Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
10260
Year built
2006
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
July 6, 2021
Certificate issued
March 2, 2025
Expires
March 31, 2032
Mode S code
A7619B

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 45

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

2004In forceSuperseded2026
ADs by the year they took effect: 50 ADs
20041
20081
20131
20172
20191
20203
20217
20228
20238
20245
20256
20267
See all 50 ADs

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations

No NTSB investigations matched to N575GJMatched 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 N575GJMatched 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 · 15

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

SDR SWIA2026081876943Skin · dentedDURING BIRD STRIKE INSPECTION FOUND DENT IS IN THE RIGHT FUSELAGE PANEL BETWEEN THE UPPER INBOARD TRU DOOR AND THE RADOME. FOUND DENT TO BE 2.5" LONG BY 1.5" WIDE BY 0.187 DEEP. STARTING AT THE EDGE OF THE TRU DOOR CUTOUT AND EXTENDING FORWARD 1.5". DENT IS OAug 18, 2026 · N575GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026061876245Fmc · failedFMS FAILURE IN FLIGHT (FLIGHT 5654). REMOVED AND REPLACED FMC NR 1 IAW AMM 34-61-07. OPS CHECK GOOD AT THIS TIME.Jun 18, 2026 · N575GJ · Cndair CL6002C11 · Flight Management Computing Hardware SystemSDR N6WA2025020701Frame · corrodedFRAME 863.00 CORRODED BETWEEN STR26L AND STR26R. REPAIRED FRAME AT 863.00 BETWEEN STR26L AND STR26R IAW MHIRJ (BOMBARDIER) REO 670-53-51-332.Feb 6, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, FrameSDR N6WA2025020505Skin · dentedDENT FOUND ON RH SIDE OF RUDDER BETWEEN RS78.82 - RS72.79. REPAIRED RUDDER IAW CJR SRM 55-41-01 AND GOJET EO C550-55MR -002-0.Feb 5, 2025 · N575GJ · Cndair CL6002C11 · Rudder, Plate/SkinSDR N6WA2025020504Strap · corrodedCIRCUMFERAL STRAP AT FS280 AT AT STR27 TO STR26R IS CORRODED. REPAIRED CIRCUMFERALSTRAP AT FS280 AT STR27 TO STG26R IAW STS EA 109-2025-005 AND GOJET EO C550-53MR -051-0.Feb 5, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR N6WA2025013101Frame · corrodedFRAME AT FS364.00 BETWEEN STRINGER 26R-25R IS CORRODED. REPAIRED FRAME AT FS364.00 BETWEEN STRINGERS 24LH AND 24RH IAW GOJET EO C550/700-53MR-006 REV O AND MHIRJ REO 670-53-21-687.Jan 31, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, FrameSDR N6WA2025013002Stringer · corrodedSTRINGER 25L SPLICE AT FS333.00 IS CORRODED. REMOVED AND REPLACED STRINGER 25L SPLICE AT FS333.00 IAW CRJ SRM 51-42-06.Jan 30, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025013001Stringer · corrodedSTRINGER 26L SPLICE AT FS333.00 IS CORRODED. REMOVED AND REPLACED STRINGER 26L SPLICE AT FS333.00 IAW CRJ SRM 51-42-06.Jan 30, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025012706Stringer Splice · corrodedSTRINGER SPLICE 25R FS333 IS CORRODED. REPLACED STINGTER SPLICE 25R AT FS333 IAW CRJ SRM 51-42-21Jan 26, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025012705Longeron · corrodedSTGR 25R HAS CORROSION AT FS333-FS349. REPLACED STGR25R AT FS 333-FS 364 IAW CRJ SRM 51-42-06.Jan 26, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025012202Floor Support · corrodedFLOOR POST FS280 RBL11.16 CORROSION. REPLACED FLOOR POST AT FS280 RBL11.16 IAW SRM 51-42-20.Jan 21, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2025011901Stringer · corrodedSTRINGER 25R CORRODED AT FS295-FS319.70. REPLACED STRINGER 25R BETWEEN FS250-FS333 IAW CRJ SRM 51-42-06.Jan 19, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025011902Stringer · corrodedSTINGTER 26R CORRODED AT FS295-FS319.70. REPLACED STINGER 26R BETWEEN FS280-FS333 IAW CRJ SRM 51-42-06.Jan 17, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2025011201Intercostal · corrodedINTERCOSTAL AT STGR 20R BETWEEN FS310-FS319 CORRODED. REPLACED INTERCOSTAL AT STGR20R BETWEEN FS310-FS319 IAW CRJ SRM 51-42-20.Jan 10, 2025 · N575GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2021101001Battery · inoperativeEMERGENCY LIGHTS INOP. R/R EMERGENCY LIGHT POWER SUPPLY #3 IAW CRJ 550 AMM 33-51-17, OPS CHECK GOOD.Oct 10, 2021 · N575GJ · Cndair CL600* · Emergency Lighting

STCs that may be installed · 17

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

See all 17 STCs