N118SY
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
27 reports on file, 2017-02-14 – 2026-08-19.
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND RIVET AT 26L AND FR15 BURNT AND DEFORMED DUE TO LIGHTING STRIKE.? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ 26L AND FR15 IN REFERENCE TO ERJ 175 SRM 51-43-04. SEE CP 32876138 FOR LEAK CHECK.
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND MELTED RIVET ON FR12 1 IN UP OFF 26L 1/2 RADIUS DUE TO LIGHTING STRIKEÃâ¬? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR12 AND STR 26L IN REFERENCE TO SRM 53-00-00/REPAIR 03P
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND A RIVET ON FR13 JUST ABOVE 25L MELTED DUE TO LIGHTING STRIKE 1/2 RADIUS ̉SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR13 JUST ABOVE STR 25L IN REFERENCE TO ERJ 175 SRM 51-43-04. SEE CP 32876138 FOR LEAK CHECK.
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND AN ENTRANCE POINT OF LIGHTING STRIKE, LOOKS WELDED AT 2"BELOW 25L JUST OFF FR13 1/2 IN RADIUSÃâ¬? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. (FILED CLOSED)COMPLIED WITH PERMANENT BLENDING REPAIR OF " AN ENTRANCE POINT OF LIGHTING STRIKE, LOOKS WELDED AT 2"BELOW 25L JUST OFF FR13 1/2 IN RADIUS" PER ETD2026-170-014368 REV.: A.
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND 3 BURN MELTED SPOTS ABOVE 25L BY 1/2 IN BETWEEN FR12 AND FR13 ONE IS 1/4 RADIUS ONE IS 1/2 IN RADIUS AND ONE IS 3/4 RADIUS ALL GROUPED TOGETHER IN 1 IN 1/4" LONG DUE TO LIGHTING STRIKEÃâ¬? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. (FILED CLOSED)COMPLIED WITH PERMANENT BLENDING REPAIR FOR Ãâ¬Å3 BURN MELTED SPOTS ABOVE 25L BY 1/2 IN BETWEEN FR12 AND FR13 ONE IS 1/4 RADIUS ONE IS 1/2 IN RADIUS AND ONE IS 3/4 RADIUS ALL GROUPED TOGETHER IN 1 IN 1/4" LONG DUE TO LIGHTING STRIKEÃâ¬? PER ETD2026-170-014368 REV.: A. DATED 8/21/2026
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND LIGHTNING STRIKE ENTRANCE POINT ON RIVET AT STGR27L NEXT TO FRAME 18 (FILED CLOSED)REPLACED 1 DAMAGED RIVET ON LH SKIN @ STGR27L NEXT TO FRAME 18 IN REFERENCE TO ERJ 175 SRM 51-41-02**SEE CP 32576138 FOR LEAK/PRESSURE CHECK SIGN-OFF
Part: SKIN — DAMAGED (ZONE 100) · airframe 30,658 hrs · 18,142 cycles
FOUND RIVET BURNT AT 26L AND FR14 DUE TO LIGHTING STRIKEÃâ¬? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ STR 26L AND FR14 IN REFERENCE TO ERJ 175 SRM 51-43-04.
Earlier reports · 2017–2025 · 20 reports
2025
Part: SLAT TRACK — CHAFED (ZONE 600) · airframe 28,459 hrs · 16,696 cycles
RIGHT SLAT NR 4 TRACK RIB 8, INTERNAL OF SLAT CHAFED. REMOVED AND REPLACED RT SLAT PANEL NR 4 IAW AMM 27-81-08 & 30-11-06.
Part: BEAM — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
AFT WET AREA LH BEAM HAS CORROSION AT FR 87. INSTALLED AFT WET AREA LH BEAM BETWEEN FR86 - FR89 IAW SRM 51-40-08.
Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
FRAME 19 CROSSBEAM CORRODED OUTBOARD OF LH SEAT TRACK. PERFORMED PERMANTENT DOUBLER REPAIR ON THE CROSSBEAM IAW ETD2025-170-926443.
Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 28,459 hrs · 16,696 cycles
CORROSION AT AFT CARGO SHEAR CLIP AT FR 89 STGR 29R-29L REMOVED AND REPLACED AFT CARGO SHEAR CLIP AT FR 89 STGR 29R-29L REF: SRM 51-40-08.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
AFT WET AREA RT SEAT TRACK HAS CORROSION AT FR 87. REMOVED AND REPLACED AFT WET AREA RT SEAT TRACK BETWEEN FR86 - FR89 REF: SRM 51-40-08.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
PAX FLOOR, RT SEAT TRACK CORRODED AT FR17. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
PAX FLOOR, LT INBD SEAT TRACK CORRODED BETWEEN FRS 19-20. REMOVED AND REPLACED THE SEAT TRACK BETWEEN FR 12-20 IAW SRM 51-40-08.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
RIGHT SEAT TRACK HAS CORROSION AT FR 84, 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED AND REPLACED RT INBD SEAT TRACK FR74-84 REF SRM 51-40-08.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
PAX FLOOR, FR 14 CROSSBEAM CORRODED AT RH TRACK/ BEAM. PERFORMED SRM DOUBLER REPAIR AT PAX FLOOR, FR 14 CROSSBEAM AT RH TRACK REF SRM 53-00-10/REPAIR 03P. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06.CPM 51-25-00 (PO:331184)NO CHANGE TO WEIGHT AND BALANCE
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
LEFT SEAT TRACK HAS CORROSION AT FR 84, 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED DAMAGED SECTION OF THE LT CENTER SEAT TRACK AT FRAME 84 AND INSTALLED A FABRICATED FILLER AND DOUBLER TO REPAIR REF ETD2025-170-926606 AND REF ERJ175 SRM 51-40-08.
Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 28,459 hrs · 16,696 cycles
LEFT LATERAL SEAT TRACK HAS CHAFING DAMAGE AT FR 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08. REPLACED WITH NEW OEM PART,
Part: RIB — CRACKED (ZONE 300) · airframe 28,459 hrs · 16,696 cycles
RH HORIZONTAL STAB RIB 12 HAS SUSPECTED CRACK ON UPPER SIDE 4TH RIVET FROM THE FRONT BETWEEN FRONT SPAR AND UPPER SKIN STRINGER 2. REMOVED AND REPLACED RH HORIZONTAL STAB RIB 12 REF: SRM 51-40-08 ETD2025-170-926732 (P.O# 325561).
2024
Part: SEAT TRACK — CRACKED (SEAT 19C) · airframe 40,885 hrs · 29,865 cycles
THE SEAT FLOOR TRACK AT SEAT 19C IS CRACKED. (FILED CLOSED)REMOVED AND REPLACED THE SEAT FLOOR TRACK AT SEAT 19C IN REF TO AMM 25-21-11
2022
Part: NONE — CORRODED · airframe 21,020 hrs · 11,691 cycles
AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 82 STGR 27R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 82 STGR 27R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
Part: NONE — WORN · airframe 21,020 hrs · 11,691 cycles
RH WING FLAP TRACK 2A OB HAS WIDTH REDUCTION OF 1.1 MM DEEPEST LOCATION ENTIRE LENGTH. FOUND TO BE OUT LIMITS. ASST # QA-50384 DUE 2-21-23. (C-CHECK RO 7/1/2022) REMOVED AND REPLACED RH WING FLAP TRACK 2A OB IN REF WITH EMB 175 AMM 57-54-25 HG2-50002 DUE-5-3-23
Part: NONE — CORRODED · airframe 21,020 hrs · 11,691 cycles
AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 83 STGR 27R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 83 STGR 27R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
Part: NONE — WORN · airframe 21,020 hrs · 11,691 cycles
LH WING FLAP TRACK 2A OB HAS WIDTH REDUCTION OF 1.0 MM DEEPEST LOCATION ENTIRE LENGTH. FOUND TO BE OUT OF LIMITS. ASST # QA-50384 DUE 2-21-23. (C-CHECK RO 7/1/2022) REMOVED AND REPLACED LH WING FLAP TRACK 2A OB IN REF WITH EMB 175 AMM 57-54-25 HG2-50002 DUE-5-3-23
Part: NONE — CORRODED · airframe 21,020 hrs · 11,691 cycles
AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 85 STGR 26R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 85 STGR 26R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
2017
Part: DOUBLER — DAMAGED (NOT REPORTED) · airframe 7,256 hrs · 3,790 cycles
AFT DOUBLER DAMAGED. REPAIRED IAW ETD.
Part: DOUBLER — DAMAGED (NOT REPORTED) · airframe 7,256 hrs · 3,790 cycles
FWD DOUBLER DAMAGED. REPAIRED IAW ETD.