Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
10314
Year built
2010
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 26, 2010
Certificate issued
March 17, 2021
Expires
March 31, 2028
Mode S code
ABF6A4

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 132

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2002In forceSuperseded2026
ADs by the year they took effect: 161 ADs
20022
20037
20043
20051
20064
20086
20099
201014
20119
20129
20134
20147
20154
201610
20176
201811
20196
20206
20217
20228
20239
20246
20256
20267
See all 161 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N870DCMatched 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-600-2C10 aircraft

FAA incident reports

No FAA accident or incident reports matched to N870DCMatched 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-600-2C10 aircraft

Service difficulty reports · 12

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

SDR SWIA2024022800007Bottle · warning messageAT NEXT OVERNIGHT MX BASE VISIT TROUBLESHOOT REPEAT CARGO BOTTLE LO CAUTION MESSAGE INFLIGHTMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 3205 FILED CLOSED)FEB 27, 2024 STATION: YUM--UPON ARRIVAL TO AIRCRAFT INTERROGATED MDC AND FOUND B1 008350. TROUBLESHOT PEFeb 27, 2024 · N870DC · Cndair CL6002C10 · Extinguishing SystemSDR SWIA202306210009Unknown · corrodedR/H FUSELAGE BELOW WL 72.5 AND AFT OF FS 977.00 PANEL 196DR HAS POSSIBLE EVIDENCE OF CORROSION AT MULTIPLE FUSELAGE ANCHOR NUT LOCATIONS. (C-CHECK RO 6/19/2023) PERFORMED PERMANENT REPAIR TO THE R/H FUSELAGE SKIN BELOW WL 72.5 AND AFT OF FS 977.00. REF Jun 6, 2023 · N870DC · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202306210007Unknown · cracked*SLAT CANISTER SUPPORT BRKT CRACKED UNDER FUEL PANEL #651AB (MARKED) (C-CHECK RO 6/19/2023) REPAIRED R/H SLAT TRACK 1-3, SLAT CANNISTER #3 SUPPORT BRACKET. REF. BOMBARDIER REO 670-57-42-577 REV. --, DATED 2016-12-02 AND MHIRJ REO 670-57-42-1418 REV--, DMay 26, 2023 · N870DC · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202306210002Unknown · corrodedANTENNA DOUBLER CORRODED BETWEEN FS295 AND FS310 AT STGR 27. (C-CHECK RO 6/19/2023) REMOVED OLD DOUBLER AND INSTALLED NEW TCAS ANTENNA DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG SH670-30023 REV. G. COMPLIEDMay 18, 2023 · N870DC · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202306120012Unknown · gougedCENTER FUSELAGE LEFT OUTBOARD SEAT RAIL FS797.0 GOUGED (MARKED) (C-CHECK RO 6/19/2023) REMOVED CENTER FUSELAGE, LEFT-OUTBOARD SEAT RAIL AT FS797.00 AND INSTALLED NEW SEAT RAIL. REF. CRJ700 A.M.M. 53-00-49-400-801-A10May 13, 2023 · N870DC · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202306210011Unknown · gougedSIDE SEAT RAIL RIGHT AFT GOUGED (MARKED) (C-CHECK RO 6/19/2023) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS.861.00- FS.969.00 WITH NEW DUE TO OUT OF LIMIT BLEND-OUT REF. CRJ 700 AMM 53-00-49-400-801-A10 TORQUE WRENCH USED TUC4978 DUE 31-AUG-23.May 12, 2023 · N870DC · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202306210010Unknown · corrodedCENTER FUSELAGE FLOOR OUTBOARD SEATRAIL FS863.0 HAS CORROSION (MARKED) (C-CHECK RO 6/19/2023) REMOVED CENTER FUSELAGE FLOOR, OUTBOARD SEATRAIL AT FS863.00, AND REPLACED WITH NEW SEAT RAIL. REF. CRJ700 A.M.M. 53-00-49-400-801-A10.May 12, 2023 · N870DC · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202306210008Unknown · corroded*CORROSION NOTED ON FRAME 295 BETWEEN STRG25L-STRG26R (C-CHECK RO 6/19/2023) REPAIRED CORROSION NOTED ON FRAME 295 BETWEEN STRG25L-STRG26R REF. CRJ 700 SRM 53-00-06-201-006-A01. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.COMPLIED WITH TASK CARD 51-900-May 11, 2023 · N870DC · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202306210003Unknown · cracked* FORWARD EQUIPMENT COMPARTMENT, L/H SIDE FLOOR WEB IS CRACKED AT FS193, MARKED. (C-CHECK RO 6/19/2023) PERFORMED PERMANENT REPAIR TO FORWARD EQUIPMENT COMPARTMENT, L/H SIDE FLOOR WEB. COMPLIED WITH AND COMPLETED ALL STEPS IN REO670-53-11-509 REV -E DATMay 11, 2023 · N870DC · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202306210001Unknown · corroded*CORROSION NOTED ON FRAME 349 BETWEEN STRG27-STRG26L (C-CHECK RO 6/19/2023) REPAIRED CORROSION NOTED ON FRAME 349 BETWEEN STRG27-STRG26L REF. SRM 51-42-06-001-001-A01 AND IAW CRJ 700 SRM 51-42-21-001-001-A01 AND DWG DWG SH690-31350 REV. M SEE CONTINUATIMay 11, 2023 · N870DC · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA20230510Unknown · crackedL/H UPPER TRANSCOWL INBD "A" STANDOFF BRACKET IS CRACKED. (C-CHECK RO 6/19/2023) REMOVED DAMAGED/CRACKED STAND-OFF ANGLE & INSTALLED NEW STAND-OFF ANGLE P/N CN624-2082-201 AT I/B LOCATION ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. A, 2017/05/1May 10, 2023 · N870DC · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2023062100013Unknown · corroded* AFT FUSELAGE TO WING FAIRING SUPPORT FRAME AT FS 939.00 HAS CORROSION ON LOWER FLANGE NEAR CENTER AND AROUND SEVERAL SCREW HOLES ON LOWER SIDE OF LOWER FLANGE. (C-CHECK RO 6/19/2023) REMOVED AND REPLACED PART P/N-SH670-39189-3 WITH NEW ONE . REF: CRMay 8, 2023 · N870DC · Cndair CL6002C10 · Aerodynamic Fairings

STCs that may be installed · 165

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 165 STCs