N278SY
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.
10 reports on file, 2021-09-28 – 2024-03-25.
Part: SEAT TRACK — CORRODED (FRMS 84-85) · airframe 12,495 hrs · 9,997 cycles
CORROSION, AFT WET AREA, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 4/15/2024) PERFORMED RIGHT HAND SEAT TRACK SPLICE FRAME 84-85 REF: ETD 2022-170-022163 REV A. WEIGHT ADDED TO REPAIR IS 294.5G. THIS DOES NOT EFFECT WEIGHT AND BALANCE TO ACFT. SEE CONTINUATION CARD FOR WORK PERFORMED
Part: SEAT TRACK — CORRODED (FRSM 19-20) · airframe 12,495 hrs · 9,997 cycles
FORWARD FUSELAGE FLOOR STRUCTURE R/H CENTRAL SEAT TRACK CORRODED ON INBOARD FLANGE BETWEEN FRAMES 19-20. (C-CHECK RO 4/15/2024) REMOVED AND REPLACED RH CENTRAL SEAT TRACK AT FRAMES 12-20 REF SRM 51-40-08.
Part: SEAT TRACK — CORRODED (FRMS 19-20) · airframe 12,495 hrs · 9,997 cycles
FORWARD FUSELAGE FLOOR STRUCTURE LH CENTRAL SEAT TRACK CORRODED ON OUTBOARD EDGE BETWEEN FRAMES 19-20. (C-CHECK RO 4/15/2024) FABRICATED AND INSTALLED REPAIR DOUBLER LH SEAT TRACK FR 19-20 AND RESTORED SURFACE PROTECTION REF ETD2024-170-008782 PO# 309867. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: FLOORBEAM — CORRODED (FRM 87) · airframe 12,495 hrs · 9,997 cycles
CORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 4/15/2024) REMOVED AND REPLACED THE R/H LONGITUDINAL FLOOR BEAM, FRAME 86-87 - 89-90 REF SRM 51-40-08. RESTORED SURFACE PROTECTION TO THE R/H LONGITUDINAL FLOOR BEAM, FRAME 86-87 - 89-90 REF CPM 51-25-00-910-001-A AND SRM 51-23-06. PO #313191 (G-46). THIS REPAIR DOES NOT EFFECT WEIGHT AND BALANCE
Part: SKIN — DENTED (FUSELAGE) · airframe 10,108 hrs · 7,838 cycles
TWO SIGNIFICANT DENTS FOUND ON LEFT SIDE FUSELAGE UNDER CAPTAINS DV WINDOW. GMM 3-26 THIS HAS BEEN DEEMED A MAJOR REPAIR. COMPLIED WITH PERMANENT REPAIR TO LEFT SIDE FUSELAGE BETWEEN FR 10-11 AND STRG 13L-14L IAW SRM 53-10-01/15P. ORIG SUBMISSION DATE: 1/6/2023
Part: NONE — FAILED · airframe 9,758 hrs · 7,540 cycles
PARK BRK NOT RELEASED ON APPROACH. RAN QRH AND MESSAGE EXTINGUISHED. DIVERTED TO LAX FOR PRECAUTION (FLIGHT #3745 FILED CLOSED) REPLACED DUAL EMERGEN. PARK VALVE PER AMM 32-44-01, ADJUSTED AND TESTED PER AMM 33-44-00. CYCLED PARKING BRAKE, CHECKS GOOD, NO LEAKS OR FAULTS NOTED. AREA CLEANED AND PANELS SECURED AS REQUIRED. OPS CHECKS GOOD.
Part: NONE — BENT · airframe 7,450 hrs · 5,539 cycles
RH #4 FLAP TRACK CONNECTING ROD BENT (171-03781-901) (C-CHECK RO 10/06/2021) / REMOVED AND REPLACED RH #4 FLAP TRACK CONNECTING ROD. REF AMM 57-57-40
Part: NONE — BENT · airframe 7,450 hrs · 5,539 cycles
RH #3 FLAP TRACK CONNECTING ROD BENT (#170-03781-901) (C-CHECK RO 10/06/2021) / REMOVED AND REPLACED RH #3 FLAP TRACK CONNECTING ROD. REF AMM 57-57-40
Part: NONE — BENT · airframe 7,450 hrs · 5,539 cycles
LH #4 FLAP TRACK CONNECTING ROD BENT. (171-03781-901) (C-CHECK RO 10/06/2021) / REMOVED AND REPLACED LH #4 FLAP TRACK CONNECTING ROD. REF AMM 57-57-40
Part: NONE — BENT · airframe 7,450 hrs · 5,539 cycles
LH #3 FLAP TRACK CONNECTING ROD BENT. (171-03781-901) (C-CHECK RO 10/06/2021) / REMOVED AND REPLACED LH #3 FLAP TRACK CONNECTING ROD. REF AMM 57-57-40