Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000588
Year built
2016
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 26, 2016
Certificate issued
August 25, 2016
Expires
August 31, 2029
Mode S code
A23914

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 66

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: 81 ADs
20041
20051
20079
20088
20093
201011
20114
20123
20135
20142
20161
20175
20181
20191
20204
20213
20227
20235
20242
20253
20262
See all 81 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N242SYMatched 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 LR aircraft

FAA incident reports

No FAA accident or incident reports matched to N242SYMatched 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 LR aircraft

Service difficulty reports · 11

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

SDR SWIA2026091077111Spring · damagedFWD SERVICE DOOR FWD EVACUATION SLIDE FITTING SPRING HAS NO TENSION. REMOVED AND REPLACED FWD SERVICE DOOR FWD EVACUATION SLIDE FITTING ASSY IAW AMM 53-10-25 OPS CHECK GOOD AT THIS TIME.Sep 10, 2026 · N242SY · Emb ERJ170200LR · Escape SlideSDR SWIA20250311216Skin · gougedFWD FUSELAGE LOWER SKIN GOUGED AS MARKED BETWEEN FRAMES 21-22 STRINGER 27L. (C-CHECK RO 1/9/2025) CUT AWAY DAMAGE ON FWD FUSELAGE LOWER SKIN BETWEEN FRAMES 21-22 STRINGER 27L. FABRICATED AND INSTALLED DOUBLER REPAIR PER ETD. REF: ETD2024-170-033341 REDec 16, 2024 · N242SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA20250110216Skin · gougedFWD FUSELAGE LOWER SKIN GOUGED AS MARKED BETWEEN FRAMES 21-22 STRINGER 27L. (C-CHECK RO 1/9/2025) CUT AWAY DAMAGE ON FWD FUSELAGE LOWER SKIN BETWEEN FRAMES 21-22 STRINGER 27L. FABRICATED AND INSTALLED DOUBLER REPAIR PER ETD. REF: ETD2024-170-033341 REDec 16, 2024 · N242SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2024042300001Window · crackedFIRST OFFICERS SIDE DV WINDOW HAS A ROCK CHIP JUST AFT OF CENTER AND MIDWAY UP FROM BOTTOM EDGE. CHIP IS DEVELOPING TWO CRACKS. CRACK ONE IS HALF INCH LONG RUNNING AFT FROM CHIP. CRACK TWO IS QUARTER INCH LONG RUNNING DOWN FROM CHIP. REMOVED AND REPLACED RT DApr 21, 2024 · N242SY · Emb ERJ170200LR · Flight Compartment WindowsSDR SWIA2023081601Unknown · gougedTWO GOUGES ON LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 16L- STGR 17L (FILED CLOSED)REPAIRED LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 17L- STGR 18L, IN REF. TO ETD2023-170-019944, REV. A. COMPLETED 51-00-00-002-SKY-U AND M-337. **NOTE** STRINGER 16L WAS IAug 10, 2023 · N242SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2023081101Unknown · gougedTWO GOUGES ON LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 16L- STGR 17L (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSAug 10, 2023 · N242SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202264307None · crackedSUSPECTED CRACK RH WING LEADING EDGE SPAR 1 OUTBD EXTENSION / (C-CHECK RO 2/15/2022) REMOVED AND REPLACED RH WING LEADING EDGE SPAR 1 OTBD EXTENSION REF E175 SRM 51-40-08.Feb 4, 2022 · N242SY · Emb ERJ170200LR · Wing StructureSDR SWIA202264313None · wornLH WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .97MM AT FWD END (C-CHECK RO 2/15/2022) REMOVED AND REPLACED LH INBOARD AFT FLAP TRACK. REF EMB-175 AMM 57-54-25. SEE CONTINUE CARD FOR WORK PERFORMED.Jan 30, 2022 · N242SY · Emb ERJ170200LR · Wing, Landing Gear Attach FittingsSDR SWIA202264304None · corrodedCORROSION CF III R/H CROSSFRAME 84 (C-CHECK RO 2/15/2022) PERFORMED CF III R/H CROSSFRAME 84 REINFORCEMENT DOUBLER REPAIR REF ETD2022-170-003349. SEE CONTINUATION CARD FOR WORK PERFORMED. THIS REPAIR DOES NOT ADVERSELY AFFECT A FATIGUE CRITICAL STRUCTUJan 30, 2022 · N242SY · Emb ERJ170200LR · Fuselage Main, FrameSDR SWIA202264303None · corrodedRH FLOOR BEAM SEAT TRACK CORRODED ON TRACK EDGE AT FR 17 (C-CHECK RO 2/15/2022) REMOVED AND REPLACED RH FLOOR BEAM SEAT TRACK FR 12/FR21 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. REPLACED SEAT TRACK WITH SAME PART. NO CHANGE IN WEIGHT Jan 28, 2022 · N242SY · Emb ERJ170200LR · Fuselage, Powerplant Attach FittingsSDR SWIA202264301None · corrodedAFT WET AREA- LH FLOOR BEAM 2" FWD FR 86-89 ; LBL12" HAS CORROSION; MARKED. (C-CHECK RO 2/15/2022) REMOVED AND REPLACED LH FLOOR BEAM FR 86-89 LBL 12 REF ERJ 175 SRM 51-40-08 SEE CONTINUE CARD FOR WORK PERFORMED.Jan 28, 2022 · N242SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure

STCs that may be installed · 63

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

See all 63 STCs