Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000644
Year built
2017
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 6, 2017
Certificate issued
April 6, 2017
Expires
April 30, 2030
Mode S code
A1B162

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 N208SYMatched 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 N208SYMatched 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 · 12

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

SDR SWIA2025011300048Beam · corrodedR/H REAR BEAM CORRODED FR 87 (C-CHECK RO 12/31/2024 - FILED CLOSED) REMOVED AND REPLACED RH LONGITUDINAL REAR BEAM AT FRAME 87 REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUATION CARD FOR WORK DEDec 14, 2024 · N208SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA20240113214Shear Panel · corrodedCORROSION UNDER AFT WET AREA RH SHEAR PANEL ON IB SIDE (C-CHECK RO 12/31/2024 - FILED CLOSED) PERFORMED CUTOUT SPLICE REPAIR OF FRAME 87 FLOOR CROSSBEAM BELOW RH SHEAR PANEL, REF ETD2024-170-033315. NO CHANGE TO WEIGHT AND BALANCE REQUIRED DUE TO REPAIRDec 14, 2024 · N208SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202501020003Beam · corrodedR/H REAR BEAM CORRODED FR 87 (C-CHECK RO 12/31/2024 - FILED OPEN) REMOVED AND REPLACED RH LONGITUDINAL REAR BEAM AT FRAME 87 REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUATION CARD FOR WORK DETADec 14, 2024 · N208SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA202501020014Frame · corrodedCORROSION UNDER AFT WET AREA RH SHEAR PANEL ON IB SIDE (C-CHECK RO 12/31/2024 - FILED OPEN) PERFORMED CUTOUT SPLICE REPAIR OF FRAME 87 FLOOR CROSSBEAM BELOW RH SHEAR PANEL, REF ETD2024-170-033315. NO CHANGE TO WEIGHT AND BALANCE REQUIRED DUE TO REPAIR PDec 14, 2024 · N208SY · Emb ERJ170200LR · Fuselage Main, FrameSDR SWIA20240113209Skin · dentedADM# N208SY-8348- DENT FOUND NEAR MAIN CABIN DOOR. ON BOTTOM, LEFT SIDE OF FWD LEFT HAND PASSENGER DOOR. DENT DAMAGE TO FUSELAGE SKIN LOCATED BETWEEN FR12 & FR13 AND BETWEEN STGR 16L & STGR 15L. EVALUATE DENT RECONTOUR AND REMOVE EVIDENCE IF POSSIBLE. (C-Dec 9, 2024 · N208SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202501020009Skin · dentedADM# N208SY-8348- DENT FOUND NEAR MAIN CABIN DOOR. ON BOTTOM, LEFT SIDE OF FWD LEFT HAND PASSENGER DOOR. DENT DAMAGE TO FUSELAGE SKIN LOCATED BETWEEN FR12 & FR13 AND BETWEEN STGR 16L & STGR 15L. EVALUATE DENT RECONTOUR AND REMOVE EVIDENCE IF POSSIBLE. (C-Dec 9, 2024 · N208SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202266154None · corrodedFWD WET AREA HAS CORROSION ON LH DOUBLER AT FR 19 AS MARKED. (C-CHECK RO 7/23/2022) REMOVED AND REPLACED FWD WET AREA LH DOUBLER AT FR 19, REF SRM 51-40-08.Jul 6, 2022 · N208SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202266153None · corrodedAFT WET AREA HAS CORROSION ON FLOOR SPLICE AT FR 90-91 RH SIDE. (C-CHECK RO 7/23/2022) REMOVED AND REPLACED FLOOR SPLICE AT FR 90-91 RH SIDE REF EMB 170/175 SRM 51-40-08. REF CONINUATION CARD FOR CORRECTIVE ACTION DETAILS.Jul 6, 2022 · N208SY · Emb EMB110* · Fuselage Internal Mounting StructureSDR SWIA202266149None · elongatedL/H AFT WINDSCREEN FRAME 84 OUTBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) PERFORMED TEMPORARY REPAIR TO L/H AFT WINDSCREEN FRAME 84 OUTBD UPPER MOUNT REF ETD2022-170-023331. THIS TEMPORARY REPAIR IS VALID FOR 7500FC AS OF JUL 13, 2022.Jul 3, 2022 · N208SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202266152None · elongatedR/H AFT WINDSCREEN FRAME 84 OTBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED R/H AFT WINDSCREEN FRAME 84 OTBD UPPER MOUNT REF SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-06Jul 2, 2022 · N208SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202266151None · elongatedR/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED R/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT. REF SRM 51-40-08.Jul 2, 2022 · N208SY · Emb EMB110* · Fuselage Structure (General)SDR SWIA202266150None · elongatedL/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED L/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT, REF SRM 51-40-08.Jul 2, 2022 · N208SY · Emb EMB110* · Fuselage Structure (General)

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