N105SY
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.
22 reports on file, 2014-07-17 – 2024-08-22.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,502 hrs · 15,344 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 9/19/2024) REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED NO CHANGE TO WEIGHT AND BALANCE
Part: BEAM — CORRODED (ZONE 200) · airframe 26,502 hrs · 15,344 cycles
FORWARD PASSENGER DOOR CUTOUT HAS CORROSION AT FORWARD CUTOUT FOR GIRTBAR FITTING AS MARKED. (C-CHECK RO 9/19/2024) REMOVED AND REPLACED FORWARD PASSENGER DOOR THRESHOLD BEAM REF SRM 51-40-08 SEE CONTINUATION CARD FOR WORK PERFORMED NO CHANGE TO WEIGHT AND BALANCE
Part: SKIN — DAMAGED (ZONE 200) · airframe 26,502 hrs · 15,344 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92805-ETD2024-170-021422 MXCODEID76852-PR - AT 2500 FT BIRD STRIKE, NOSE RADOME AND WINDSHIELD FIRST OFFICER WAS IMPACTED. PERFORMED BIRD STRIKE INSPECTION PER AMM05-50-02-200-801-A. DAMAGE FOUND ON SKIN AT FRAME 4 STR 2 RH. ETD TO FLY-ON GRANTED. PER ETD 2024-170-021422 RECONTOUR OF DAMAGE PER SRM PART II 51-10-05 REQUIRED WITHIN 100 FC WITH ESCALATION PROVIDED BY ETD2024-021422 REV A.., PART NUMBER: - , SERIAL NUMBER: 17000395, POSITION: (C-CHECK RO 9/19/2024) COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA92805-ETD2024-170-021422. REMOVED AND REPLACED FWD FUSELAGE EXTERNAL SKIN BETWEEN FR 1 - FR 5 AND STGR 6R-6L IAW REF EMB SRM 51-40-08. P/N: 170-03293-013 IS OEM, NO CHANGES TO WEIGHT NOTED. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.
Earlier reports · 2014–2023 · 19 reports
2023
Part: NONE — DAMAGED · airframe 23,013 hrs · 12,919 cycles
THE SEAT TRACK AT SEAT 23C IS DAMAGED. (FILED CLOSED)REMOVED AND REPLACED SEAT TRACK AT SEAT 23C IN REF TO AMM 25-21-11.
2022
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
LH FLOOR BEAM SEAT TRACK CORRODED AS MARKED FR 82-85. (C CHECK RO 01/28/2022) / REPAIRED LH FLOOR BEAM SEAT TRACK FR 82-85 BY SPLICING SEAT TRACK REF EMB ETD2022-170-001077.
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
FORWARD PAX DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS CORRODED (C CHECK RO 01/28/2022) REMOVED AND REPLACED FORWARD PAX DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS REF EMB175 AMM 20-10-01 ASSETT #456 DUE CAL 5-3-22
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
CORROSION ON CENTER SHEAR PANEL AT FR 87-88 (C CHECK RO 01/28/2022) REMOVED AND REPLACED CENTER SHEAR PANEL AT FR 87-88 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
R/H SHEAR PANEL FR 87-88 HAS AREAS OF CORROSION. (C CHECK RO 01/28/2022) REMOVED AND REPLACED R/H SHEAR PANEL FR 87-88 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
FORWARD PAX DOOR EVACUATION-SLIDE-MECHANISM CABLE LOWER ATTACHING HARDWARE CORRODED. (C CHECK RO 01/28/2022) REMOVED AND REPLACED FORWARD PAX DOOR EVACUATION-SLIDE-MECHANISM CABLE LOWER ATTACHING HARDWARE REF EMB175 AMM 20-10-01 ASSETT #456 DUE CAL 5-3-22
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
CORROSION ON LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALONG THE FORWARD EDGE BETWEEN FRAMES 19 AND 20. (C CHECK RO 01/28/2022) / REMOVED AND REPLACED LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALONG THE FORWARD EDGE BETWEEN FRAMES 19 AND 20 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
FORWARD SERVICE DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS CORRODED (C CHECK RO 01/28/2022) REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE MOUNT BRACKET BOLTS. REF. EMB 175 AMM 20-10-01. TW; TC1-456 CAL DUE; 5-3-22.
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
CORROSION ON RH GUSSET SPLICE AT FR 90. (C CHECK RO 01/28/2022) REMOVED AND REPLACED RH GUSSET SPLICE AT FR 90 REF EMB SRM 51-40-08
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
R/H FLOOR PANEL SUPPORT AT FR 87-90 IS CORRODED IN MULTIPLE AREAS. (C CHECK RO 01/28/2022) REMOVED AND REPLACED R/H FLOOR PANEL SUPPORT AT FR 87-90 REF EMB SRM 51-40-08
Part: NONE — DENTED · airframe 20,616 hrs · 11,365 cycles
DENT OIL CANNING ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. (C CHECK RO 01/28/2022) REPAIRED DENT ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. REF SRM 53-30-01/REPAIR12P. REPAIR INSPECTION REQUIRMENTS : DET EXTERNAL SIDE INSPETION THRESHOLD 20,000 FC OR 26,600 FH WHICHEVER OCCURS FIRST, INSPECTION INTERVAL 10,000 FC OR 13,300 FH WHICHEVER OCCURS FIRST.
Part: NONE — DAMAGED · airframe 20,616 hrs · 11,365 cycles
L2 FUSELAGE STOPS 4EA HAVE DAMAGED FACES. (C CHECK RO 01/28/2022) REMOVED AND REPLACED 1EA DAMAGED L2 FUSELAGE STOP. UPON FURTHER INSPECTION, FOUND ONLY 1EA FUSELAGE STOP TO BE DAMAGED. REF. E175 AMM 52-12-23
Part: NONE — CRACKED · airframe 20,616 hrs · 11,365 cycles
CRACKED RIVET AND EVIDENCE OF CRACKED AERODYNAMIC FLANGE AT FRAME 54, ABOVE OVER-WING PNL. (MARKED) (C CHECK RO 01/28/2022) REMOVED AND REPLACED AERODYNAMIC FLANGE AT FRAME 54 REF EMB SRM 51-40-08
Part: NONE — CRACKED · airframe 20,616 hrs · 11,365 cycles
R/H WING LOWER SURFACE HAS CRACK AT FORWARD EDGE OF MLG CUTOUT I/B OF GEAR. (C CHECK RO 01/28/2022) REPAIRED R/H LOWER SURFACE WING CRACK AT FWD EDGE OF MLG CUTOUT I/B OOF GEAR PER ETD2022-170-000846 REV.: A
2021
Part: NONE — CORRODED · airframe 20,616 hrs · 11,365 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: 96/88 MO INSP E175 - COMPLY WITH ERJ175 96/88 MO INSPECIOTN , PART NUMBER: - , SERIAL NUMBER: 17000395, POSITION: (C CHECK RO 01/28/2022) COMPLIED WITH SCHEDULED MAINTENANCE CODE: 96/88 MO INSP E175 - COMPLIED WITH ERJ175 96/88 MO INSPECTION
Part: WARNING MESSAGE — FALSE ACTIVATION (LT BRAKE) · airframe 19,022 hrs · 10,449 cycles
BRAKE LH FAULT MSG AFTER GEAR EXTENSION ON APPROACH. COMPLIED WITH QRH. MSG REMAINED UNTIL GEAR CYCLED. (FLIGHT 4735 - FILED CLOSED) TROUBLESHOT LH BRAKE FAULT MSG PER ERJ 175 FIM 32-41-00-810-823-A. PER SUBTASK 810-095-A IN THE CMC PREFORMED BCM1 PR PULSE INIT TEST. OPS CHECK GOOD AT THIS TIME NO DEFECTS NOTED. MESSAGE FOUND TO BE TRANSITORY CONDITION OF MAIN BRAKE CONTROL MODULE 1.
2017
Part: FAULT MESSAGE — FALSE ACTIVATION (LT & RT BRAKES) · airframe 10,532 hrs · 5,824 cycles
RIGHT AND LEFT BRAKE FAULTS. PERFORMED A RESET IAW FIM, MESSAGES CLEARED.
2014
Part: SKIN — DENTED (FRAMES 21-22) · airframe 888 hrs · 666 cycles
SMALL DENT AFT OF MAIN CABIN DOOR. PERFORMED A DETAILED INSPECTION OF THE DAMAGE AREA IAW SRM AND FOUND TWO DENTS THAT OUR OUT OF LIMITS IAW THE SRM. REPAIRED IAW ETD.
Part: LIGHT — FAILED (CABIN) · airframe 627 hrs · 523 cycles
EMERGENCY LIGHT OVER MAIN CABIN DOOR IS ONLY HALF LIGHTED WHEN SELECTED ON. R & R FORWARD EMERGENCY LIGHT ASSY IAW AMM. OPS CHECKED OK.