N116SY
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.
40 reports on file, 2019-02-23 – 2024-09-26.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
GOUGES ON R/H SIDEWALL SEAT TRACK BETWEEN FR 74-84 IN 11 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) REMOVED AND REPLACED RH OUTBD LATERAL SEAT TRACK FR 74-84 PER REF EMB SRM 51-40-08. NEW PART INSTALLED IS OEM, NO CHANGES TO WEIGHT AND BALANCE NOTED. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 74-84 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED GOUGES FROM THE R/H FLOOR SEAT TRACK BETWEEN FRAME 74-84, IN 10 LOCATIONS, AS MARKED, BY BLENDING. MEASUREMENTS OF THE WORST OUT OF LIMIT AREA ARE: 2.826"(L) X 1.22"(W) X .021"(H). MAXIMUM MATERIAL LOSS: .013". FOUND TO BE OUT OF LIMITS REF ERJ SRM 53-23-10/AD01. TOOLING I.D.: TC2-9003, CALIBRATION DUE: 01/10/2025 AND TOOLING I.D.: TC2-7641, CALIBRATION DUE: 11/21/2024. REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 74-84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED BY THIS REPAIR. SEE CONTINUE CARDS FOR WORK PERFORMED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 26,675 hrs · 15,239 cycles
GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 74-84 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED GOUGES FROM THE R/H FLOOR SEAT TRACK BETWEEN FRAME 74-84, IN 10 LOCATIONS, AS MARKED, BY BLENDING. MEASUREMENTS OF THE WORST OUT OF LIMIT AREA ARE: 2.826"(L) X 1.22"(W) X .021"(H). MAXIMUM MATERIAL LOSS: .013". FOUND TO BE OUT OF LIMITS REF ERJ SRM 53-23-10/AD01. TOOLING I.D.: TC2-9003, CALIBRATION DUE: 01/10/2025 AND TOOLING I.D.: TC2-7641, CALIBRATION DUE: 11/21/2024. REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 74-84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED BY THIS REPAIR. SEE CONTINUE CARDS FOR WORK PERFORMED.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
CORROSION ON AFT WET AREA LH BEAM AROUND RIVETS AT FR 87 STGR27L/28L (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED AFT WET AREA LH BEAM AT FR 87 STGR27L/28L . REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
CORROSION ON AFT WET AREA RH BEAM AROUND RIVETS AT FR 87 STGR27R/28R (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED THE AFT WET AREA RH BEAM AT FR 87 STGR27R/28R. REF EMB SRM 51-40-08. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
Part: BEAM — CORRODED (ZONE 100) · airframe 26,675 hrs · 15,239 cycles
CORROSION ON AFT WET AREA RH BEAM AROUND RIVETS AT FR 87 STGR27R/28R (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED THE AFT WET AREA RH BEAM AT FR 87 STGR27R/28R. REF EMB SRM 51-40-08. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
RH IB SEAT TRACK HAS GOUGING FROM FR 23 TO FR 34 (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED RH IB SEAT TRACK FROM FR 23 TO FR 34 IAW REF EMB SRM 51-40-08. PART INSTALLED WAS OEM. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARDS FOR MAINTENANCE PERFORMED.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 26,675 hrs · 15,239 cycles
RH IB SEAT TRACK HAS GOUGING FROM FR 23 TO FR 34 (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED RH IB SEAT TRACK FROM FR 23 TO FR 34 IAW REF EMB SRM 51-40-08. PART INSTALLED WAS OEM. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARDS FOR MAINTENANCE PERFORMED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,799 hrs · 15,331 cycles
FWD WET AREA RH SEAT TRACK BETWEEN FRAME 17/18 HAS CORROSION AS MARKED (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK BETWEEN FR 12 TO FR 20 IAW REF EMBSRM 51-40-08. PART WAS REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND BALANCE NOTED. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 26,675 hrs · 15,239 cycles
FWD WET AREA RH SEAT TRACK BETWEEN FRAME 17/18 HAS CORROSION AS MARKED (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK BETWEEN FR 12 TO FR 20 IAW REF EMBSRM 51-40-08. PART WAS REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND BALANCE NOTED. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.
Part: LANDING GEAR — WARNING MESSAGE · airframe 26,113 hrs · 14,887 cycles
LG LEVER DISAG WARNING MESSAGE AFTER LANDING GEAR RETRACTION ON TAKEOFF. LANDING GEAR SHOWING ALL 3 DOWN WITH THE LEVER IN THE UP POSITION. CYCLED GEAR PER QRH PROCEDURE AND MESSAGE CLEARED AND GEAR CAME UP. (FLIGHT 4723 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
Part: CONTROL HANDLE — WARNING MESSAGE (MLG) · airframe 26,136 hrs · 14,899 cycles
LG LEVER DISAG WARNING MESSAGE AFTER LANDING GEAR RETRACTION ON TAKEOFF. LANDING GEAR SHOWING ALL 3 DOWN WITH THE LEVER IN THE UP POSITION. CYCLED GEAR PER QRH PROCEDURE AND MESSAGE CLEARED AND GEAR CAME UP. (FLIGHT 4723 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28438483 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT LG LEVER DISAG PER ERJ 175 FIM 32-61-00-810-913-A AND SEE CP 28439189 FOR TROUBLESHOOTING AND CP 28442409 FOR NLG RETRACTION ACTUATOR REPLACEMENT. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SYSTEM ON JACKS FUNCTIONAL TEST IAW ERJ 175 AMM 32-33-00-720-801-A. OPS CHECK GOOD AT THIS TIME, NO FAULTS FOUND AT THIS TIME."
Earlier reports · 2019–2022 · 28 reports
2022
Part: NONE — DAMAGED · airframe 20,924 hrs · 11,428 cycles
THE I/B SEAT TRACK AT SEATS 19B & 19C ARE DAMAGED. (FILED CLOSED) REMOVED AND REPLACED THE I/B SEAT TRACK AT SEATS 19B & 19C IN REF TO AMM 25-21-11.
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.74 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR74 STR29 REF SRM 51-40-08, NEW SHEAR CLIP WITH ORIGINAL PART NUMBER AS OLD SHEAR CLIP INSTALLED SO WEIGHT AND BALANCE IS NOT AFFECTED.
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.75 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 75 STR 29R AS REQUIRED REF SRM 51-40-08. INSTALLATION ODF SHEAR CLIP WITH SAME PART NUBER AS OLD SHEAR CLIP WILL NOT EFFECT WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.83 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR.83 STR.29R, REF SRM 51-40-08, CPM 51-25-00-910-001-AWEIGHT AND BALANCE IS NOT AFFECTED WITH INSTALLATION OF NEW SHEAR CLIP
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.83 STR.28R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR.83 STR.28R, REF SRM 51-40-08, 51-23-05, 51-23-06, CPM 51-25-00-910-001-A.SHEAR CLIP INSTALLATION DOESN'T EFFECT WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
CENTER FUSELAGE III FRAME.88 CORRODED AT STR.28R FORWARD OF THE WASTE BOX. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED CENTER FUSELAGE III BOTTOM SECTION OF FRAME 88 REF EMB SRM 51-40-08,INSTALLATION OF ORIGINAL SHEAR CLIP AND NEW FR 88 WITH SAME PART NUMBER AS OLD FR88 DOESN'T EFFECT WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
WASTE SERVICE DOUBLER HAS MULTIPLE AREAS OF CORROSION INCLUDING DETERIORATED FASTENERS BETWEEN FR.88-89 STR. 28R-27R. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED WASTE SERVICE DOUBLER AT FR 88 - FR 89 REF EMB SRM 51-40-08,WEIGHT AND BALANCE WILL NOT BE EFFECTED WITH INSTALLATION OF WASTE DOUBLER.
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.88 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STR 28R-29R REF EMB SRM 51-40-08,INSTALLATION OF SHEAR CLIP DOESN'T EFFECT WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
L/H SIDE FLOOR SEAT TRACK CORRODED BETWEEN FR76 AND FR77 AS MARKED. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED L/H SIDE FLOOR SEAT TRACK FR74 AND FR84 AS REQUIRED REF SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.87 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR.87 BETWEEN STR.28R-29R REF EMB SRM 51-40-08INSTALLATION OF NEW SHEAR CLIP DOESN'T EFFECT WEIGHT AND BALANCE.
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
R/H SIDE FLOOR SEAT TRACK CORRODED BETWEEN FR78 AND FR79 AS MARKED. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED R/H SIDE FLOOR SEAT TRACK FR74 AND FR84 AS REQUIRED REF SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
Part: NONE — CORRODED · airframe 20,460 hrs · 11,133 cycles
SHEAR CLIP AT FR.85 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 85 BETWEEN STR 28R-29R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, AND 51-23-06. APPLIED CORROSION INHIBITING COMPOUND REF CPM 51-25-00-910-001-A.
Part: NONE — CRACKED · airframe 20,460 hrs · 11,133 cycles
LH FR 52 FORWARD WEBBING ANGLE, AT LOWER SURFACE OF LH WING STUB, IS CRACKED ON THE OB END AS MARKED (C-CHECK RO 2/11/2022) REMOVED AND REPLACED LH FR 52 FORWARD WEBBING ANGLE, AT LOWER SURFACE OF LH WING STUB REF EMB SRM 51-40-08 REFER TO ATTACHED CONTINUATION CARD FOR WORK PERFORMED
Part: NONE — WORN · airframe 20,460 hrs · 11,133 cycles
L/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.0095" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED LH WING FLAP TRACK #1A. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.
Part: NONE — WORN · airframe 20,460 hrs · 11,133 cycles
R/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.010" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED RH WING #1A FLAP TRACK. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.
Part: NONE — WORN · airframe 20,460 hrs · 11,133 cycles
R/H WING OUTBOARD UPPER FLAP TRACK #3 HAS THICKNESS REDUCTION OF 0.0035" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) BLENDED RH OUTBOARD UPPER #3 FLAP TRACK WITH FLAPS EXTENDED. NOMINAL 39MM. REMOVED .16MM MATERIAL REMAINING 38.84MM TRACK WITHIN LIMITS. REF ERJ 175 SRM 57-55-03 TC2-7514 DATE 2-17-22
2019
Part: SENSOR — DIRTY (E&E BAY) · airframe 13,559 hrs · 7,203 cycles
FWD EBAY FANS FAIL MESSAGE RECEIVED IN FLIGHT. (FLT#5478) CLOSED CLEANED FAN FWD AVIONICS BAY FLOW SENSOR IAW AMM AND C/W OPERATIONAL CHECK IAW AMM AND FAULT CLEARED. OK TO CONTINUE SERVICE.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FWD CARGO CUTOUT TRIM RETAINING BRACKET HAS CORROSION NR 5 FROM THE FRONT. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FWD CARGO CUTOUT TRIM RETAINING BRACKET (NR 5 FROM THE FRONT) IAW SRM.
Part: SEAL REST — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FWD CARGO DOOR CUTOUT FWD SEAL REST HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FWD CARGO DOOR CUTOUT SEAL REST IAW SRM.
Part: BEAM — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
RT BEAM FR 89-90 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED CORROSION ON RT BEAM FR 89-90 IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
RT PANEL SUPPORT FR 87-90 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / INSTALLED NEW RT FLOOR SUPPORT (P/N:170-86181-005) AT FR 87-90 IAW SRM.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
CENTER SHEAR PANEL FR 87-88 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED CORROSION FROM CENTER SHEAR PANEL AT FR 87 -88 IAW SRM.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FLOOR GUSSET FR 90 OTBD OF RT BEAM (AT BASE OF AVIONICS CABINET) HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FLOOR GUSSET FR90 OUTBD RT BEAM IAW SRM.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FLOORBEAM GUSSET FR 90 ON RT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FLOORBEAM GUSSET FR 90 ON RT BEAM IAW SRM.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FLOORBEAM GUSSET FR 89 ON LT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED AND REPLACED FLOORBEAM GUSSET FR89 ON LT BEAM IAW SRM.
Part: BEAM — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
RT BEAM FR 86-89 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED AND REPLACED RT BEAM FR 86-89 IAW SRM.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
RT SHEAR PANEL FR 87-88 HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED RT SHEAR PANEL FR 87-88 IAW SRM.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 13,542 hrs · 7,195 cycles
FLOORBEAM GUSSET FR 89 ON RT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 INSTALLED NEW FLOORBEAM GUSSET FR 89 ON RT BEAM AND APPLIED TOPCOAT TO FASTENERS IAW SRM.