Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000621
Year built
2016
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
December 14, 2016
Certificate issued
December 13, 2016
Expires
December 31, 2029
Mode S code
A26801

From the FAA registry file of October 24, 2026.

On this page

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 N254SYMatched 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 N254SYMatched 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 · 10

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

SDR SWIA2025072800023Windshield · cracked2 CRACKS OBSERVED IN CAPTAINS SIDE WINDSHIELD. TOP RIGHT CORNER. (FLIGHT 3794 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30545140 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPTAINS WINDSHIELD PER ERJ 175 AMM 56-11-00. LEAK AJul 23, 2025 · N254SY · Emb ERJ170200LR · Flight Compartment WindowsSDR SWI2025F00494Floorbeam · corrodedFRAME 84 CROSSBEAM BETWEEN R/H FLOOR BEAM AND OTBD SILL CORRODED AS MARKED. (C-CHECK RO 04/21/2025)PERFORMED CUTOUT SPLICE REPAIR TO THE FRAME 84 CROSSBEAM BETWEEN RH FLOOR BEAM AND RH OUTBOARD SILL AND TRIMMED OUT NUTPLATE BRACKET OB EDGE P/N 170-66797-001 Mar 26, 2025 · N254SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA202504210326Seat Track · gougedRH INBOARD SEAT TRACK SEGMENT FR 73-85 IS GOUGED AT FR 74/75, 76/77, 77/78, 78/79, 79/80, 80/81, 81/82, 82/83, AND 83/84 (C-CHECK) REMOVED AND REPLACED R/H INBOARD SEAT TRACK SEGMENT BETWEEN FR 73 - FR 85 REF. SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERMar 26, 2025 · N254SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2024052400021Lever · warning messageAFTER TAKEOFF WE SELECTED LANDING GEAR UP. THE GEAR DID NOT GO UP FOR APPROXIMATELY 60 SECONDS. WE DID RECEIVE A LG LEVER DISAG MASTER WARNING. GEAR WENT UP WHEN WE SELECTED FLAPS 1. WE RAN QRH THEN RETURNED TO THE DEPARTURE AIRPORT. (FLIGHT 3698 FILED CLOSED)May 21, 2024 · N254SY · Emb ERJ170200LR · Landing Gear SelectorSDR SWIA2024052200021Landing Gear · slowAFTER TAKEOFF WE SELECTED LANDING GEAR UP. THE GEAR DID NOT GO UP FOR APPROXIMATELY 60 SECONDS. WE DID RECEIVE A LG LEVER DISAG MASTER WARNING. GEAR WENT UP WHEN WE SELECTED FLAPS 1. WE RAN QRH THEN RETURNED TO THE DEPARTURE AIRPORT. THIS IS CURRENTLY A WORK IMay 21, 2024 · N254SY · Emb ERJ170200LR · Landing Gear Retraction/Extension SystemSDR SWIA202266321None · odorBURNT SMELL IN FLIGHT DECK AT GATE. (FLIGHT#4076 FILED CLOSED) INSPECTED COCKPIT FOUND OBSERVERS OVERHEAD READING LIGHT ASSY TO BE CAUSE OF BURNING SMELL. REMOVED AND REPLACED OBSERVERS READING LIGHT ASSY IN REF TO AMM 33-11-03. OPS AND SMELL CHECK GOOD.Aug 18, 2022 · N254SY · Emb EMB110* · Air Conditioning SystemSDR SWIA202265940Rail · damagedR/H FLAP TRACK 1A HAS THICKNESS REDUCTION DAMAGE ON UPPER FORWARD SURFACE MEASURED AT .12MM. (C-CHECK RO 6/15/2022) R/H FLAP TRACK 1A REMOVED AND REPLACED. REF AMM57-54-25 / TW:TC1-458 / DUE:7-22-22May 25, 2022 · N254SY · Emb EMB110* · AileronsSDR SWIA202265939None · damagedL/H FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE AT UPPER FORWARD SURFACE MEASURED AT .26MM. (C-CHECK RO 6/15/2022) REMOVED AND REPLACED L/H FLAP TRACK 1A. REF EMB-175 AMM 57-54-25. TW TC2-7543 CAL DUE 5-10-23May 25, 2022 · N254SY · Emb EMB110* · AileronsSDR SWIA202265938None · damagedL/H FLAP TRACK #2 A OUTBOARD HAS WIDTH REDUCTION DAMAGE ON UPPER AND LOWER SURFACE MEASURED AT 1.18MM. (C-CHECK RO 6/15/2022) REMOVED AND REPLACED L/H FLAP TRACK #2 A OUTBOARD HAS WIDTH REDUCTION DAMAGE ON UPPER AND LOWER SURFACE REFERENCE APPLICABLE STMay 25, 2022 · N254SY · Emb EMB110* · Aileron TabsSDR SWIA202265941None · corrodedCENTER INTERCOSTAL SPLICE AT FR90 HAS CORROSION AS MARKED (C-CHECK RO 6/15/2022) REMOVED AND REPLACED WITH NEW INTERCOSTAL SPLICE AT FR90. RESTORED PROTECTIVE FINISH, APPLIED CIC. NO FURTHER DEFECTS NOTED. REF SRM 51-40-02, SRM 51-40-08 SRM 51-23-04, SRMay 23, 2022 · N254SY · Emb EMB110* · Fuselage Main, Longeron/Stringer

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