N113SY
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.
15 reports on file, 2014-08-15 – 2024-07-17.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
FWD WET AREA RH INBD FLOOR SEAT TRACK HAS CORROSION AT MACHINED COIN SLOT RIB FROM UPPER FLANGE TRANSITION; FR 17. (C-CHECK RO 8/19/2024) PERFORMED DOUBLER REPAIR ON RH IB SEAT TRACK AT FR 17. REF ETD2024-170-020492-A. ADDITIONAL WEIGHT DOES NOT EFFECT WEIGHT AND BALANCE OT AIRCRAFT
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
AFT WET AREA FLOOR STRUCTURE HAS CORROSION ON LH I/B BEAM AT FR 87 AS MARKED. (C-CHECK RO 8/19/2024) REMOVED AND REPLACED AFT WET AREA FLOOR STRUCTURE LH I/B BEAM AT FR 87 REF. EMB SRM 51-40-08 NO CHANGE TO WEIGHT AND BALANCE
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
FWD WET AREA LH INBD FLOOR SEAT TRACK HAS CORROSION AT MACHINED COIN SLOT -TO -FLANGE TRANSITION AREA FR 19- FR 20. (C-CHECK RO 8/19/2024) FWD WET AREA LH INBD FLOOR SEAT TRACK HAS CORROSION AT MACHINED COIN SLOT -TO -FLANGE TRANSITION AREA FR 19- FR 20. INSTALLED REPAIR DOUBLER AND FILLER ON L/H INBD SEAT TRACK FR 19-20 REF ETD2024-170-019896 REV.:/ NO CHANGE TO WEIGHT AND BALANCE
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
FWD WET AREA LH INBD FLOOR SEAT TRACK HAS CORROSION AT FASTENER HOLE OF UPPER FLANGE FR 18- FR19. (C-CHECK RO 8/19/2024) INSTALLED REPAIR DOUBLER AND FILLER ON L/H I/B SEAT TRACK FR 18-19 REF SRM 53-10-10/REPAIR 01P. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
FWD WET AREA LH INBD FLOOR SEAT TRACK HAS CORROSION AT FASTENER HOLE OF UPPER FLANGE FR 18- FR19. (C-CHECK RO 8/19/2024) INSTALLED REPAIR DOUBLER AND FILLER ON L/H I/B SEAT TRACK FR 18-19 REF SRM 53-10-10/REPAIR 01P. REPAIR PARTS WEIGHED LESS THAN 2.5 LBS, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
CORROSION ON L/H FLOOR SEAT TRACK BETWEEN FR 74-85 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 8/19/2024) REMOVED AND REPLACE L/H I/B FLOOR SEAT TRACK BETWEEN FR 74-85 REF EMB SRM 51-40-08 SEAT TRACK REPLACEMENT WITH OEM PART DOES NOT ADD ANY ADDITIONAL WEIGHT AND DOES NOT EFFECT WEIGHT AND BALANCE OF THE ACFT
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,550 hrs · 15,238 cycles
AFT WET AREA FLOOR STRUCTURE HAS CORROSION ON RH I/B BEAM AT FR 87 AS MARKED. (C-CHECK RO 8/19/2024) REMOVED AND REPLACED AFT WET AREA FLOOR STRUCTURE RH I/B BEAM AT FR 87 REF. EMB SRM 51-40-08
Earlier reports · 2014–2021 · 8 reports
2021
Part: NONE — NONE · airframe 20,444 hrs · 11,148 cycles
R/H OUTBOARD SEAT TRACK GOUGED BETWEEN FR.20-21 AS MARKED. (C-CHECK RO 12/19/2021) REMOVED AND REPLACED R/H O/B SEAT TRACK AT FR 17 -21 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT OF AIRCRAFT NOTED
Part: NONE — FAILED · airframe 20,444 hrs · 11,148 cycles
R/H ELEVATOR OTBD PCU FAILED BACKLASH FUNCTIONAL CHECK (C-CHECK RO 12/19/2021) REMOVED AND REPLACED RH OUTBOARD ELEVATOR PCU TOGGLE LINK TO ELEVATOR BOLT AND BUSHING REF EMB175 AMM 27-32-01. RH ELEVATOR OUTBOARD PCU BACKLASH FUNCTIONAL CHECKPASSED AT THIS TIME. REF ATTACHED TASK CARD 27-32-01-006-RH.
2020
Part: I/O MODULE — FAILED · airframe 17,359 hrs · 9,344 cycles
ON LANDING LG WOW SYS FAIL CAUTION MESSAGE. AUTO BRAKES DID NOT WORK. THRUST REVERSE DID NOT WORK. GROUND LIFT DUMP DID NOT DEPLOY. MAX MANUAL BRAKING RESULTED IN USING ENTIRE RUNWAY TO STOP AIRCRAFT. MESSAGE CLEARED ON TAXI. FLIGHT 5276 - FILLED CLOSED INTERROGATED CMC, FOUND GENERIC I/O MODULE FAULTED (FAULT CODE 32600010UT, REMOVED AND REPLACED DENERIC I/O MODULE 1 IN REFERENCE TO AMM. PERFORMED THRUST REVERSER FUNCTIONAL CHECK IN REFERENCE TO AMM, MAIN-BRAKE AUTO BRAKE SYSTEM FUNCTIONAL CHECK IN REFERENCE TO AMM, AND SPOILER SYSTEM OPERATIONAL TEST IN REFERENCE TO AMM. ALL OPS CHECKS GOOD AT THIS TIME.
2018
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,116 hrs · 6,490 cycles
EMER/PRKG BRAKE INDICATION ILLUMINATED IN CRUISE INTERMITTENTLY THEN STAYED ON. PRKG BRK NOT RELEASED THEN CAME ON. FOLLOWED QRH. DECLARED AN EMERGENCY. LANDING WAS NORMAL WITH NO ADVERSE BRAKING. (FLT 5506)
Part: VALVE — FAILED (PARKING BRAKE) · airframe 12,206 hrs · 6,543 cycles
EMERGENCY PARKING BRAKE INDICATION ILLUMINATED DURING CRUISE INTERMITTENTLY THEN STAYED ON. PARKING BRAKE NOT RELEASED THEN CAME ON. FOLLOWED QRH. DECLARED AN EMERGENCY. LANDING WAS NORMAL WITH NO ADVERSE BRAKING. REMOVED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IAW AMM.
2015
Part: SENSOR — FAILED (MLG WOW) · airframe 3,692 hrs · 1,853 cycles
PSEM-1 FAULT LANDING GEAR, NO DISPATCH AND LANDING GEAR WOW SYSTEM FAULT. PERFORMED RESET PROCEDURE IAW FIM. FAULT MESSAGES CLEARED.
2014
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 462 hrs · 259 cycles
ACRID, UNUSUAL ODOR COMING FROM OVERHEAD VENTS IN GALLEY, STRONGER IN AFT GALLEY. FOUND AFT EMERGENCY LIGHT POWER UNIT AT LT POSITION ZONE 254 TO BE CAUSE OF ELECTRICAL ODOR. R & R ELPU IAW AMM.
Part: RUDDER — OUT OF RIG · airframe 307 hrs · 176 cycles
RUDDER APPARENTLY MISALIGNED; CROSS-CONTROLLED DURING TAKE OFF, MORE THAN 50 PERCENT RUDDER TRIM REQUIRED TO MAINTAIN COORDINATED FLIGHT. FOUND RUDDER TO BE OUT OF RIG. PERFORMED FULL RIG OF RUDDER IAW AMM.