N162SY
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.
12 reports on file, 2021-06-14 – 2024-06-24.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 20,293 hrs · 11,994 cycles
GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 9 LOCATIONS AS MARKED. (C-CHECK RO 7/14/2024) REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34 REF SRM 51-40-08 THIS REPAIR DOES NOT EFFECT THE WEIGHT AND BALANCE OF THE ACFT
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,293 hrs · 11,994 cycles
CORROSION ON R/H SEAT TRACK BETWEEN FR 17-21 IN 3 LOCATIONS AS MARKED. (C-CHECK RO 7/14/2024) REMOVED AND REPLACED R/H SEAT TRACK BETWEEN FR 17-21. REF SRM 51-40-08 REPLACEMENT PART IS AN OEM REPLACEMENT PART AND DOES NOT EFFECT WEIGHT AND BALANCE.
Part: SKIN — DENTED (ZONE 100) · airframe 20,293 hrs · 11,994 cycles
ADM#N162SY-5352 - DENT MEASURES 2.275" LONG X 1.164" WIDE X 0.025 DEEP. NOMINAL THICKNESS IS 0.0393" AND W/D IS 46.60. LOCATED EXTERNAL LH, ZONE 100, FCBS 53-10-00-004, FORWARD FUSELAGE SKIN PANEL, FR10 TO FR11, STRG15L TO STRG17L. (C-CHECK RO 7/14/2024) REPAIRED 2 EA DENTS BETWEEN FR 10-11 STGR 15L-17L. REF ETD2024-170-017737. NO WEIGHT AND BALANCE CHANGE REQUIRED DUE TO REPAIR PARTS WEIGHING LESS THAN 2.5 LBS. SEE CONTINUATION FOR WORK PERFORMED.EXTERNAL LOW FREQUENCY EDDY CURRENT [*], NDT PART 6 TASK 51-06-00-250-806-A, THRESHOLD= 20,667 FC OR 27,487 FH, WHICHEVER OCCURS FIRST, INTERVAL: 20,667 FC OR 27,487 FH, WHICHEVER OCCURS FIRST. THE EXTERNAL SDE SHALL BE ACCOMPLISHED BY MEANS OF A LOW FREQUENCY EDDY CURRENT (LFEC) IN ORDER TO DETECT A CRACK ON THE SKIN UNDER THE DOUBLER. THIS IS AN ADDITIONAL AND SPECIFIC INSPECTION REQUIREMENT.
Part: FITTING — CORRODED (FRM 19) · airframe 13,408 hrs · 7,483 cycles
FWD WET AREA- CORROSION FOUND ON FLOOR FITTING AT FRAME 19 LH SIDE NEAR FWD PAX THRESHOLD (C-CHECK RO 6/28/2021) REMOVED AND REPLACED FLOOR FITTING AT FR19 LH SIDE NEAR PAX THRESHOLD PER REF SRM 51-40-08
Part: DOUBLER — CORRODED (FRAME 19) · airframe 13,408 hrs · 7,483 cycles
CORROSION FOUND ON DOUBLER FWD CORNERS AT FRAME 19 LH SIDE (C-CHECK RO 6/28/2021) REMOVED AND REPLACED DOUBLER AT FRAME 19 LH SIDE REF SRM 51-40-08
Part: SEAT TRACK — CORRODED (FRMS 18-19 LT) · airframe 13,408 hrs · 7,483 cycles
LH INBD SEAT TRACK HAS CORROSION BETWEEN FRAME 18 AND 19 (C-CHECK RO 6/28/2021) INSTALLED LH INBD SEAT TRACK FR18-19 REPAIR DOUBLERS REF EMB SRM 53-10-10
Part: SPLICE — CORRODED (FRAME 91) · airframe 13,408 hrs · 7,483 cycles
CORROSION AS MARKED ON RH FLOOR BEAM SPLICE FR 91. (C-CHECK RO 6/28/2021) BLENDED AND EVALUATED RH FLOOR BEAM SPLICE FR91. MEASUREMENTS .6"L X .35"W X .008"H. NOMINAL THICKNESS .04", REMAINING THICKNESS .032". ITEMS IS OUT OF LIMITS PER REF SRM 51-75-16. TOOL DATA ID:TC1-66878-2 DUE:8-12-21. REMOVED AND REPLACED RH FLOOR BEAM SPLICE AT FR 91 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-06.
Part: FLOOR SUPPORT — CORRODED (FRMS 86-87) · airframe 13,408 hrs · 7,483 cycles
CORROSION AS MARKED ON RH FLOOR BEAM UPPER AND LOWER SURFACES FR 86-87. (C-CHECK RO 6/28/2021) REMOVED AND REPLACED RH BEAM FR84-90 REF EMB SRM 51-40-08
Part: FLOOR SUPPORT — CORRODED (FRMS 90-91) · airframe 13,408 hrs · 7,483 cycles
CORROSION AS MARKED ON RH FLOOR BEAM INTERCOSTAL FR 90-91. (C-CHECK RO 6/28/2021) BLENDED AND EVALUATED RH FLOOR BEAM INTERCOSTAL FR 90-91. MEASUREMENTS .8"L X .55"W X .012"H. NOMINAL THICKNESS .04", REMAINING THICKNESS .028". ITEM IS OUT OF LIMITS PER REF SRM 51-75-16 TOOL DATA ID:TC1-66878-2 DUE:8-12-21. REMOVED AND REPLACED RH FLOOR BEAM INTERCOSTAL FR 90-91 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04 AND SRM 51-23-06.
Part: SUPPORT — CORRODED (FRMS 18-19) · airframe 13,408 hrs · 7,483 cycles
RH SILL HAS CORROSION RIGHT SIDE BETWEEN FRAME 18/19 (C-CHECK RO 6/28/2021) REMOVED AND REPLACED RH SILL BETWEEN FRAME 18-19 PER SRM 51-40-08 APLLIED TOP COAT PER SRM 51-23-06
Part: SPLICE — CORRODED (FRM 89) · airframe 13,408 hrs · 7,483 cycles
CORROSION AS MARKED ON RH FLOOR BEAM SPLICE FR 89 (C-CHECK RO 6/28/2021) REMOVED CORROSION FROM RH FLOOR BEAM SPLICE AT FR 89. 100% MATERIAL LOSS. FOUND OUT OF LIMITS REF EMB SRM 51-10-03. REMOVED AND REPLACED RH FLOOR BEAM SPLICE AT FR 89 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04 AND SRM 51-23-06.
Part: DOUBLER — CORRODED (FRM 16) · airframe 13,408 hrs · 7,483 cycles
CORROSION FOUND ON LEFT FLOOR DOUBLER 170-12118-001 AT FRAME 16 AFT RIGHT CORNER (C-CHECK RO 6/28/2021) REMOVED AND REPLACED NEW DOUBLER ON L/H FR 16 , REF. SRM: 51-40-08