Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000736
Year built
2018
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
June 27, 2018
Certificate issued
June 26, 2018
Expires
June 30, 2028
Mode S code
A2B6FF

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 30

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: 35 ADs
20041
20051
20082
20091
20131
20172
20181
20191
20204
20213
20226
20235
20242
20253
20262
See all 35 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N274SYMatched 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 Embraer S A ERJ 170-200 LL aircraft

FAA incident reports

No FAA accident or incident reports matched to N274SYMatched 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 Embraer S A ERJ 170-200 LL aircraft

Service difficulty reports · 6

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

SDR SWIA2026061776362Skin · gougedDURING THE RECONTOUR OF THE DENT ON FWD FUSELAGE SKIN AT FR 1-2, STGR 12R-17R, THE MECHANIC WAS USING A RIVET GUN AND BUCKING BAR TO KNOCK OUT SOME FASTENERS TO GAIN ACCESS FOR THE RECONTOUR. DURING REMOVAL, THE BUCKING BAR CHATTERED ON THE SKIN CAUSING GOUGINJun 17, 2026 · N274SY · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR SWIA2026061476361Skin · damagedFASTENER HOLE ELONGATED EXTERNAL FUSELAGE SKIN FR19-19A STGR 18L-19L. REPAIRED ELONGATED HOLE ON EXTERNAL FUSELAGE SKIN FR19-19A STGR 18L-19L BY PERFORMING BUSHING REPAIR IAW REF SRM 51-10-07 AND ETD2026-170-010476 REV A.Jun 14, 2026 · N274SY · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR SWI2025F01453None · no discrepancySTRONG SMELL OF SMOKE DURING TAKEOFF IN BURBANK. BECAME VERY PRONOUNCED IN TO THRUST AND THEN DISSIPATED WHEN THRUST WAS REDUCED TO CLIMB. FLIGHT ATTENDANTS NOTICED THE STRONG SMELL OF SMOKE WHEN I CALLED THEM AT 10,000 FT. NO FURTHER ANOMALIES IN FLIGHT. (FOct 20, 2025 · N274SY · Emb ERJ170200LL · Standard Practices/StructuresSDR SWIA202412031129Slat System · failedSLAT FAIL CAUTION ON CLIMB OUT. MESSAGE CLEARED ONCE FLAP 1 SELECTED ON APPROACH (FLIGHT 3858 - FILED CLOSED) INTERROGATED CMC, FOUND NO ACTIVE FAULTS. BUT FAULT HISTORY FOR PREVIOUS LEG INDICATES 27811021ACE [SLAT SURFACE JAMMED/UNDERSPEED]. REFERENCINGNov 29, 2024 · N274SY · Emb ERJ170200LL · Leading Edge Slat Control SystemSDR SWIA20240417Seat Track · corrodedCORROSION, AFT WET AREA, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. REMOVED DAMAGED SECTION AND INSTALLED REPAIR SPLICE ON RT INBD SEAT TRACK AT FR 84-FR85 IN REF ETD2022-170022163. WEIGHT OF REPAIR: 62.2 OZ SEE CONTINUATION CARD FOR PO #'S. TApr 17, 2024 · N274SY · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091561082Bolt · wornRH AILERON CONTROL SYSTEM INBOARD PCU FAILED BACKLASH FUNCTIONAL TEST. (C-CHECK RO 9/14/21) / REMOVED AND REPLACED RH IB PCU TOGGLE LINK TO AILERON SURFACE BOLT, BUSHING, AND WASHERS, AND RE-CHECKED RH AILERON IB PCU BACKLASH. BACKLASH IS WITHIN SPECS. ASSETSep 7, 2021 · N274SY · Emb ERJ170200LL · Wing, Attach Fittings

STCs that may be installed · 20

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

See all 20 STCs