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Aircraft record

N108SY2014 Embraer ERJ 170-200 LL

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply46 service difficulty reports

Registration
Valid
expires May 31, 2027
Based in
St George, UT
owner city / state
Owners
1
since 2014
NTSB events
None
since 1982
ADs may apply
7
confirm with A&P
Service reports
46
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Skywest Airlines INC
Owner type
Corporation
City, state
St George, UT
Certificate issued
May 23, 2014
Expires
May 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Nov 23, 2024

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Embraer
Model
ERJ 170-200 LL
Year
2014
Serial number
17000401
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
88
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A02413

Engine

Make and model
Ge Cf34-8e5
Type
Turbo-fan
Power
14,510 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2014 – nowSkywest Airlines INCSt George, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (7)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2025-01-05Time Limits/ Maintenance ChecksMar 17, 2025Airframe (ERJ 170-200 LL)Certain serial numbers: 17000002; 17000004–17000013; 17000015–17000948
2023-03-19InstrumentsApr 7, 2023Airframe (ERJ 170-200 LL)Serial numbers per ANAC AD 2022-05-03
2023-02-05Turbine Engine Combustion SectionMar 14, 2023Engine (CF34-8E5)
2022-16-01WindowsAug 15, 2022Airframe (ERJ 170-200 LL)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3.
2020-25-08Flight controlsJan 21, 2021Airframe (ERJ 170-200 LL)Serial numbers per ANAC AD 2020-05-01 (ERJ 170) and ANAC AD 2020-05-02 (ERJ 190)
Show all 7 ADs
ADSubjectEffectiveApplies to
2020-12-12Nacelles/ pylonsAug 13, 2020Airframe (ERJ 170-200 LL)
2019-19-03FuselageOct 31, 2019Airframe (ERJ 170-200 LL)Serial numbers per Embraer Service Bulletins SB170-53-0142 Rev 01, SB190-53-0098 Rev 01, and SB190LIN-53-0072 Rev 01

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (46)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuselage · shear panel · damagedSep 26, 2024

    ELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLING TO SPECIFIC DIAMETER TO REMOVE DAMAGE. INSTALLED BUSHING.SEE CONTINUATION CARD FOR WORK PERFORMED. REF ETD2024-170-026011 REV:A. THIS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedSep 25, 2024

    AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED CLOSED)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF: SRM 51-00-10/REPAIR 03P. WEIGHT OF…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 25, 2024

    AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED OPEN)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF: SRM 51-00-10/REPAIR 03P. WEIGHT OF…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDING. MAX MATERIAL REMOVED FOUND TO BE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDING. MAX MATERIAL REMOVED FOUND TO BE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedSep 24, 2024

    CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · gougedSep 23, 2024

    LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 46 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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