N128SY
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | 2017-12-18 – 2017-12-18 | Operator named in NTSB report |
| SKYWEST AIRLINES INC | Operator | 2017-12-18 – 2017-12-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
COMPLY WITH REPAIR AUTHORIZATION: RA92795-ETD2024-170-019819 MXCODEID76651-PR - SKIN DAMAGE ON FORWARD FUSELAGE SKIN FR18-FR19 AND STGR 21R- STGR22R. PER ETD ETD2024-170-019819 PERFORM PERMANENT REPAIR. DUE AT 14559 CYCLES , PART NUMBER: , SERIAL NUMBER: , POSITION: (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR ON FORWARD FUSELAGE SKIN FR18-FR19 AND STGR 21R- STGR22R IN REFERENCE TO ERJ SRM 53-10-01/REPAIR12P PER THE SRM THIS PEREMANENT REPAIR HAS RE-INSPECTION REQUIREMENTS:LOWFREQUENCYEDDY CURRENT (SDI ) FOR SINGLE DOUBLER:NDTPART6 TASK51-06-00-250-805-A INSPECTION THRESHOLD: 20667 FC OR 27487 FH WHICHEVER OCCURS FIRSTINSPECTION INTERVAL: 20667 FC OR 27487 FH WHICHEVER OCCURS FIRSTCURRENT FC: 14450 CURRENT FH: 24926.90INSPECTION DUE AT : 35117 FC OR 52413.90 FH
LEFT ELEVATOR HINGE 2 AND 3 HARDWARE WORN. REPLACED LT ELEVATOR HINGE 2 AND 3 HARDWARE ON RACK SEE CP25810196 FOR FINAL INSTALL IAW AMM 27-31-05.
L/H I/B FLAP TRACK 2A O/B HAS WIDTH REDUCTION OF .040. OUT OF LIMITS OF SRM 57-52-03/AD01. REMOVED AND RELPACED L/H I/B FLAP TRACK 2A O/B. REF E175 AMM 57-45-25.
R/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF .029" WITH A GOUGE IN RADIUS OF TRACK. (C-CHECK RO 1/3/2023) .REMOVED AND REPLACED RH I/B FLAP TRACK 1A REF EMB 175 AMM 57-54-25.ASSET# TC2-552 CAL DUE 4/7/23.
L/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF .030". LENGTH OF DAMAGE IS .6". REMOVED AND REPLACED LH I/B FLAP TRACK 1A REF EMB 175 AMM 57-54-25.
R/H I/B FLAP TRACK 2A HAS WIDTH REDUCTION OF .042". OUT OF LIMITS OF SRM 57-52-03/AD01. ASSET TC2-7153 DUE 11-17-23. REMOVED AN REPLACED R/H I/B FLAP TRACK 2A REF. E175 AMM 57-54-25.
CABIN RH SEAT TRACK BEAM CORRODED AT SEAT TRACK FLOOR BETWEEN FR 31-31. (C-CHECK RO 1/3/2023) REMOVED AND REPLACED RH I/B SEAT TRACK BEAM FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS ACTION DOES NOT EFFECT THE A/C WEIGHT AND BALLANCE.
ADM N128SY-6792 DAMAGE LOCATED APPROX ON FR10, 1.9" ABOVE STRL 17L AND 3.8" FWD OF PREVIOUS REPAIR DOUBLER, DENT MEASURES 4.4" LONG BY 2.2" WIDE BY .060" DEEP. REINSPECT EVERY 750 FC FROM 7808 UNTIL OR BEFORE PERMANENT REPAIR DUE BY FC 15308 IAWETD 2019-170-156729, REV -. PERFORMED PERMANENT REPAIR TO FORWARD FUSE LAGE SKIN BTWEEN FR. 9 - 10 AND STGRS 17L - 15L REF.ETD2019-170-156729 REV.: A REF CONTINUATION CARD FOR CORRECTIVE ATION DETAILS. WEIGHT OF REPAIR PARTS AND FASTENERS IS 25.2G. ID 61241 CAL8-17-23. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALANCE. DENT NEW MEASURMENTS L 2.100 X W 1.500 X D 0.025 SEE CONTINUATION CARD FOR ADDITIONAL WORK PERFORMED.
FLOOR BEAM AT + Y= 273.0 CORRODED AT FR 16. (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED CORRODED FLOOR BEAM AT + Y= 273.0 AT FR 12-20 REF SRM. SEE CONTINUATION CARD FOR DETATAILS.
CORROSION AFT WET AREA ON THE FR84 CROSSBEAM AS MARKED (C-CHECK) RO 1/11/2020 PERFORMED INNER DOUBLER REPAIR ON FR84 CROSSBEAM IAW SRM.
CORROSION AFT WET AREA ON THE R/H BEAM LOCATED BETWEEN FR89-90 CROSSBEAM Y= +10.748" (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED RH BEAM BETWEEN FR 89-90 CROSSBEAM. REF SRM.
CORROSION AFT WET AREA ON THE FLOOR SUPPORT R/H SIDE LOCATED ON THE FR87 CROSSBEAM (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED FLOOR SUPPORT ON THE RH SIDE LOCATED ON THE FR 97 CROSSBEAM. REF SRM.
CORROSION AFT WET AREA ON THE L/H SIDE S SPLICE PLATE LOCATED BETWEEN FR87-88 CROSSBEAMS (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED LH SPLICE PLATE LOCATED BETWEEN FR87-88 PER SRM.
R/H AFT PYLON FAIRING FRAME 1 INBD PIP PIN ATTACH POINT HAT BUSHING MIGRATED OUT. (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED R/H AFT PYLON FAIRING FRAME 1 REF EMB SRM.
CORROSION ON INTERNAL SURFACE OF LAV. SERVICE DOOR. (C-CHECK) RO 1/11/2020 REMOVED CORROSION ON INTERNAL SURFACE OF LAV. SERVICE DOOR. DOOR NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.005". NON SIG ALLOWABLE: 0.001". REMAINING MATERIAL: 0.045". LAV. SERVICE DOOR IS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED LAV. SERVICE DOOR. REF EMB SRM. AMM. DEPTH GAUGE ASSET #: 7641. CAL. DUE: 11-27-20.
SKIN HAS A DENT JUST AFT OF THE CAPT'S SIDE WINDOW. REPAIRED IAW SRM.