N156SY
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.
24 reports on file, 2018-10-16 – 2024-01-21.
Part: FLOOR SUPPORT — CORRODED (FRM 87) · airframe 19,984 hrs · 11,874 cycles
CORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C-CHECK RO 2/9/2024) REMOVED AND REPLACED L/H LONGITUDINAL FLOOR BEAM, FRAME 86-89, WHERE THE BEAM PASSES BETWEEN THE L/H AND CENTER SHEAR PANELS REF SRM 51-40-08. RESTORED SURFACE PROTECTION, PAINT PO: 309867, TO THE L/H LONGITUDINAL FLOOR BEAM, FRAME 86-89, WHERE THE BEAM PASSES BETWEEN THE L/H AND CENTER SHEAR PANELS REF SRM 51-23-06. THIS REPAIR DOES NOT EFFECT WEIGHT AND BALANCE
Part: FLOOR SUPPORT — CORRODED (FRM 87) · airframe 19,984 hrs · 11,874 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 2/9/2024) REMOVED AND REPLACED RH LONGITUDIUNAL BEAM AT FR 87. REF EMB SRM 51-40-08. SEE CONITUATION FOR ALL WORK PERFORMED. THIS REQAIR DOES NOT EFFECT WEIGHT AND BALANCE.
Part: SEAT TRACK — GOUGED (FRMS 74-84) · airframe 19,984 hrs · 11,874 cycles
RH INBOARD SEAT TRACK SEGMENT FR74 - 84 CROWN TEETH HAVE MULTIPLE AREAS OF SURFACE PROTECTION DAMAGE AND 8 GOUGED AREAS (FR74, 74/75, 78/79, 80, 80/81, 81/82, 82/83, AND 83/84). (C-CHECK RO 2/9/2024) REMOVED AND REPLACED RH INBOARD SEAT TRACK SEGMENT FR74 - 84, REF SRM 51-40-08. REPLACED WITH NEW SEAT TRACK, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
Earlier reports · 2018–2022 · 21 reports
2022
Part: RIB — CRACKED (FRM 52) · airframe 17,254 hrs · 9,978 cycles
CRACK IN LEFT WHEEL WELL BETWEEN OPENINGS FOR FLIGHT CONTROL CABLES. (FLIGHT 4724) REMOVED AND REPLACED LEFT SIDE INBOARD RIB COMPLEMENT AT FRAME 52 IAW SRM 51-42-01.
Part: NONE — SMOKE · airframe 17,191 hrs · 9,941 cycles
D: FLIGHT ATTENDANT REPORTS A SPARK AND WISP OF SMOKE BETWEEN FORWARD GALLEY COFFEE MAKERS. / C: NEF-GAL-2 / CAT C DUE 11/15/22 (FLIGHT 4789 - FILED CLOSED) NOV 05, 2022 STATION: CLT--INSPECTED FORWARD COFFEE MAKERS FOR EVIDENCE OF ANY ELECTRICAL OR SMOKE DAMAGE. NO DAMAGE NOTED. RIGHT COFFEE MAKER HAS A SLIGHTLY NOTICABLE ELECTRICAL ODOR. DEFERRED LEFT AND RIGHT FORWARD GALLEY COFFEE MAKERS PER NEF-GAL-2. MX PROCEDURE COMPLIED WITH. PLACARDED AS REQUIRED.
2021
Part: SEAL REST — CORRODED (CARGO DOOR FRAME) · airframe 13,330 hrs · 7,515 cycles
CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER AFT SEAL REST IN 2 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES), X= 345", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED RIVETS ON THE 2 NUTPLATES FORWARD CARGO DOOR CUTOUT, ON THE LOWER AFT SEAL REST IN 2 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES), X= 345", Y= +17", Z=-63".PER SRM 51-45-00
Part: SEAL REST — CORRODED (CARGO DOOR FRAME) · airframe 13,330 hrs · 7,515 cycles
CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER CENTER SEAL REST IN 4 LOCATIONS, X= 325", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT, ON THE LOWER CENTER SEAL REST REF EMB SRM 51-40-08
Part: SEAL REST — CORRODED (CARGO DOOR FRAME) · airframe 13,330 hrs · 7,515 cycles
CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER FORWARD SEAL REST IN 3 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES AND 1 SPOT ON EDGE UNDER LATCH FITTING), X= 305", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED (2EA) NUTPLATES ON THE FORWARD CARGO DOOR CUTOUT, ON THE LOWER FORWARD SEAL REST IN 3 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES AND 1 SPOT ON EDGE UNDER LATCH FITTING), X= 305", Y= +17", Z=-63 PER SRM 51-45-00
Part: SUPPORT — CORRODED (FRM 19) · airframe 13,330 hrs · 7,515 cycles
FWD FUSELAGE LH SILL IB AFT OF FR 19 HAS CORROSION AROUND NUT HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD FUSELAGE LH SILL IB AFT OF FR 19 REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED
Part: SUPPORT — CORRODED (FRM 13) · airframe 13,330 hrs · 7,515 cycles
FWD WET AREA RH SILL HAS CORROSION AFT OF FR 13. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD WET AREA RH SILL AFT OF FRAME 13 AND APPLIED SURFACE PROTECTION PER SRM 51-23-06 SRM 51-40-08
Part: SUPPORT — CORRODED (FRM 19) · airframe 13,330 hrs · 7,515 cycles
FWD FUSELAGE LH SILL OB AFT OF FR 19 HAS CORROSION AROUND FASTENER HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD FUSELAGE LH SILL OB AFT OF FR 19 REF EMB SRM 51-40-08
Part: FLOORBEAM — CORRODED (FRM 90) · airframe 13,330 hrs · 7,515 cycles
CORROSION- AFT WET AREA, RH OUTBD FLOOR SUPPORT PANEL HAS CORROSION AT FR 90 AS MARKED. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED AFT WET AREA, RH OUTBD FLOOR SUPPORT PANEL AT FR 90 REF EMB SRM 51-40-08
Part: SEAT TRACK — CORRODED (CABIN) · airframe 13,330 hrs · 7,515 cycles
FWD WET AREA RH SEAT TRACK FWD OF FR 13 HAS CORROSION AROUND NUT HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK REF SRM 51-40-08. NO CHANGE IN WEIGHT AND BALANCE.
Part: SHEAR PANEL — CORRODED (FRMS 87-88) · airframe 13,330 hrs · 7,515 cycles
CORROSION- AFT WET AREA, RH FLOOR BEAM BETWEEN CENTER AND RH SHEAR PANEL HAS CORROSION AS MARKED. ( FR87-88) (C-CHECK RO 5/8/2021) REMOVED AND REPLACED RH FLOOR BEAM BETWEEN CENTER AND RH SHEAR PANEL ( FR87-88) REF EMB SRM 51-40-08. NO CHANGE IN WEIGHT AND BALANCE.
Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 13,330 hrs · 7,515 cycles
FR 52 SUPPORT ANGLE IS CRACKED THROUGH THE O/B FASTENER FWD OF THE LH MLG WHEEL WELL AREA AS MARKED. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED L/H FR 52 SUPPORT ANGLE FWD OF MLG WHEEL WELL REF SRM 51-40-08. DOME SEALED AND TOPCOATED FASTENERS REF SRM 51-23-09 AND 51-23-06
Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 13,330 hrs · 7,515 cycles
FR 52 LH WEB FWD OF THE LH MLG WHEEL WELL AREA HAS DAMAGE/ CRACKED IN 2 AREAS. (C-CHECK) REMOVED AND REPLACED L/H FR 52 WEB FWD OF MLG WHEEL WELL REF SRM 51-40-08. TOPCOATED FASTENERS REF SRM 51-23.-06.
2018
Part: TIP CAP — CRACKED (LT WING) · airframe 7,117 hrs · 3,992 cycles
LT WING TIP CRACKED AT WING TIP ATTACH POINT. (C-CHECK) RO: 10/24/2018. REMOVED AND REPLACED THE LT WING TIP REF AMM 57-30-00.
Part: TIP CAP — CRACKED (RT WING) · airframe 7,117 hrs · 3,992 cycles
RT WING TIP SPAR 1 CRACKED AT WING TIP ATTACH POINT. (C-CHECK) RO: 10/25/2018. REMOVED AND REPLACED THE RT WING TIP REF AMM 57-30-00.
Part: VANE — CRACKED (ENGINE) · airframe 7,117 hrs · 3,992 cycles
PANEL 421DR VANE IS CRACKED AT THE WELD.(C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM.
Part: PANEL — CRACKED · airframe 7,117 hrs · 3,992 cycles
PANEL 822DRW HAS CRACK IN COMPOSITE. (C-CHECK) RO: 10/24/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822DRW IN REFERENCE TO AMM 50-31-00.
Part: PANEL — CRACKED · airframe 7,117 hrs · 3,992 cycles
822ARW PANEL HAS CRACK IN COMPOSITE.(C-CHECK) RO: 10/25/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822ARW IN REFERENCE TO AMM 50-31-00.
Part: RETAINER — BENT (CARGO DOOR) · airframe 7,117 hrs · 3,992 cycles
FWD CARGO DOOR AFT LOWER CORNER SEAL RETAINER BENT. (C-CHECK) RO: 10/24/2018. RECONTOURED DENT ON THE FWD CARGO DOOR AFT LOWER SEAL RETAINER REF SRM 52-00-02.
Part: VANE — CRACKED (ENGINE) · airframe 7,117 hrs · 3,992 cycles
PANEL 411DR VANE IS CRACKED AT THE WELD. (C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM.
Part: PANEL — CRACKED (LT MLG WW) · airframe 7,117 hrs · 3,992 cycles
TIRE BURST PANEL CRACKED IN LT MLG WHEEL WELL. (C-CHECK) RO: 10/24/2018. COMPLIED WITH REPAIR OF LT MLG WHEEL WELL FAIRING, REF SRM 53-22-04.