [SDR MASA2022040900100](https://openairdocs.org/sdr/MASA2022040900100), Apr 9, 2022: NONE. NONE. 13A EMERGENCY EXIT SIGN-1 BULB INOP. REPLACED BULB.
- [SDR MASA2022040900099](https://openairdocs.org/sdr/MASA2022040900099), Apr 9, 2022: NONE. NONE. SERVICE DOOR EXIT SIGN-2 BULBS INOP. REPLACED BULBS.
- [SDR MASA2022030300071](https://openairdocs.org/sdr/MASA2022030300071), Mar 3, 2022: NONE. NONE. GEAR DISAGREE WARN IN FLIGHT -EMER DECLARED. AIRCRAFT CURRENTLY OOS.
- [SDR MASA20220208108](https://openairdocs.org/sdr/MASA20220208108), Feb 8, 2022: NONE. CRACKED. THE LBL 12.00 FLOOR BEAM (P/N: CC670-33202-15) WAS FOUND WITH A CRACK. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) 53-11-43-001-001-A0
- [SDR MASA20220204104](https://openairdocs.org/sdr/MASA20220204104), Jan 25, 2022: NONE. CORRODED. SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM 
- [SDR MASA20220204103](https://openairdocs.org/sdr/MASA20220204103), Jan 25, 2022: NONE. CORRODED. SLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER
- [SDR MASA20220204102](https://openairdocs.org/sdr/MASA20220204102), Jan 25, 2022: NONE. CORRODED. SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM 
- [SDR MASA20220204101](https://openairdocs.org/sdr/MASA20220204101), Jan 25, 2022: NONE. CORRODED. SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM 
- [SDR MASA20220204100](https://openairdocs.org/sdr/MASA20220204100), Jan 25, 2022: NONE. CORRODED. SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE U
- [SDR MASA20220204099](https://openairdocs.org/sdr/MASA20220204099), Jan 25, 2022: NONE. NONE. SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE U
- [SDR MASA20220204098](https://openairdocs.org/sdr/MASA20220204098), Jan 25, 2022: NONE. NONE. SLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER
- [SDR MASA20220204097](https://openairdocs.org/sdr/MASA20220204097), Jan 25, 2022: NONE. NONE. SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE U
- [SDR MASA20211223647](https://openairdocs.org/sdr/MASA20211223647), Dec 23, 2021: NONE. NONE. THE MAINTENANCE DISCOVERED CRACK ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-14-06, FIG. 51-14-06-991-815, 51-23-00 AND SRM 51-21-16.
- [SDR MASA20211223646](https://openairdocs.org/sdr/MASA20211223646), Dec 23, 2021: NONE. NONE. THE PYLON DETACHABLE TRAILING EDGE ASSEMBLY WAS FOUND TO HAVE EROSION DAMAGE AFFECTING THE ALUMINUM MESH. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-73-00-201
- [SDR MASA20211221644](https://openairdocs.org/sdr/MASA20211221644), Dec 21, 2021: ACCESS PANEL. NONE. THE RH WING L/E SLAT# 2 ACCESS PANEL 63102 WAS FOUND TO HAVE AN ELONGATED FASTENER HOLE. PERFORMED PERMANENT REPAIR IAW CRJ900 IPC 57-42-32, FIG. 5, ITEM 125 (R
- [SDR MASA20211221645](https://openairdocs.org/sdr/MASA20211221645), Dec 21, 2021: NONE. CRACKED. THE LH ENGINE LOWER TRANSCOWL INNER SKIN WAS FOUND TO HAVE 11 SMALL CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 54-21-05-991-801, ITEMS 2&3 (REV. 38 DATED
- [SDR MASA20211221643](https://openairdocs.org/sdr/MASA20211221643), Dec 21, 2021: NONE. DENTED. THE LONGERON SIDE FITTING FUEL VENT AND THE WELDED TUBE ASSEMBLY WERE FOUND TO HAVE DENTS ON THE OUTER SURFACE OF THE TUBES. PERFORMED PERMANENT REPAIR IAW CRJ9
- [SDR MASA20211221642](https://openairdocs.org/sdr/MASA20211221642), Dec 21, 2021: NONE. NONE. THE PASSENGER DOOR FWD SEAL STRIKER WAS FOUND BENT COMMON TO THE OUTBOARD FLANGE OF THE STRIKER. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-23-001-001-A01,
- [SDR MASA20211221641](https://openairdocs.org/sdr/MASA20211221641), Dec 21, 2021: NONE. NONE. THE LOWER FUSELAGE SKIN PANEL WERE REPORTED WITH TOTAL OF FOUR ZONES WITH MULTIPLE NICK DAMAGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-01-991-806, ITE
- [SDR MASA20211221640](https://openairdocs.org/sdr/MASA20211221640), Dec 21, 2021: FLOORBEAM. CORRODED. THE CROSSBEAM WAS FOUND TO HAVE SEVERE CORROSION DAMAGE ON THE UPPER FLANGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-43-001-A02, FIG. 53-21-43-991-802, 
- [SDR MASA20211221639](https://openairdocs.org/sdr/MASA20211221639), Dec 21, 2021: NONE. NONE. THE LH WING L/E SLAT 1 T/E WEDGE WAS FOUND WITH AN EXISTING DAMAGE BLENDOUT.AT THE AFT EDGE, BETWEEN SLAT TRACK 1-2 AND SLAT TRACK 1-3. PERFORMED PERMANENT REPA
- [SDR MASA20211221638](https://openairdocs.org/sdr/MASA20211221638), Dec 21, 2021: PANEL. NONE. A MISS DERILLED HOLE WAS FOUND ON THE RH OUTBOARD LEADING EDGE ACESS PANEL #632EB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-42-32-991-801, 29A (REV 38 DATED
- [SDR MASA20211221637](https://openairdocs.org/sdr/MASA20211221637), Dec 21, 2021: NONE. NONE. THE RH WING SLAT #3 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (I
- [SDR MASA20211221636](https://openairdocs.org/sdr/MASA20211221636), Dec 20, 2021: NONE. NONE. THE RH WING SLAT #2 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (I
- [SDR MASA20211221635](https://openairdocs.org/sdr/MASA20211221635), Dec 20, 2021: NONE. NONE. THE RH WING SLAT #1 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (I
- [SDR MASA20211221634](https://openairdocs.org/sdr/MASA20211221634), Dec 20, 2021: NONE. NONE. THE FUSELAGE SKIN LOWER PANEL WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEM
- [SDR MASA20211221633](https://openairdocs.org/sdr/MASA20211221633), Dec 20, 2021: NONE. NONE. THE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-003-A02 ITEM 1A, D AND E (REV.38 DATED 9 JU
- [SDR MASA20211221632](https://openairdocs.org/sdr/MASA20211221632), Dec 20, 2021: NONE. NONE. THE FUSELAGE LH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-002-A02 ITEM 1, C, AND D (REV.38 DATED 9 JUL 2
- [SDR MASA20211221631](https://openairdocs.org/sdr/MASA20211221631), Dec 20, 2021: NONE. NONE. THE FUSELAGE RH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-004-A02 ITEM 1, A, AND D (REV.38 DATED 9 JUL 2
- [SDR MASA20211221630](https://openairdocs.org/sdr/MASA20211221630), Dec 20, 2021: NONE. NONE. A CRACK WAS DISCOVERED ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CR7/9 SRM 53-11-01-991-810, ITEM 1A (CRJ7/9 REV. 38 DATED JUL 9TH, 2021).
- [SDR MASA20211221629](https://openairdocs.org/sdr/MASA20211221629), Dec 20, 2021: NONE. NONE. THE UPPER CAP OF THE CENTER FUSELAGE FLOOR BEAM WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-43-991-801, ITEM 2A (REV. 33
- [SDR MASA20211221628](https://openairdocs.org/sdr/MASA20211221628), Dec 20, 2021: NONE. NONE. SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27
- [SDR MASA20211221627](https://openairdocs.org/sdr/MASA20211221627), Dec 20, 2021: NONE. NONE. SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27
- [SDR MASA20211221626](https://openairdocs.org/sdr/MASA20211221626), Dec 20, 2021: NONE. NONE. SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27
- [SDR MASA20211221625](https://openairdocs.org/sdr/MASA20211221625), Dec 20, 2021: NONE. NONE. THE FORWARD AND AFT SEAL CARRIERS OF THE AFT SERVICE DOOR PLUG WAS FOUND TO HAVE (2) CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 52-46-07 FIG. 52-46-07-99
- [SDR MASA20211221624](https://openairdocs.org/sdr/MASA20211221624), Dec 20, 2021: NONE. NONE. THE PASSENGER DOOR INNER SKIN WAS FOUND WITH A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-24-36, 51-21-16, 51-23-00. DEFECT LOCATION: FWD PASSENGER DOO
- [SDR MASA20211221623](https://openairdocs.org/sdr/MASA20211221623), Dec 17, 2021: NONE. NONE. THE LOWER FUSELAGE SKIN PANEL HAD A PREVIOUS REPAIR INSTALLED PER REO 690-53-21-989 THAT CONFLICTED WITH THE OPERATOR RECOMMENDED SERVICE BULETIN 670BA-53-057 T
- [SDR MASA20211221622](https://openairdocs.org/sdr/MASA20211221622), Dec 17, 2021: NONE. NONE. THE LH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-12-00, SRM 51-40-11-001-001.
- [SDR MASA20211221621](https://openairdocs.org/sdr/MASA20211221621), Dec 17, 2021: NONE. DENTED. THE FUSELAGE LOWER SKIN PANEL WAS FOUND TO HAVE THREE PROTRUDING DENTS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01, FIG. 53-21-01-991-802, ITEM 1 (REV. 
- [SDR MASA20211130595](https://openairdocs.org/sdr/MASA20211130595), Nov 30, 2021: NONE. NONE. FUSELAGE LOWER SKIN PANEL AT FS394.00 AND STGR20L -STGR21L WAS FOUND TO HAVE A PREVIOUS BLENDOUT, PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-00
- [SDR MASA20211130594](https://openairdocs.org/sdr/MASA20211130594), Nov 30, 2021: NONE. NONE. LH MAIN LANDING GEAR HYDRAULIC INTERFACE IN THE MLG BAY BETWEEN WS 14.50 AND WS 68.00 WAS FOUND WITH MISSING MATERIAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/90
- [SDR MASA20211129582](https://openairdocs.org/sdr/MASA20211129582), Nov 24, 2021: NONE. NONE. L/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 51-13-02, EA 69-2021-201.
- [SDR MASA20211129581](https://openairdocs.org/sdr/MASA20211129581), Nov 24, 2021: NONE. NONE. L/H WING LEADING EDGE SLAT NO. 2 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 69-2021-200.

All 334: https://openairdocs.org/deregistered/N905J-2025-06-23/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20051004026609I](https://openairdocs.org/incident/20051004026609I), Oct 4, 2005: Cndair CL6002D24 (N905J), Memphis, TN. (-23) Emergency evacuation only, no injuries or casualties. ASH6185 reported westbound on "p" taxiway to Memphis ground one & was instructed to continue via…

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