Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000636
Year built
2017
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 9, 2017
Certificate issued
March 9, 2017
Expires
March 31, 2030
Mode S code
A1A63D

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 N205SYMatched 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 N205SYMatched 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 · 15

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

SDR SWIA2025090819Shear Tie · corrodedCORROSION - SHEAR CLIP AT FR88 BETWEEN STR 27R/28R (C-CHECK RO 09/05/2025)REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR 88 BETWEEN STR 27R/28R REF. EMB SRM 51-40-08. RESTORED SURFACE PROTECTION. SEE CONTINUATION CARD FOR WORK PERFORMED.Aug 19, 2025 · N205SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWI2025F01195Seat Track · corrodedPASSENGER CABIN L/H SEAT TRACK AT FR 84/85 HAS CORROSION (C-CHECK RO 09/05/2025)EVALUATED CORROSION ON PASSENGER CABIN L/H SEAT TRACK AT FR 84/85 AND REMOVED DAMAGE BY BLENDING. DAMAGE 1 (UPPER FLANGE) DAMAGE IS FOUND OUT OF LIMITS. REF EMB SMR 53-23-10/AD01.Aug 13, 2025 · N205SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2025F01194Beam · corrodedCORROSION - LH BEAM BETWEEN FR87/88 (C-CHECK RO 09/05/2025) REMOVED AND REPLACED LH BEAM BETWEEN FR 87/88 REF EMB SRM 51-40-08Aug 13, 2025 · N205SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA2025090813Beam · corrodedCORROSION - RH BEAM BETWEEN FR87/88 (C-CHECK RO 09/05/2025)REMOVED AND REPLACED RH BEAM BETWEEN FR85-89. REF EMB SRM 51-40-08. REPAIRCOMPLETED WITH FACTORY REPLACEMENT PART THERE IS NO CHANGE TO AIRCRAFT WEIGHT AND BALANCE.. SEE CONTINUATION CARD FOR WORK ACCAug 13, 2025 · N205SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA202406060001Switch · failedPRKG BRK NOT RELEASED CAUTION MESSAGE COMPLIED WITH QRH EAP 13-6 EMERGENCY DECLARED (FLIGHT 5454 FILED CLOSED)PERFORMED TROUBLESHOOTING FOR PRKG BRK NOT RELEASED REF FIM 32-41-00, SLAVED IN PARKING BRAKE PRESS SWITCH FOR #2 SYSTEM, DID NOT FIX, REMOVED AND REPJun 6, 2024 · N205SY · Emb ERJ170200LR · Landing Gear Brake SystemSDR SWIA202266581None · damagedREF AML 1005421 CATERING TRUCK HITTING AC: FOUND DAMAGE IS A HOLE APPROXIMATELY 6.25 INCHES LONG BY APPROXIMATELY 4.5 INCHES WIDE IN TOTAL WIDTH LOCATED ON THE BOTTOM OF THE TAIL CONE. IN ADDITION TO THE HOLE, THERE IS BUCKLING IN THE AREA OF THE HOLE, WITH THOct 3, 2022 · N205SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202265971None · failedCA AIRSPEED AND ALT FAILED ON CLIMB OUT (FLIGHT 4629 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25053405 WITH THE FOLLOWING CORRECTIVE ACTION: "AFTER INTERROGATING THE AIRCRAFT, FOUND CAUTION MESSAGE REFERENCING ADS PROBE 1 FAILURE CIJun 25, 2022 · N205SY · Emb EMB110* · Air Data ComputerSDR SWIA202265966None · crackedANGLE IS CRACKED AT LH SIDE BELLY PANEL RIB 52 ATTACH POINT. (C-CHECK RO 6/23/2022) REMOVED AND REPLACED L ANGLE AT LH SIDE BELLY PANEL RIB 52 REF SRM 51-40-08.Jun 8, 2022 · N205SY · Emb EMB110* · Fuselage Main, FrameSDR SWIA202265965None · crackedFRAME 12 CENTER ANGLE BRACKET CRACKED ON COCKPIT FLOOR BEAM. (C-CHECK RO 6/23/2022) REMOVED AND REPLACED CENTER ANGLE BRACKET AT FRAME 12. / REF SRM 51-40-08Jun 8, 2022 · N205SY · Emb EMB110* · Fuselage Main, FrameSDR SWIA202265962None · wornLH WING FLAP TRACK 2A OUTBD SIDE HAS WIDTH REDUCTION APPROX. 1.4MM NOMINAL OF 21.0MM, A TOTALOF 4" IN LENGTH 1.4MM IS BEYOND ALLOWABLE BLEND LIMITS. CALIPER QA50384 CAL DUE 02-21-23 (C-CHECK RO 6/23/2022) REMOVED AND REPLACED L/H WING FLAP TRACK 2A OB WJun 8, 2022 · N205SY · Emb EMB110* · Aileron TabsSDR SWIA202265961None · wornRH WING FLAP TRACK 2A OUTBD SIDE HAS WIDTH REDUCTION OF 1.2MM NOMINAL IS 21.0MM WEAR IS BEYOND BLEND LIMITS CALIPER QA50384 CAL DUE 02-21-23 (C-CHECK RO 6/23/2022) REMOVED AND REPLACED RH WING FLAP TRACK 2A OUTBOARD. REF: EMB175 AMM 57-57-35, ASSET# Jun 8, 2022 · N205SY · Emb EMB110* · Aileron TabsSDR SWIA202265964None · crackedFRAME 52 WING TO FUSELAGE RIB STRUCTURE HAS CRACK IN OUTBOARD SURFACE. (C-CHECK RO 6/23/2022) / REMOVED AND REPLACED FRAME 52 TO FUSELAGE RIB STRUCTURE REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06, CPM 51-25-00.Jun 7, 2022 · N205SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202265960None · corrodedCORROSION ON BEAM CAP AROUND FASTENERS AT FR 87, Y= -273. (C-CHECK RO 6/23/2022) REMOVED AND REPLACED BEAM @ FRAME 87 REF SRM 51-40-08. APPLIED SURFACE PROTECTION AND CIC PROTECTION REF SRM 51-23-06 AND REF CPM 51-25-00. THIS REPAIR DOES NOT AFFECT WEIGJun 7, 2022 · N205SY · Emb EMB110* · Fuselage Main, FrameSDR SWIA202265959None · corrodedCORROSION ON BEAM CAP AROUND FASTENERS FR 87 AT Y= +273. (C-CHECK RO 6/23/2022) REMOVED AND REPLACED R/H BEAM AT FR 87 REF SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT AFFECT WEIGHT AND BALANCE.Jun 7, 2022 · N205SY · Emb EMB110* · Fuselage Main, FrameSDR SWIA202265963None · corrodedLH SILL PLATE AT FLOOR FRAME 19 HAS CORROSION AROUND FASTENER HOLE AS MARKED. (C-CHECK RO 6/23/2022) REMOVED AND REPLACED LH SILL PLATE AT FLOOR FRAME 19, REF SRM 51-40-08.Jun 6, 2022 · N205SY · Emb EMB110* · 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