N142SY
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | on 2021-10-01 | Operator named in NTSB report |
Accident & incident history
Operated by SKYWEST AIRLINES INC (per NTSB report)
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.
34 reports on file, 2020-08-21 – 2025-08-05.
Part: APU — ODOR (ZONE 100) · airframe 26,206 hrs · 15,477 cycles
FAÃâ¬â¢S SMELLED STRONG PLASTIC BURNING SMELL. PAX SMELLED TOO. (FLIGHT 5577 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30613473 WITH THE FOLLOWING CORRECTIVE ACTION: "REF CP CP 30619772 FOR WORK PERFORMED. PERFORMED ENGINE RUNS TO TA POWER, TURNED OFF APU BLEED AIR COULD NOT SMELL PLASTIC OR SMOKE SMELL."
Part: UNKNOWN — ODOR (CABIN) · airframe 26,166 hrs · 15,451 cycles
FAS SMELLED STRONG PLASTIC BURNING ODOR. PAX SMELLED TOO. PLEASE REFERENCE AML 1673468
Part: UNKNOWN — ODOR (CABIN) · airframe 25,184 hrs · 14,781 cycles
APPROXIMATELY ONE MIN AFTER TAKEOFF FWD FLIGHT ATTENDANT REPORTED VERY STRONG SMELL OF BURNING WIRES IN FWD GALLEY, DID NOT REPORT SMOKE. RETURNED TO COS. FLIGHT ATTENDANT REPORTED THE SMELL LASTED ABOUT 5 MINUTES. (FLIGHT 5325 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29730555 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE FOLLOWING CP'S FOR CORRECTIVE ACTIONS:29733068297331992973319729732255"
Part: UNKNOWN — ODOR (CABIN) · airframe 25,160 hrs · 14,762 cycles
APPROXIMATELY ONE MIN AFTER TAKEOFF FWD FLIGHT ATTENDANT REPORTED VERY STRONG SMELL OF BURNING WIRES IN FWD GALLEY, DID NOT REPORT SMOKE. RETURNED TO COS. FLIGHT ATTENDANT REPORTED THE SMELL LASTED ABOUT 5 MINUTES. (FLIGHT 5325 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
Earlier reports · 2020–2023 · 30 reports
2023
Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
CORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 27R-28R. (C-CHECK RO 6/9/2023) REMOVED AND REPLACED SHEAR CLIP AT FR 88 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08
Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
CORROSION ON WASTE BOX DOUBLER SURFACE AT WASTE DOOR HINGE AS MARKED. (C-CHECK RO 6/9/2023) REMOVED CORROSION AT WASTE BOX DOUBLER BY INSTALLING OUTER REPAIR DOUBLER AT FRAME 88, STRGS 26R-27R. SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 53-23-60-REPAIR 01P. REPAIR PARTS WEIGHT 471.9 GRAMS (LESS THAN 2.5 LBS) NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: UNKNOWN — SCRATCHED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
RH, O/B SEAT TRACK, SCRATCHED, GOUGED, SHOWS EVIDENCE OF CORROSION AT FR45, FR46, FR47, FR48, FR50, FR53, FR54, FR55, FR57, FR58, AND FR59 (C-CHECK RO 6/9/2023) REMOVED AND REPLACED RH O/B SEAT TRACK BETWEEN FR45-59 REF EMB SRM 51-40-08. NO WEIGHT AND BALANCE CHANGE REQUIRED DUE TO REPLACING WITH NEW SEAT TRACK.
Part: UNKNOWN — SCRATCHED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
LH, I/B SEAT TRACK, SCRATCHED, GOUGED, SHOWS EVIDENCE OF CORROSION AT FR60 AND FR73 AS MARKED. (C-CHECK RO 6/9/2023) REMOVED AND REPLACED LH INBOARD SEAT TRACK FR 59-74, REF EMB175 SRM 51-40-08. NO WEIGHT AND BALANCE CHANGE REQUIRED DUE TO REPLACING WITH NEW SEAT TRACK.
Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
CORROSION IN R/H I/B SEAT TRACK AT SEAT MOUNT LOCATIONS FROM FR. 73-84. (C-CHECK RO 6/9/2023) REMOVED AND REPLACED RH INBD SEAT TRACK AT FRAMES 73-84 REF SM 51-40-08. NO WEIGHT AND BALANCE CHANGE REQUIRED, REPLACED WIH NEW SEAT TRACK.
Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 21,194 hrs · 12,007 cycles
CORROSION IN L/H I/B SEAT TRACK AT SEAT MOUNT LOCATIONS FROM FR. 73-84. (C-CHECK RO 6/9/2023) REMOVED AND REPLACED LH IB SEAT TRACK AT FR 73-84. REF EMB SRM 51-40-08
2020
Part: ATTACH BOLT — CORRODED (RT MLG DOOR) · airframe 14,842 hrs · 8,136 cycles
RT MLG MID DOOR LOWER ATTACH BOLT CORRODED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED RT MLG MID DOOR LOWER ATTACH BOLT, REF AMM TQ 605 CAL 2-19-21.
Part: SEAT TRACK — CORRODED (FRAMES 84-85) · airframe 14,842 hrs · 8,136 cycles
CORROSION, LT INBOARD SEAT TRACK AT FR.84-85, MARKED. C-CHECK RO 9/8/2020. REMOVED CORROSION AND REPAIRED LT INBOARD SEAT TRACK AT FR 84-85. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION FOR WEIGHT OF REPAIR PARTS, REF EMB175 SRM.
Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · airframe 14,842 hrs · 8,136 cycles
CORROSION, PANEL SUPPORT AT FR.90-91 Y= -11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED PANEL SUPPORT AT FR 90-91 Y= -11. APPLIED TOPCOAT TO NEW PANEL SUPPORT, REF EMB175 SRM.
Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · airframe 14,842 hrs · 8,136 cycles
CORROSION, INTERCOSTAL AT FR.90-91 Y=11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED INTERCOSTAL AT FR.90-91 Y=11, PER REF SRM. SEE CONTINUATION CARD FOR WORK PERFORMED.
Part: BEAM — CORRODED (FRAME 87) · airframe 14,842 hrs · 8,136 cycles
CORROSION, LT BEAM AT FR.87 Y= -11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED LT BEAM AT FR 87 Y=-11, REF EMB175 SRM.
Part: SPLICE — CORRODED (FRAME 89) · airframe 14,842 hrs · 8,136 cycles
CORROSION, SPLICE AT FR.89 Y= 11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED SPLICE AT FR 89 Y = 11, REF EMB175 SRM.
Part: CLOSEOUT PANEL — CHAFED (FWD CARGO DOOR) · airframe 14,842 hrs · 8,136 cycles
FWD CARGO DOOR CUTOUT CLOSEOUT PANEL CHAFFED AS MARKED. C-CHECK RO 9/8/2020. LOCATED AND DRILLED NEW FWD CARGO DOOR CUTOUT CLOSEOUT PANEL, REF EMB SRM.
Part: DOUBLER — CORRODED (COCKPIT FLOOR) · airframe 14,842 hrs · 8,136 cycles
CORROSION, ON LEFT SIDE FLIGHT DECK FLOOR DOUBLER JUST FORWARD AND TO THE LEFT OF THE PILOT CONTROL COLUMN, AS MARKED. C-CHECK RO 9/8/2020. REMOVED FLOOR DOUBLER AND INSTALLED NEW REPAIR DOUBLER, PER EMB ETD.
Part: SPLICE — CORRODED (FRAME 90) · airframe 14,842 hrs · 8,136 cycles
CORROSION, SPLICE AT FR.90 Y=11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED SPLICE AT FR 90, REF SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SPLICE — CORRODED (FRAME 90) · airframe 14,842 hrs · 8,136 cycles
CORROSION, SPLICE AT FR.90 Y= -11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED SPLICE AT FR 90 Y=-11, REF EMB175 SRM.
Part: SPLICE — CORRODED (FRAME 90) · airframe 14,842 hrs · 8,136 cycles
CORROSION, SPLICE AT FR.90 Y=22, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED SPLICE AT FRAME 90 Y=22, MARKED, REF EMB175 SRM.
Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · airframe 14,842 hrs · 8,136 cycles
CORROSION, INTERCOSTAL AT FR.90-91 Y= -11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPACED AFT WET AREA INTERCOTAL AT FR 90-91 Y= -11. RESTORED SURFACE PROTECTION TO NEW INTERCOSTAL, REF EMB175 SRM.
Part: BEAM — CORRODED (FRAME 87) · airframe 14,842 hrs · 8,136 cycles
CORROSION, RT BEAM AT FR.87 Y= 11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED AFT WET AREA RT BEAM AT FRAME 87, REF EMB175 SRM. REPLACEMENT OF BEAM DID NOT MAKE A CHANGE TO THE WEIGHT AND BALANCE.
Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · airframe 14,842 hrs · 8,136 cycles
CORROSION, PANEL SUPPORT AT FR.90-91 Y=11, MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED PANEL SUPPORT AT FR 90-91, REF SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: PLATE — CORRODED (FRAMES 13-14) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON RIGHT FORWARD SILL PLATE BETWEEN FRAMES 13 AND 14, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FORWARD WET AREA RIGHT FORWARD SILL PLATE BETWEEN FRAMES 13 AND 14, REF EMB SRM.
Part: FLOOR SUPPORT — CRACKED (FRAMES 11-12) · airframe 14,842 hrs · 8,136 cycles
FLIGHT DECK FLOOR SUPPORT BRACKET CRACKED ON AFT END OF THE CONNECTOR FWD FUSELAGE SUPPORT BETWEEN FRAMES 11 AND 12, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FLOOR SUPPORT BRACKET BETWEEN FRAMES 11-12, REF SRM.
Part: CROSSBEAM — CORRODED (FRAME 17) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON FRAME 17 FLOOR CROSS BEAM NEAR THE CENTER OF THE BEAM ON THE UPPER FLANGE, AS MARKED. C-CHECK RO 9/8/2020. REMOVED CORROSION AND REPAIRED FWD WET AREA FRAME 17 UPPER FLANGE NEAR CENTER OF BEAM, REF EMB175 SRM.
Part: DOUBLER — CORRODED (FRAMES 19-20) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON FLOOR DOUBLER AROUND THE LEFT FORWARD WINDSCREEN INBOARD FLOOR MOUNT BETWEEN FR 19 AND 20, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FWD WET AREA FLOOR DOUBLER BETWEEN FR19 AND FR20, REF EMB175 SRM.
Part: PLATE — CORRODED (FRAME 17) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON RIGHT AFT SILL PLATE FORWARD EDGE AT FRAME 17, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FWD WET AREA RT AFT SILL PLATE AT FR17, REF EMB175 SRM.
Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 14,842 hrs · 8,136 cycles
FLIGHT DECK FLOOR SUPPORT BRACKET CRACKED AT FRAME 12 ON PILOTS SIDE, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FLIGHT DECK FLOOR SUPPORT BRACKET AT FRAME 12 ON PILOTS SIDE. REF EMB175 SRM.
Part: SEAT TRACK — CORRODED (FRAME 12-21) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON LEFT MOST INBOARD SEAT TRACK SEGMENT FRAME 12 TO FRAME 20/21 IN THE FOLLOWING 2 LOCATIONS: BETWEEN FR 19 AND 20; AND FR 20, AS MARKED. C-CHECK RO 9/8/2020. REMOVED AND REPLACED FWD WET AREA LT INBOARD SEAT TRACK FR 12 TO FR 20/21. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF EMB175 SRM.
Part: SEAT TRACK — CORRODED (FRAMES 12-21) · airframe 14,842 hrs · 8,136 cycles
CORROSION, FORWARD WET AREA ON RIGHT INBOARD SEAT TRACK SEGMENT FRAME 12 TO FRAME 20/21 IN THE FOLLOWING 4 LOCATIONS: BETWEEN FR 12 AND 13; BETWEEN FR 13 AND 14; FR 14, AND FR 17, AS MARKED. 21424322 C-CHECK RO 9/8/2020. REMOVED AND REPLACED FWD WET AREA RT INBOARD SEAT TRACK FRAME 12 TO 20/21. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF EMB175 SRM.
Part: STIFFENER — SHEARED (BULKHEAD) · airframe 14,842 hrs · 8,136 cycles
RT WHEEL WELL FR 56 AFT PRESSURE BULKHEAD VERTICAL STIFFENER HAS SHEARED RIVET HEAD. C-CHECK RO 9/8/2020. REMOVED AND REPLACED RIVET (1) EA ON RT WHEEL WELL FR 56 AFT PRESSURE BULKHEAD VERTICAL STIFFENER AND RESTORED SURFACE PROTECTION RIVET HEAD, REF SRM.
Part: FAIRING — DAMAGED (LEFT) · airframe 14,842 hrs · 8,136 cycles
COMPOSITE DAMAGE TO REAR FUSELAGE DRAIN FAIRING. C-CHECK RO 9/8/2020. AFTER FURTHER EVALUATION OF THE FWD REAR FUSELAGE DRAIN FAIRING, DAMAGE IS THROUGH FAIRING ON LEFT SIDE. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED REAR FUSELAGE DRAIN FAIRING, REF EMB SRM.