N161SY
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 2016-12-04 | 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.
36 reports on file, 2016-12-12 – 2026-06-02.
Part: SKIN — DENTED (ZONE 200) · airframe 24,643 hrs · 14,953 cycles
INSPECTED SKIN DEFORMATION/DENT OBSERVED BTWN FR10 & FR12, STR 14 THROUGH STR 16, DAMAGED AREA INITIATES APPROX 2.00 IN FWD OF FR10 & EXTENTS AFT TO FR12. OVERALL AFFECTED AREA MESSURES 27.0 IN IN LENGTH & 7 INCHES IN WIDTH, WITH A MAX DEPTH OF 0.204 IN ALONG WITH A DENT/GOUGE LOCATED AT STR 15 & FR 11 INTERSECTION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01AD/02. DAMAGE OUT OF LIMITS & REPAIR. CLASSIFIED AS A MAJOR REPAIR. PERFORMED REPAIR TO DAMAGED AREA ON LT FWD FUSELAGE AREA BETWEEN FR10 & FR12, STGR-14 THROUGH STGR-16 IAW ETD 2026-170-009627-A,
Earlier reports · 2016–2024 · 35 reports
2024
Part: FLAP TRACK — DAMAGED (ZONE 500) · airframe 20,182 hrs · 11,973 cycles
L/H FLAP TRACK #2A OUTBOARD HAS WIDTH REDUCTION DAMAGE WITH A MAXIMUM LOSS OF .40 MM. TC2-8916 CAL DUE 11-20-24. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH #2A OB FLAP TRACK REF EMB AMM 57-54-25-400-801-A TW: TC2-7543 CAL DUE: 05/13/2025
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 20,182 hrs · 11,973 cycles
CORROSION, AFT WET AREA, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 7/22/2024) PERFORMED PERMANENT SPLICE REPAIR ON RH INBD FLOOR BEAM SEAT TRACK FR 83-84 REF. ETD2022-170-022163 REV. B. CHANGE IN WEIGHT MEASURES 308.96 GRAMS. WEIGHT LESS THAN 2.5 LBS, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. CAL. TOOL I.D.# SH2-10286, DUE DATE 4-22-25. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,182 hrs · 11,973 cycles
LH OB LATERAL SEAT TRACK FROM FR 74 TO FR 84 HAS CORROSION AS MARKED. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH OB LATERAL SEAT TRACK FROM FR 74 TO FR 84 REF EMB SRM 51-40-08. SEAT TRACK REPLACED WITH OEM PART NO CHANGES TO WEIGHT AND BALANCE NOTED
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 20,182 hrs · 11,973 cycles
MAIN CABIN FLOOR STRUCTURE LEFT OUTBOARD SEAT TRACK SECTION FR 34/43 - 59 HAS GOUGING AT FRS 45, 47, 51, 53, 55, 57 AND 59. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH OB SEAT TRACK FR 34-59 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,182 hrs · 11,973 cycles
RH IB FLOOR SEAT TRACK HAS MULTIPLE AREAS WHERE CORROSION IS PRESENT AS MARKED FR 23- FR 34 (C-CHECK RO 7/22/2024) REMOVED AND REPLACED RH IB FLOOR SEAT TRACK FR 23- FR 34 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,182 hrs · 11,973 cycles
LH IB FLOOR SEAT TRACK HAS MULTIPLE AREAS WHERE CORROSION IS PRESENT AS MARKED FR 30- FR 34 (C-CHECK RO 7/22/2024) REMOVED AND REPLACED R/H I/B SEAT TRACK BETWEEN FR23 - FR34 REF: SRM 51-40-08. REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 20,182 hrs · 11,973 cycles
SHEAR CLIP AT FR 84 AND STR 28 CORRODED. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED SHEAR CLIP AT FR 84 BETWEEN STR 28R -27R REF: SRM 51-40-08
2023
Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 18,761 hrs · 10,979 cycles
TRANSFER FROM EAML 1239521 : WRITE UP FROM EAML 1239214. FOUND GOUGE IN SKIN AT FRAME 20.5 AND STRINGER 9 TO BE .042" DEEP, 1.5 INCHES LONG, AND 0.249 INCHES WIDE. (FILED CLOSED)REPAIR ACCOMPLISHED BY MHIRJ REFER TO SOW MIS-4505 DATED 11/11/2023 - I/A/W ETD 2023-170-027824 REV B DATED NOV 8 2023
2021
Part: NONE — CRACKED · airframe 13,988 hrs · 7,851 cycles
LH LOWER FUSELAGE FRAME 52 L-ANGLE HAS A CRACK EMANATING FROM THE OUTBOARD MOST RIVET. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L-ANGLE AT LH LOWER FUSELAGE FRAME 52. / REF SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
CORROSION, FORWARD WET AREA, ON LH FLOOR BEAM BETWEEN FR19 AND FR20 AROUND WINDSCREEN MOUNTING POINT. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H FLOOR BEAM BETWEEN FR 19 AND FR 20 AROUND WINDSCREEN MOUNTING POINT. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H O/B SPLICE AT FR. 87-88 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H O/B SPLICE AT FR. 87-88. REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H I/B BEAM AT FR.86-88 HAS 5(EA) AREAS OF CORROSION. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H I/B BEAM AT FR.86-88 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H O/B SPLICE AT FR.87-88 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H O/B SPLICE PLATE BETWEEN FRAMES 87-88. / REF SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H I/B SPLICE AT FR.89 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H I/B SPLICE AT FR.89 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
CROSSBEAM AT R/H FR.84 CORRODED IN 4(EA) PLACES AS MARKED. (C-CHECK RO 10/28/2021) FABRICATED AND INSTALLED REPAIR DOUBLER REF EMB ETD2021-170-033929 AND EMB SRM 53-00-10 REPAIR 03. SEE ATTACHED CONTINUATION CARD FOR ALL WORK ACCOMPLISHED.
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H INTERCOSTAL AT FR.90-91 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H INTERCOSTAL AT FR 90-91 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H I/B SPLICE AT FR.89 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H I/B SPLICE AT FR 89 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED
Part: NONE — CRACKED · airframe 13,988 hrs · 7,851 cycles
COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H I/B SEAT TRACK HAS 2(EA) AREAS OF CORROSION BETWEEN FR.84-85 (C-CHECK RO 10/28/2021) BLENDED R/H I/B SEAT TRACK 2(EA) AREAS OF CORROSION BETWEEN FR.84-85NOMINAL THICKNESS .195" MATERIAL REMOVED .195" WITHIN ALLOWABLE LIMITS OF ETD 2021-170-033926. RESTORED SURFACE PROTECTION REF ETD 2021-170-033926. SEE CONTINUATION CARD FOR WORK PERFROMED.
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H SPLICE AT FR.91 CORRODED AT 6(EA) FASTENERS AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H SPLICE AT FR 91 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H I/B SEAT TRACK CORRODED AT FR.84 AS MARKED. (C-CHECK RO 10/28/2021) REPAIRED CORROSION ON LH IB SEAT TRACK BY SPLICE REPAIR PER ETD2021-170-033946 WEIGHT OF REPAIR PARTS IS 227 GRAMS .RESTORED SURFACE PROTECTION REF SRM 51-23-06. SEE CONTINUATION FOR WORK PERFORMED.
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H SPLICE AT FR.90 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H SPLICE AT FR 90 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
CORROSION, FORWARD WET AREA, ON RH INBOARD SEAT TRACK (FR12 TO FR20/21 SEGMENT) IN 2 LOCATIONS AT FR17/18 AND FR20/21. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED RH INBOARD SEAT TRACK FR12 TO FR20/21 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H SPLICE AT FR.90 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H SPLICE AT FR.90 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
CORROSION, FORWARD WET AREA, ON LH INBOARD SEAT TRACK (FR12 TO FR20/21 SEGMENT) BETWEEN FR19 AND FR20. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED LEFT HAND INBOARD SEAT TRACK BEAM BETWEEN FRAMES 13-20 (FWD WET AREA). / REF SRM 51-40-08
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H I/B BEAM AT FR.86-88 HAS 6(EA) AREAS OF CORROSION. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED R/H I/B BEAM AT FR 86-89 REF EMB SRM 51-40-08. R/H I/B BEAM REPLACED WITH OEM PART NO CHANGE TO WEIGHT
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
L/H INTERCOSTAL BETWEEN FR. 90-91 CORRODED AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H INTERCOSTAL BETWEEN FR. 90-91 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
CORROSION AFT WET AREA, ON L/H ANGLE SUPPORT ATTACHED TO INTERCOSTAL BETWEEN FR. 90-91 IS CORRODED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L/H ANGLE SUPPORT ATTACHED TO INTERCOSTAL BETWEEN FR. 90-91 REF EMB SRM 51-40-08. SEE ATTACHED CONTINUATION CARD FOR ALL WORK ACCOMPLISHED.
Part: NONE — CORRODED · airframe 13,988 hrs · 7,851 cycles
R/H INTERCOSTAL AT FR.89-90 CORRODED IN 2(EA) PLACES AS MARKED. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED INTERCOSTAL AT FR 89-90 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06
2016
Part: STRINGER — DAMAGED (FRAMES 5-6) · airframe 1,320 hrs · 748 cycles
STRINGER 20L DAMAGED BETWEEN FRAMES 5 AND 6. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: ANGLE — DAMAGED (FRAMES 2-4) · airframe 1,320 hrs · 748 cycles
DAMAGED ANGLE FROM FRAMES 2-4 BETWEEN STRINGERS 26 AND 28R. REMOVED AND REPLACED THE ANGLE IAW SRM.
Part: ATTACH FITTING — DAMAGED (FRAME 8) · airframe 1,320 hrs · 748 cycles
LWR ATTACH FLANGE AT FRAME 8 IS DAMAGED. REMOVED AND REPLACED THE ATTACH FLANGE IAW SRM.
Part: STRINGER — CRACKED (FRAME 4) · airframe 1,320 hrs · 748 cycles
STRINGER 28L IS CRACKED AT FRAME 4. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: STRINGER — DAMAGED (FRAME 4) · airframe 1,320 hrs · 748 cycles
STRINGER 24R DAMAGED AT FRAME 4. REMOVED AND REPLACED THE STRINGER IAW SRM.
Part: LANDING GEAR — COLLAPSED (NOSE) · airframe 1,310 hrs · 740 cycles
DIVERTED DUE TO A NOSE GEAR DISAGREE, ON LANDING THE NOSE GEAR COLLAPSED AT AROUND 90KTS. REPAIRED IAW AMM AND SRM.