# N108SY: 2014 Embraer S A ERJ 170-200 LL

- Status: Valid registration
- Airframe: [Embraer S A ERJ 170-200 LL](https://openairdocs.org/model/embraer-s-a-erj-170-200-ll) (registry code 326041A, 88 seats)
- Engine: [GE CF34-8E5](https://openairdocs.org/engine/ge-cf34-8e5) (registry code 30061)
- Data sheets: [TCDS A56NM](https://openairdocs.org/tcds/A56NM) (Embraer S.A.), [TCDS E00063EN](https://openairdocs.org/tcds/E00063EN) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 17000401
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 23, 2024
- Certificate issued: May 23, 2014
- Expires: May 31, 2027
- Mode S code: A02413
- Registered owner: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%20George)
- Owner type: Corporation
- Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=108SY
- Page: https://openairdocs.org/aircraft/N108SY

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 30 in force

### Matched by airframe (Embraer S A ERJ 170-200 LL)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-14-05](https://openairdocs.org/ad/2025-14-05): Nacelles/Pylons · Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE and 12 more. Effective Aug 25, 2025
- [AD 2025-01-05](https://openairdocs.org/ad/2025-01-05): Time Limits/Maintenance Checks · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Mar 17, 2025
- [AD 2024-14-08](https://openairdocs.org/ad/2024-14-08): Pneumatic System · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Sep 25, 2024
- [AD 2024-12-08](https://openairdocs.org/ad/2024-12-08): Landing gear · Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE and 5 more. Effective Jul 11, 2024
- [AD 2023-13-02](https://openairdocs.org/ad/2023-13-02): Flight controls · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Sep 5, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-03-19](https://openairdocs.org/ad/2023-03-19): Instruments · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Apr 7, 2023
- [AD 2022-16-01](https://openairdocs.org/ad/2022-16-01): Windows · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Aug 15, 2022
- [AD 2022-11-51](https://openairdocs.org/ad/2022-11-51): Wing structure · Embraer ERJ 170-200 STD, ERJ 170-200 LR, ERJ 170-200 SU and 1 more. Effective Jun 21, 2022
- [AD 2020-25-08](https://openairdocs.org/ad/2020-25-08): Flight controls · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Jan 21, 2021
- [AD 2020-07-21](https://openairdocs.org/ad/2020-07-21): Landing gear · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective May 26, 2020
- [AD 2020-05-22](https://openairdocs.org/ad/2020-05-22): Indicating/recording systems · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Apr 24, 2020
- [AD 2019-19-03](https://openairdocs.org/ad/2019-19-03): Fuselage · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Oct 31, 2019

### Matched by engine (GE CF34-8E5)

- [AD 2026-21-11](https://openairdocs.org/ad/2026-21-11): Turbine Engine Compressor Section · General Electric Company GE Aerospace CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 27, 2026
- [AD 2025-12-08](https://openairdocs.org/ad/2025-12-08): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jul 23, 2025
- [AD 2023-02-05](https://openairdocs.org/ad/2023-02-05): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 9 more. Effective Mar 14, 2023
- [AD 2022-21-06](https://openairdocs.org/ad/2022-21-06): Turbine Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 15, 2022
- [AD 2022-09-14](https://openairdocs.org/ad/2022-09-14): Compressor Bleed Valve · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jun 24, 2022
- [AD 2022-08-06](https://openairdocs.org/ad/2022-08-06): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Apr 29, 2022
- [AD 2021-26-19](https://openairdocs.org/ad/2021-26-19): Turbine Section · General Electric CF34-8C5, CF34-8C5B1, CF34-8E2 and 6 more. Effective Jan 25, 2022
- [AD 2021-23-51](https://openairdocs.org/ad/2021-23-51): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Dec 29, 2021
- [AD 2021-18-13](https://openairdocs.org/ad/2021-18-13): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 22, 2021
- [AD 2018-17-14](https://openairdocs.org/ad/2018-17-14): Thrust Reverser · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 7, 2018
- [AD 2017-20-09](https://openairdocs.org/ad/2017-20-09): Turbine Engine Bypass Section · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 13, 2017
- [AD 2017-17-18](https://openairdocs.org/ad/2017-17-18): Turbine Engine Compressor Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 6, 2017
- [AD 2013-06-06](https://openairdocs.org/ad/2013-06-06): Operability bleed valves (OBV) · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective May 8, 2013
- [AD 2009-24-06](https://openairdocs.org/ad/2009-24-06): Full authority digital electronic controls · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Dec 28, 2009
- [AD 2008-05-01](https://openairdocs.org/ad/2008-05-01): Fuel metering units (FMU) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 8 more. Effective Apr 3, 2008
- [AD 2005-07-09](https://openairdocs.org/ad/2005-07-09): Master variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Apr 20, 2005

### Historical (superseded or no longer in force)

- [AD 2022-25-07](https://openairdocs.org/ad/2022-25-07) (historical): Time Limits/Maintenance Checks, Flight controls, Fuel, Doors, Fuselage, Nacelles/pylons, Stabilizers, Wings, Powerplant, Exhaust · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Jan 23, 2023
- [AD 2020-12-12](https://openairdocs.org/ad/2020-12-12) (historical): Nacelles/pylons · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Aug 13, 2020
- [AD 2019-25-16](https://openairdocs.org/ad/2019-25-16) (historical): Flight controls · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Feb 10, 2020
- [AD 2008-16-01](https://openairdocs.org/ad/2008-16-01) (historical): Full authority digital engine controls (FADECs) · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Aug 15, 2008
- [AD 2004-04-04](https://openairdocs.org/ad/2004-04-04) (historical): Master Variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Mar 9, 2004

## Information bulletins (advisory) (1 in force)

- [SAIB NM-20-12](https://openairdocs.org/saib/NM-20-12): Powerplant System - Operating in Icing Conditions. Issued Jun 18, 2020

## NTSB investigations

None matched to N108SY.

## FAA accident and incident reports

None matched to N108SY.

## Service difficulty reports (46)

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

- [SDR SWIA20241017926](https://openairdocs.org/sdr/SWIA20241017926), Sep 26, 2024: SHEAR PANEL. DAMAGED. ELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLIN
- [SDR SWI2024F01126](https://openairdocs.org/sdr/SWI2024F01126), Sep 25, 2024: FLOORBEAM. CORRODED. AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED CLOSED)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FAS
- [SDR SWIA20241017925](https://openairdocs.org/sdr/SWIA20241017925), Sep 25, 2024: BEAM. CORRODED. AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED OPEN)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTE
- [SDR SWI2024F01130](https://openairdocs.org/sdr/SWI2024F01130), Sep 24, 2024: BEAM. CORRODED. CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WO
- [SDR SWI2024F01129](https://openairdocs.org/sdr/SWI2024F01129), Sep 24, 2024: BEAM. CORRODED. CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 A
- [SDR SWI2024F01128](https://openairdocs.org/sdr/SWI2024F01128), Sep 24, 2024: BEAM. CORRODED. CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NE
- [SDR SWIA20241017024](https://openairdocs.org/sdr/SWIA20241017024), Sep 24, 2024: BEAM. CORRODED. CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK
- [SDR SWIA20241017023](https://openairdocs.org/sdr/SWIA20241017023), Sep 24, 2024: BEAM. CORRODED. CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND
- [SDR SWIA20241017924](https://openairdocs.org/sdr/SWIA20241017924), Sep 24, 2024: BEAM. CORRODED. CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW 
- [SDR SWI2024F01137](https://openairdocs.org/sdr/SWI2024F01137), Sep 23, 2024: SEAT TRACK. GOUGED. RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM P
- [SDR SWI2024F01136](https://openairdocs.org/sdr/SWI2024F01136), Sep 23, 2024: SEAT TRACK. GOUGED. LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-
- [SDR SWIA20240923](https://openairdocs.org/sdr/SWIA20240923), Sep 23, 2024: SEAT TRACK. GOUGED. GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWE
- [SDR SWIA20241017022](https://openairdocs.org/sdr/SWIA20241017022), Sep 23, 2024: SEAT TRACK. GOUGED. RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM PAR
- [SDR SWIA202410170021](https://openairdocs.org/sdr/SWIA202410170021), Sep 23, 2024: SEAT TRACK. GOUGED. LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40
- [SDR SWIA2024101700923](https://openairdocs.org/sdr/SWIA2024101700923), Sep 23, 2024: SEAT TRACK. GOUGED. GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN
- [SDR SWI2024F01141](https://openairdocs.org/sdr/SWI2024F01141), Sep 22, 2024: BEAM. CORRODED. AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)INSTALLED NEW AFT PAX DOOR 
- [SDR SWIA20240922](https://openairdocs.org/sdr/SWIA20240922), Sep 22, 2024: BEAM. CORRODED. AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED TH
- [SDR SWIA202410170025](https://openairdocs.org/sdr/SWIA202410170025), Sep 22, 2024: BEAM. CORRODED. AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)INSTALLED NEW AFT PAX DOOR LO
- [SDR SWIA202410170922](https://openairdocs.org/sdr/SWIA202410170922), Sep 22, 2024: BEAM. CORRODED. AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE 
- [SDR SWIA2024110409201](https://openairdocs.org/sdr/SWIA2024110409201), Sep 20, 2024: DOUBLER. CORRODED. WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED CLOSED).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DO
- [SDR SWIA20241017920](https://openairdocs.org/sdr/SWIA20241017920), Sep 20, 2024: SKIN. CORRODED. WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED OPEN).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DOOR
- [SDR SWIA202264783](https://openairdocs.org/sdr/SWIA202264783), Mar 2, 2022: NONE. NONE. WARRANTY - RIBS 10A , 11A, AND 12A MISLOCATED DURING DRILL UP OF NEW RIBS (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH HORIZONTAL STABILIZER RIBS 10A , 11A, 
- [SDR SWIA202264792](https://openairdocs.org/sdr/SWIA202264792), Feb 27, 2022: NONE. CRACKED. FLOOR SUPPORT AT R/H FR. 86 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 86 I/B OF AFT SERVICE DOOR AN
- [SDR SWIA202264791](https://openairdocs.org/sdr/SWIA202264791), Feb 27, 2022: NONE. CRACKED. FLOOR SUPPORT AT R/H FR. 85 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 85 I/B OF AFT SERVICE DOOR AN
- [SDR SWIA202264782](https://openairdocs.org/sdr/SWIA202264782), Feb 26, 2022: NONE. NONE. LH HORIZONTAL STABILIZER UPPER SKIN MIS-DRILLED HOLE AT RIB 14 FWD END (C CHECK RO 03/07/2022) REPAIRED L/H HORIZONTAL STABILIZER UPPER SKIN AT RIB 14 FWD END. 
- [SDR SWIA202264790](https://openairdocs.org/sdr/SWIA202264790), Feb 23, 2022: NONE. CORRODED. AFT CARGO DOOR AFT DOOR SILL REST ( EXTERNAL SIDE) HAS CORROSION AROUND MULTIPLE NUTPLATES AS MARKED (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT CARGO DOOR
- [SDR SWIA202264800](https://openairdocs.org/sdr/SWIA202264800), Feb 17, 2022: NONE. DAMAGED. LH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLAC
- [SDR SWIA202264799](https://openairdocs.org/sdr/SWIA202264799), Feb 17, 2022: NONE. DISPLACED. LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING IS MIGRATED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING AS R
- [SDR SWIA202264798](https://openairdocs.org/sdr/SWIA202264798), Feb 17, 2022: NONE. DAMAGED. RH ELEVATOR HINGE #2 HARDWARE STACK UP (BOLT/NUT/BUSHING/WASHERS) WAS FOUND SEIZED AND WERE DAMAGED DURING REMOVAL. (C CHECK RO 03/07/2022) REMOVED AND REPLACED
- [SDR SWIA202264797](https://openairdocs.org/sdr/SWIA202264797), Feb 17, 2022: NONE. DAMAGED. RH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLAC
- [SDR SWIA202264796](https://openairdocs.org/sdr/SWIA202264796), Feb 17, 2022: NONE. DAMAGED. RH ELEVATOR HINGE #3 BOLT OUTBOARD HAT BUSHINGS (FLOATING AND PRESSED IN) HAVE DENTS/SCORING DAMAGE. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HI
- [SDR SWIA202264795](https://openairdocs.org/sdr/SWIA202264795), Feb 17, 2022: NONE. DAMAGED. RH ELEVATOR HINGE #4 BOLT AND NUT HAVE THREAD DAMAGE/NUT WILL NOT THREAD ONTO BOLT. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #4 BOLT AND N
- [SDR SWIA202264794](https://openairdocs.org/sdr/SWIA202264794), Feb 17, 2022: NONE. BINDS. RH HORIZONTAL STABILIZER #2 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #2 HINGE BEARING, REF. EM
- [SDR SWIA202264793](https://openairdocs.org/sdr/SWIA202264793), Feb 17, 2022: NONE. BINDS. RH HORIZONTAL STABILIZER #3 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #3 HINGE BEARING. REF. EM
- [SDR SWIA202264789](https://openairdocs.org/sdr/SWIA202264789), Feb 16, 2022: NONE. CRACKED. CENTER COCKPIT FLOOR CONSOLE SUPPORT ANGLE IS CRACKED ON THE FORWARD SIDE OF FLOOR BEAM AT FRAME 12. (C CHECK RO 03/07/2022) / REMOVED AND REPLACED CENTER COCKP
- [SDR SWIA202264781](https://openairdocs.org/sdr/SWIA202264781), Feb 16, 2022: NONE. CORRODED. UNDER AFT WET AREA, FWD OF WASTE BOX, SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STRINGERS 23R AND 24R (C CHECK RO 03/07/2022) REMOVED AND REPLACED SHEAR CLIP AT F
- [SDR SWIA202264788](https://openairdocs.org/sdr/SWIA202264788), Feb 15, 2022: NONE. CORRODED. AFT WET AREA, RH SIDE, PANEL, SHEAR CORRODED IN 2 PLACES, 2ND AND 4TH BOLT HOLES FROM RH END (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE,
- [SDR SWIA202264787](https://openairdocs.org/sdr/SWIA202264787), Feb 15, 2022: NONE. CORRODED. AFT WET AREA, RH SIDE, PANEL SUPPORT CORRODED IN 2 PLACES, AFT AND CENTER BOLT HOLES (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA RH SIDE PANEL SUP
- [SDR SWIA202264786](https://openairdocs.org/sdr/SWIA202264786), Feb 15, 2022: NONE. CORRODED. AFT WET AREA, RH SIDE, GUSSET PLATE CORRODED AT INBOARD BOLT HOLE (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE, GUSSET PLATE AT FR90 REF E
- [SDR SWIA202264785](https://openairdocs.org/sdr/SWIA202264785), Feb 14, 2022: NONE. CORRODED. L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS CORRODED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED L/H AND 
- [SDR SWIA202264784](https://openairdocs.org/sdr/SWIA202264784), Feb 14, 2022: NONE. DAMAGED. L/H WING #2A O/B FLAP TRACK HAS WIDTH REDUCTION DAMAGE OF .031". (C CHECK RO 03/07/2022) LH WING #2A OB FLAP TRACK OUT OF LIMITS. NOMINAL 1.003" REMOVED.44" REM
- [SDR SWIA202264780](https://openairdocs.org/sdr/SWIA202264780), Feb 13, 2022: NONE. WORN. LH SLAT #3 O/B TRACK THICKNESS REDUCTION .41MM OUT OF LIMITS. ASSET TC2-7153 DUE 11/18/22 (C CHECK RO 03/07/2022) / COMPLIED WITH PERMANENT REPAIR PER ETD2022-1
- [SDR SWIA202264779](https://openairdocs.org/sdr/SWIA202264779), Jan 5, 2022: NONE. DAMAGED. COMPLY WITH SCHEDULED MAINTENANCE CODE: RA47357-ETD2019-170-043590-N108SY-PR - DENT AND SCRATCH DAMAGE TO THE FWD FUSE SKIN BTWN FR10-FR11 AND STR14L-15L. PERFO
- [SDR SWIA202158611](https://openairdocs.org/sdr/SWIA202158611), Jun 3, 2021: UNKNOWN. ODOR. FUME EVENT DURING CRUISE STRONG SULFUR ACIDIC SMELL. EYES AND THROAT IRRITATION. DID NOT GET TO ISOLATE ANY PACKS OR ENG BLEEDS AND NO APU ON TAXI IN. (FLIGHT 5
- [SDR SWIA2019071246056](https://openairdocs.org/sdr/SWIA2019071246056), Jul 11, 2019: LINE. FAILED. RECEIVED HYDRAULIC 2 LOW PRESSURE AND HYD 2 QTY CAUTION MESSAGES IN FLIGHT. PERFORMED QRH. MESSAGES REMAINED. DIVERTED. LANDING GEAR MANUALLY EXTENDED. LANDING 
- [SDR SWIA201540630](https://openairdocs.org/sdr/SWIA201540630), Jan 20, 2015: ANTENNA. DAMAGED. FOUND TCAS ANTENNA DAMAGED. R & R THE BOTTOM OMNI DIRECTIONAL TCAS ANTENNA IAW AMM. OPS CHECKED GOOD.

## STCs that may be installed (OpenAirDocs) (20)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer S A ERJ 170-200 LL)

- [STC ST04801NY](https://openairdocs.org/stc/ST04801NY): Installation (including Demod option) of Connectivity Antenna. Delta Engineering Corporation
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04748NY](https://openairdocs.org/stc/ST04748NY): Installation of the SpaceX Starlink Aviation System. Space Exploration Technologies Corp. / Starlink Aviation
- [STC ST02722LA](https://openairdocs.org/stc/ST02722LA): Updates the aircraft recording system by replacing the forward Cockpit Voice and Data Recorder (CVDR) with a new SRVIVR25 CVDR with Recorder Independent Power Supply (RIPS). Acron Aviation Inc
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST11372DS](https://openairdocs.org/stc/ST11372DS): De-modification of Air-To-Ground (A TG) antennas and associated cabin equipment i. Altitude Aerospace USA
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12138CH](https://openairdocs.org/stc/ST12138CH): Installation of Universal Avionics KAPTURE Combined Cockpit Voice and Flight Data Recorders i. GoAeroMx, LLC
- [STC ST02402LA](https://openairdocs.org/stc/ST02402LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST02534SE](https://openairdocs.org/stc/ST02534SE): Installation and maintenance of a Crane Aerospace & Electronics Tire Pressure Sensor Assembly. ELDEC Corporation
- [STC ST09900AC](https://openairdocs.org/stc/ST09900AC): installation of an Electronic Flight Bag (EFB) power system. L2 Aviation
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04820NY](https://openairdocs.org/stc/ST04820NY): Installation (including Demod option) of Cabin Connectivity. Delta Engineering Corporation
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04535AT](https://openairdocs.org/stc/ST04535AT): Installation of the CES-170 Emergency Light Power Unit (ELPU). Chippewa Aerospace Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00957DE](https://openairdocs.org/stc/ST00957DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery. MarathonNorco Aerospace Inc
- [STC ST04435AT](https://openairdocs.org/stc/ST04435AT): Installation of Astronics Passenger In-Seat Power in the Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 Series Aircraft. Chippewa Aerospace Inc
- [STC ST03406NY](https://openairdocs.org/stc/ST03406NY): Installation of a gogo Cabin Connectivity System. Delta Engineering Corporation

## Related

- Other Embraer S A ERJ 170-200 LL aircraft: https://openairdocs.org/model/embraer-s-a-erj-170-200-ll/aircraft.md
- The GE CF34-8E5 engine: https://openairdocs.org/engine/ge-cf34-8e5.md

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