Registered owner
Skywest Airlines Inc
Owner type
Corporation
Serial number
17000576
Year built
2016
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
July 21, 2016
Certificate issued
July 20, 2016
Expires
July 31, 2029
Mode S code
A0FAC3

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 66

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2004In forceSuperseded2026
ADs by the year they took effect: 81 ADs
20041
20051
20079
20088
20093
201011
20114
20123
20135
20142
20161
20175
20181
20191
20204
20213
20227
20235
20242
20253
20262
See all 81 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N162SYMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Embraer S A ERJ 170-200 LR aircraft

FAA incident reports

No FAA accident or incident reports matched to N162SYMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Embraer S A ERJ 170-200 LR aircraft

Service difficulty reports · 12

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR SWI2024F00596Seat Track · gougedGOUGES 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 ACFTJun 24, 2024 · N162SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20240716624Seat Track · corrodedCORROSION 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.Jun 24, 2024 · N162SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20240716618Skin · dentedADM#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) Jun 18, 2024 · N162SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2021062959186Fitting · corrodedFWD 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 51-40-08Jun 16, 2021 · N162SY · Emb ERJ170200LR · Fuselage Main, Attach FittingsSDR SWIA2021062959185Doubler · corrodedCORROSION 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 51-40-08Jun 15, 2021 · N162SY · Emb ERJ170200LR · Fuselage Main, FrameSDR SWIA202159190Splice · corrodedCORROSION 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 51-75-16Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202159189Splice · corrodedCORROSION 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 51-40Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202159188Floor Support · corrodedCORROSION 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 PERJun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202159187Doubler · corrodedCORROSION 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: 51-40-08Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202159184Support · corrodedRH 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 51-23-06Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2021062959183Floor Support · corrodedCORROSION 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 51-40-08Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2021062959182Seat Track · corrodedLH 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 53-10-10Jun 14, 2021 · N162SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings

STCs that may be installed · 63

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 63 STCs