N125SY
Registered owner: SKY WEST 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.
28 reports on file, 2015-06-10 – 2024-05-20.
Part: FMS — OUT OF SEQUENCE · airframe 25,053 hrs · 14,404 cycles
FMS WOULD NOT SEQUENCE APPROACH PROPERLY GOING INTO OKC. WOULD ONLY LOAD BACK COURSE, TRIED MULTIPLE TIMES WITH MULTIPLE APPROACHES AND FMS WOULD ONLY LOAD BACK COURSE WHEN APPROACH WAS ARMED. DIVERTED BACK TO DIRECT TO DFW AND ARMED LNAV ABOUT 30MILES AWAY AND WHEN LNAV WAS PRESSED IT ACTIVATE A LOCALIZER. (FLIGHT 5220 FILED CLOSED)TROUBLE SHOT THE FMS SYSTEM PER FIM-5093 AND FOUND NO FAULTS TO THE FMS SYSTEM OR MESSAGES ASSOCIATED WITH APPROACH SEQUENCE. PERFORMED OPS CHECK OF THE FMS IN REFERENCE TO AMM 34-61-00 AND OPS CHECK GOOD. COULD NOT FIND ANY MESSAGES IN THE CMC IN REFERENCE TO AMM 45-45-00. COULD NOT DUPLICATE PROBLEM. NOTED FOR FURTHER PROBLEMS. OK FOR SERVICE.
Earlier reports · 2015–2023 · 27 reports
2023
Part: UNKNOWN — MISSING (UNKNOWN) · airframe 22,777 hrs · 12,799 cycles
THE SEAT TRACK AT SEAT 2A IS MISSING. (FILED CLOSED)REPLACED THE MISSING SEAT TRACK AT SEAT 2A IN REF TO AMM 25-21-11
Part: ACTUATOR — FAILED (SLAT SYS) · airframe 21,981 hrs · 12,265 cycles
SLAT FAIL IN FLIGHT, ARRIVED AT AIRCRAFT AND ATTEMPTED TO OPS CHECK SLAT SYSTEM. SLATS WOULD NOT MOVE. INTERROGATED MDC AND FOUND MULTIPLE INSTANCES OF FSACE 2 WRG FAULTS. REMOVED AND REPLACED FSACE 2 PER E175 AMM 27-53-02-000-801-A AND 27-53-02-400-801-A. PERFORMED OPS CHECK OF FLAP AND SLAT SYSTEM THREE TIMES. ALL OPS CHECKS GOOD AT THIS TIME.
2022
Part: BEAM — CORRODED (FRMS 77-78) · airframe 21,458 hrs · 11,934 cycles
AFT CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION AT FR 77/78 JUST BELOW THE FWD LATCH FITTING MOUNT AREA. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED AFT CARGO DOOR CUTOUT LOWER BEAM, REF EMB175 SRM 51-40-08. PART REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
Part: SHEAR TIE — CORRODED (FRM 84 S27-28R) · airframe 21,458 hrs · 11,934 cycles
CORROSION, AFT WET AREA BELOW FLOOR STRUCTURE ON SHEAR CLIP AT FR 84 BETWEEN STRINGERS 27R-28R. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 84 STR 27R - 28R REF EMB 175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALLANCE. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS.
Part: SHEAR TIE — CORRODED (FRM 85 S27-28R) · airframe 21,458 hrs · 11,934 cycles
CORROSION, AFT WET AREA BELOW FLOOR STRUCTURE ON SHEAR CLIP AT FR 85 BETWEEN STRINGERS 27R-28R. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 85, BETWEEN STGR 27-28R.REF SRM 51-40-08. NO WEIGHT CHANGE REPLACED WITH PMA PART.
Part: SEAT TRACK — GOUGED (FRMS 74-81) · airframe 21,458 hrs · 11,934 cycles
CF III L/H INBOARD SEAT TRACK HAS MULTIPLE GOUGES FROM FWD OF FR74 TO FR 81 AS MARKED (C-CHECK RO 10/31/2022) PERFORMED SPLICE REPAIR TO CF III LH INBOARD SEAT TRACK FR 81-85 ON LH IB SEAT TRACK REF ETD2022-170-031776 REV B. THIS REPAIR DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT. LH SEAT TRACK CF III FROM FRAME 74 TO 80 FOUND TO WTHIN LIMTS PER REF SRM 53-23-10/AD01, REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS.
Part: FLAP TRACK — DAMAGED (LT WING TE FLAP) · airframe 21,458 hrs · 11,934 cycles
LH WING FLAP TRACK 2A HAS WIDTH REDUCTION DAMAGE TO THE OUTBOARD SIDE RAIL WITH THE FLAPS EXTENDED AND RETRACTED THAT IS OUT OF LIMITS. MAX DEPTH OF DAMAGE IS .01.043". ASSET# TC2-8909 CAL DUE: 12-7-22. (C-CHECK RO 10/31/2022) / REPLACED LH WING FLAP TRACK 2A. REF ERJ 175 AMM 57-54-25. TC2-7399 DATE 5-10-23 HG4-50097 DATE 6-22-23
Part: FLAP TRACK — DAMAGED (LT WING TE FLAP) · airframe 21,458 hrs · 11,934 cycles
LH WING FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE MEASURING .033". REQUIRES 200 FC REINSPECT IF NOT REPLACED, REF EMB175 SRM 57-52-03/AD01 TABLE 101. ASSET: TC2-7153 CAL DUE: 11-18-22. (C-CHECK RO 10/31/2022) / REPLACED LH WING FLAP TRACK 1A. REF ERJ 175 AMM 57-54-25. TC2-7399 DATE 5-10-23
Part: INTERCOSTAL — CORRODED (FRMS 86-87) · airframe 21,458 hrs · 11,934 cycles
AFT WET AREA FR 86-87, STGR 27R-28R HAS 1(EACH) CORRODED INTERCOSTAL FWD OF AFT HOT DRAIN MAST. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED INTERCOSTAL BETWEEN FR 86-87, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
Part: HINGE — SCORED (RT ELEVATOR) · airframe 21,458 hrs · 11,934 cycles
RH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED RH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE ON RACK. REF CAMP #25527485 FOR INSTALL.
Part: PCU — SCORED (LT ELEVATOR) · airframe 21,458 hrs · 11,934 cycles
LH ELEVATOR INBD AND OTBD PCU HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED LH ELEVATOR INBD AND OTBD PCU HARDWARE ON RACK. REF CAMP #25574992 FOR INSTALL.
Part: HINGE — SCORED (LT ELEVATOR) · airframe 21,458 hrs · 11,934 cycles
LH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED LH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE ON RACK. REF CAMP #25574992 FOR INSTALL.
Part: PCU — SCORED (RT ELEVATOR) · airframe 21,458 hrs · 11,934 cycles
RH ELEVATOR INBD AND OTBD PCU HARDWARE IS SCORED. (C-CHECK) REPLACED RH ELEVATOR INBD AND OTBD PCU HARDWARE ON RACK. REF CAMP #25527485 FOR INSTALL.
Part: SHEAR TIE — CORRODED (FRM 87 S27-28R) · airframe 21,458 hrs · 11,934 cycles
AFT WET AREA HAS 1(EACH) CORRODED SHEAR CLIP AT FR 87, STGR 27R-28R. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 87, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
Part: SHEAR TIE — CORRODED (FRM 88 S27-28R) · airframe 21,458 hrs · 11,934 cycles
AFT WET AREA HAS 1(EACH) CORRODED SHEAR CLIP AT FR 88, STGR 27R-28R. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 88, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
Part: SEAT TRACK — GOUGED (FRMS 23-34) · airframe 21,458 hrs · 11,934 cycles
RH OB SEAT TRACK IS GOUGED AT FR 23-34. SEE CONTINUATION. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED R/H O/B SEAT TRACK FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT'S WEIGHT AND BALLANCE.
Part: SEAT TRACK — GOUGED (FRMS 23-24) · airframe 21,458 hrs · 11,934 cycles
LH OB SEAT TRACK IS GOUGED AT FR 23-34. SEE CONTINUATION. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED L/H O/B SEAT TRACK FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT'S WEIGHT AND BALLANCE.
Part: ROD — GOUGED (WINDOW) · airframe 21,458 hrs · 11,934 cycles
PILOT DV WINDOW LOWER ROD IS GOUGED. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED PIOT DV WINDOW LOWER ROD. ADJUSTMENT CHECK GOOD. REF EMB 175 AMM 56-12-00.
Part: SEAT TRACK — GOUGED (FRMS 20-21) · airframe 21,458 hrs · 11,934 cycles
RH OB SEAT TRACK IS GOUGED AT FR 20/21. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED RH OB SEAT TRACK AT FR 20/21. REF EMB SRM 51-40-08. PART REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
Part: SEAT TRACK — GOUGED (FRMS 20-21) · airframe 21,458 hrs · 11,934 cycles
LH OB SEAT TRACK IS GOUGED AT FR 20/21. (C-CHECK) REMOVED AND REPLACED L/H O/B SEAT TRACK FR20/21. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED. THIS ACTION DOES NOT EFFECT THE SIRCRAFTS WEIGHT AND BALLANCE.
Part: BRACKET — DAMAGED (FRM 84) · airframe 21,458 hrs · 11,934 cycles
R/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED R/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE REF EMB SRM 51-40-08 AND RETORED SURFACE PROTECTION REF SRM 51-23-06 PO # 715293
Part: BRACKET — DAMAGED (FRM 84) · airframe 21,458 hrs · 11,934 cycles
L/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED L/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-06 PO # 715293
Part: BRACE — DAMAGED (FRM 84) · airframe 21,458 hrs · 11,934 cycles
R/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED RH AFT WINDSCREEN GROMMET AT FRME 84 PER ETD2022-170-032175. THIS TEMPORARY REPAIR IS VALID FOR 7500FC AS OF OCTOBER 20, 2022.
Part: BRACE — ELONGATED (FRM 84) · airframe 21,458 hrs · 11,934 cycles
L/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED LH AFT WINDSCREEN UPPER OUTBD SHUTE BOLT BRACKET AT FRAME 84 REF SRM 51-40-08. APPLIED SURFACE PROTECTION AND CIC PROTECTION REF SRM 51-23-06 P.O.# 288971 AND CPM 51-25-00 P.O.#291128
2019
Part: SEAT TRACK — OUT OF LIMITS (FRAME 16) · airframe 14,889 hrs · 8,019 cycles
RIGHT HAND SEAT TRACK BEAM IN (3 EACH) AREAS AT FRAME 16 NUTPLATE CUTOUT, FORWARD EDGE OF SEAT TRACK, AND ON THE SEAT TRACK AFT EDGE OF BEAM BETWEEN FRAMES 20-23 AS MARKED (C-CHECK) RO 10/14/2019 REMOVED AND REPLACED OUT OF LIMITS RH SEAT TRACK AT FR 12-23, REF. SRM 51-40-08. THIS SDR IS BEING REPORTED AS PART OF THE CORRECTIVE ACTION PLAN FOR VDR REGARDING SDRS OVER DUE.
2016
Part: SKIN — DENTED (NR 1 SLAT) · airframe 3,947 hrs · 2,001 cycles
BIRDSTRIKE ON RT INBD OF L/E WING BETWEEN FUSELAGE AND RT ENGINE. DENT FOUND ON INBD SLAT L/E SURFACE. PERMANENTLY REPAIRED RT NR 1 SLAT NOSE SKIN BETWEEN TRACK RIB 1 & TRACK RIB 2 IAW SRM.
2015
Part: CONTROL VALVE — FAILED (BRAKES) · airframe 1,484 hrs · 669 cycles
RIGHT AND LEFT BRAKE FAULT MESSAGES DURING APPROACH, AUTO BRAKE FELL OFFLINE. AFTER LANDING EXCESSIVE BRAKING REQUIRED TO STOP ACFT. REPLACED THE BRAKE CONTROL VALVE. OPS CHECKED GOOD.