# N637AS: 2010 Embraer-Empresa Brasileira De EMB-500

- Status: Valid registration
- Airframe: [Embraer-Empresa Brasileira De EMB-500](https://openairdocs.org/model/embraer-empresa-brasileira-de-emb-500) (registry code 3260402, 6 seats)
- Engine: [Pratt & Whitney Canada PW617F-E](https://openairdocs.org/engine/pratt-whitney-canada-pw617f-e) (registry code 52293)
- Data sheets: [TCDS A59CE](https://openairdocs.org/tcds/A59CE) (Embraer S.A.), [TCDS E00080EN](https://openairdocs.org/tcds/E00080EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 50000133
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: February 26, 2010
- Certificate issued: April 12, 2023
- Expires: April 30, 2030
- Mode S code: A857CE
- Registered owner: [637as Aviation LLC](https://openairdocs.org/faa-owner/637AS%20AVIATION%20LLC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: LLC
- Owner's area on the map: 36.0602° N, 115.2623° W: Placed by OpenAirDocs at the center of ZIP code 89113, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=637AS
- Page: https://openairdocs.org/aircraft/N637AS

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): 13 in force

### Matched by airframe (Embraer-Empresa Brasileira De EMB-500)

- [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 2021-24-21](https://openairdocs.org/ad/2021-24-21): Operations · Embraer EMB-500 and EMB-505. Effective Jan 25, 2022
- [AD 2018-07-10](https://openairdocs.org/ad/2018-07-10): Flight Controls · Embraer EMB-500 and EMB-505. Effective May 15, 2018
- [AD 2016-22-02](https://openairdocs.org/ad/2016-22-02): Equipment/Furnishing · Embraer EMB-500 and EMB-505. Effective Dec 1, 2016
- [AD 2014-15-51](https://openairdocs.org/ad/2014-15-51): Stabilizers · Embraer EMB-500. Effective Aug 21, 2014
- [AD 2011-17-15](https://openairdocs.org/ad/2011-17-15): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Sep 26, 2011
- [AD 2011-01-04](https://openairdocs.org/ad/2011-01-04): Wiring Elements · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Feb 9, 2011
- [AD 2010-23-16](https://openairdocs.org/ad/2010-23-16): Pneumatic · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Dec 14, 2010
- [AD 2010-21-15](https://openairdocs.org/ad/2010-21-15): Flight controls · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Nov 18, 2010
- [AD 2010-15-09](https://openairdocs.org/ad/2010-15-09): Ice and Rain Protection · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Aug 12, 2010
- [AD 2009-24-14](https://openairdocs.org/ad/2009-24-14): Flight controls · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Jan 4, 2010
- [AD 2009-05-06](https://openairdocs.org/ad/2009-05-06): Flap system · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Feb 27, 2009

### Matched by engine (Pratt & Whitney Canada PW617F-E)

- [AD 2010-17-01](https://openairdocs.org/ad/2010-17-01): Fuel Filter Bypass Valve poppet · Pratt & Whitney Canada PW617F-E. Effective Sep 27, 2010

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

- [AD 2009-23-11](https://openairdocs.org/ad/2009-23-11) (historical): Ice and Rain Protection · Embraer - Empresa Brasileira de Aeronautica EMB-500. Effective Dec 2, 2009

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

- [SAIB AIR-21-04](https://openairdocs.org/saib/AIR-21-04): HYDRAULIC POWER SYSTEM. Issued Feb 11, 2021

## NTSB investigations

None matched to N637AS.

## FAA accident and incident reports

None matched to N637AS.

## Service difficulty reports (5)

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 XMXR202104230008](https://openairdocs.org/sdr/XMXR202104230008), Mar 12, 2021: ACTUATOR. FAILED. AFTER ENGINE START, FLAP FAIL CAS MESSAGE WITH FLAP HANDLE IN POSITION ). FLAP HANDLE IN POSITION 1 CONTINUED WITH YELLOW FLAP INDICATIONS AND CAS MESSAGE. RETU
- [SDR XMXR2020121408](https://openairdocs.org/sdr/XMXR2020121408), Sep 2, 2020: VALVE. FAILED. BLEED 2 FAILED IN FLIGHT. RESET AND FAILED A SECOND TIME.
- [SDR E07A201902110001](https://openairdocs.org/sdr/E07A201902110001), Feb 10, 2019: PRESSURE SENSOR. UNKNOWN. DURING CRUISE FLIGHT. CREW RECEIVED A RH ENGINE LOW OIL PRESSURE CAS MESSAGE. CREW CONFIRMED RH ENGINE OIL PRESSURE INDICATION WAS SHOWING ZERO PSI. CREW SHUTDO
- [SDR E07A2016050300001](https://openairdocs.org/sdr/E07A2016050300001), Apr 30, 2016: CONTROL VALVE. INOPERATIVE. UNCOMMANDED BRAKE APPLICATION FOLLOWED BY BRAKE FAIL CAS MESSAGE.
- [SDR E07A20150819637](https://openairdocs.org/sdr/E07A20150819637), Jul 8, 2015: SCREW. LOOSE. FOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 50% OF SCREWS.

## Service difficulty reports on N637AS not matched to an aircraft (96, newest 50)

They name N637AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR TRAX200800659](https://openairdocs.org/sdr/TRAX200800659), May 18, 2008: LIGHT. INOPERATIVE. PAX DOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW ATR 72 JIC 33-51-04. CHECKED GOOD. (B)
- [SDR TRAX200800558](https://openairdocs.org/sdr/TRAX200800558), Apr 17, 2008: DOOR. MALFUNCTIONED. SERVICE DOOR WILL NOT CLOSE. FLT 4344 DEL 60 MINS.
- [SDR TRAX200800554](https://openairdocs.org/sdr/TRAX200800554), Apr 16, 2008: DOOR. MALFUNCTIONED. SERVICE DOOR WILL NOT CLOSE.
- [SDR TRAX200800139](https://openairdocs.org/sdr/TRAX200800139), Jan 27, 2008: CONNECTOR. DAMAGED. UPON INSTALLATION OF FWD FLOORBOARDS, FOUND 2 EMERGENCY LIGHT TRACK CONNECTORS DAMAGED.
- [SDR TRAX200701934](https://openairdocs.org/sdr/TRAX200701934), Dec 14, 2007: COVER. MISSING. FLT 4268 - LEFT FWD LOWER EXIT SIGN IS MISSING COVER.
- [SDR TRAX200701885](https://openairdocs.org/sdr/TRAX200701885), Dec 7, 2007: LIGHT. INTERMITTENT. ASD DOOR LOWER EMERGENCY LIGHT INTERMITTENT.
- [SDR TRAX200701702](https://openairdocs.org/sdr/TRAX200701702), Nov 7, 2007: STEP. BROKEN. TOP STEP OF AIRSTAIR DOOR BROKEN.
- [SDR TRAX200701500](https://openairdocs.org/sdr/TRAX200701500), Oct 15, 2007: LIGHT. INOPERATIVE. ASD EMERGENCY LIGHT INOP.
- [SDR TRAX200701339](https://openairdocs.org/sdr/TRAX200701339), Sep 10, 2007: ANGLE. CRACKED. RIGHT WING BOX AREA, ANGLE CRACKED AT FR 25 (FABRICATION REQ'D).
- [SDR TRAX200701359](https://openairdocs.org/sdr/TRAX200701359), Sep 4, 2007: FRAME. CRACKED. AT JCT FR 25 & WING RIB 4, WING BOX FRAME FOUND CRACKED AROUND RIVET.
- [SDR TRAX200701358](https://openairdocs.org/sdr/TRAX200701358), Sep 4, 2007: ANGLE. CRACKED. LEFT WING BOX FAIRING, ANGLE AT RIB 4 FR 25 CRACKED.
- [SDR TRAX200701332](https://openairdocs.org/sdr/TRAX200701332), Sep 4, 2007: ANGLE. CRACKED. WING BOX AREA ANGLE CRACKED AT FR 25 LEFT SIDE.
- [SDR TRAX200701331](https://openairdocs.org/sdr/TRAX200701331), Sep 4, 2007: SEAT TRACK. CORRODED. CORROSION FOUND ON RIGHT SEAT TRACK BETWEEN FR 39-40 OUT OF LIMIT, NEED TO FABRICATE NEW SEAT TRACK.
- [SDR TRAX200701324](https://openairdocs.org/sdr/TRAX200701324), Sep 4, 2007: SEAT TRACK. CORRODED. LEFT SEAT TRACK BETWEEN FR 36-39 FOUND CORRODED ON W/C 100-46. NEED TO FABRICATE NEW SEAT TRACK. FABRICATED AS PER SRM 53-63-00 FIG 201 LT SEAT TRACK INSTALLATI
- [SDR TRAX200701285](https://openairdocs.org/sdr/TRAX200701285), Aug 31, 2007: FLOORBEAM. CORRODED. ON FLOORBEAM AT FR 36 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42
- [SDR TRAX200701284](https://openairdocs.org/sdr/TRAX200701284), Aug 31, 2007: FLOORBEAM. CORRODED. ON FLOORBEAM AT FR 38 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 450.
- [SDR TRAX200701283](https://openairdocs.org/sdr/TRAX200701283), Aug 31, 2007: FRAME. CORRODED. FR 38 CORRODED, FOUND OUT OF LIMIT ON W/C 100-44, NEEDS REPAIR. REPAIRED AS PER SRM 53-61-40 FIG 414.
- [SDR TRAX200701282](https://openairdocs.org/sdr/TRAX200701282), Aug 31, 2007: NUT. BROKEN. LEFT SEAT DOOR BETWEEN FR 41 AND 44 ANCHOR NUT FOUND BROKEN. REPLACED SRM 51-25-01
- [SDR TRAX200701281](https://openairdocs.org/sdr/TRAX200701281), Aug 31, 2007: STRINGER. CORRODED. ON FR 37, RIGHT SIDE AT STRINGER 14 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42.
- [SDR TRAX200701280](https://openairdocs.org/sdr/TRAX200701280), Aug 31, 2007: STRUCTURE. CORRODED. ON RIGHT Z-FLOOR, BETWEEN FR 39 AND FR 41 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42.
- [SDR TRAX200701279](https://openairdocs.org/sdr/TRAX200701279), Aug 31, 2007: NUT. BROKEN. ON RIGHT SEAT TRACK BETWEEN FR 36 AND FR 39 ANCHOR NUT FOUND BROKEN.
- [SDR TRAX200701278](https://openairdocs.org/sdr/TRAX200701278), Aug 30, 2007: STRINGER. CORRODED. ON FR 36, LEFT SIDE STRINGER 14 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42.
- [SDR TRAX200701277](https://openairdocs.org/sdr/TRAX200701277), Aug 30, 2007: SEAT TRACK. CORRODED. RIGHT SEAT TRACK BETWEEN FR 36-39 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 51-21-42.
- [SDR TRAX200701276](https://openairdocs.org/sdr/TRAX200701276), Aug 30, 2007: SEAT TRACK. CORRODED. LEFT SEAT TRACK BETWEEN FR 36-39 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42.
- [SDR TRAX200701275](https://openairdocs.org/sdr/TRAX200701275), Aug 30, 2007: SEAT TRACK. CORRODED. RIGHT SEAT TRACK BETWEEN FR 39-40 CORROSION FOUND. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42.
- [SDR TRAX200701274](https://openairdocs.org/sdr/TRAX200701274), Aug 30, 2007: FRAME. CORRODED. ON FRAME 38 BETWEEN STRINGER 21 LEFT AND STRINGER 20 LEFT CORROSION FOUND. CORROSION REMOVED IAW SRM 51-21-42.
- [SDR TRAX200701297](https://openairdocs.org/sdr/TRAX200701297), Aug 28, 2007: PLACARD. MISSING. EXTERNAL PLACARDS MISSING. 10-18-07 EXTERNAL PLACARD ERPLACED IAW MM 11-00-00.
- [SDR TRAX200701296](https://openairdocs.org/sdr/TRAX200701296), Aug 27, 2007: SPAR. CRACKED. SDI - CRACK DET-4 LOWER SPAR FASTENERS BETWEEN RIB 13 & 14. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 312. REFER TO THIS NON-ROUTINE FOR MTC ACTION
- [SDR TRAX200701293](https://openairdocs.org/sdr/TRAX200701293), Aug 27, 2007: SPAR. CRACKED. SDI - CRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 8. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 214. REFER TO THIS NON-ROUTINE FOR MTC ACTI
- [SDR TRAX200701288](https://openairdocs.org/sdr/TRAX200701288), Aug 27, 2007: SPAR. CRACKED. SDI - CRACK DET - REAR SPAR LOWER SURFACE FLANGE BETWEEN RIB 12 & RIB 13. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 284. REFER TO THIS NONROUTINE F
- [SDR TRAX200701292](https://openairdocs.org/sdr/TRAX200701292), Aug 27, 2007: SPAR. CRACKED. CRACK DETECT - FRONT SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 278. REFER TO THIS NONROUTINE FOR MTC ACTION. SUP
- [SDR TRAX200701291](https://openairdocs.org/sdr/TRAX200701291), Aug 27, 2007: SPAR. CRACKED. CRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 280. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPP
- [SDR TRAX200701290](https://openairdocs.org/sdr/TRAX200701290), Aug 27, 2007: SPAR. CRACKED. CRACK DET - FRONT SPAR LOWER SURFACE FLANGE AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 285. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLE
- [SDR TRAX200701289](https://openairdocs.org/sdr/TRAX200701289), Aug 27, 2007: SPAR. CRACKED. CRACK DET - REAR SPAR LWR SURFACE FLANGE AT WING TO FUSE JUNCTION AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 286. REFER TO THIS NONROUTINE 
- [SDR TRAX200701295](https://openairdocs.org/sdr/TRAX200701295), Aug 27, 2007: SPAR. CRACKED. SDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 10.
- [SDR TRAX200701294](https://openairdocs.org/sdr/TRAX200701294), Aug 27, 2007: SPAR. CRACKED. SDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 12.
- [SDR TRAX200701250](https://openairdocs.org/sdr/TRAX200701250), Aug 27, 2007: ANGLE. CRACKED. A/C OPERATION WITH CRACKED WINGS PRESSURE DECK ANGLES EO 72-53-0168 COMPLY WITH. PERFORMED AMO 46-90 IAW EO 72-53-0168. CRACKS IN ANGLE DO NOT EXTEND BEYOND EXI
- [SDR TRAX200700457](https://openairdocs.org/sdr/TRAX200700457), Apr 3, 2007: BULB. INOPERATIVE. ASD EMERGENCY LIGHT BULB INOP.
- [SDR TRAX200700438](https://openairdocs.org/sdr/TRAX200700438), Mar 29, 2007: LIGHT. INOPERATIVE. BOARDING DOOR EMERGENCY LIGHT INOP.
- [SDR TRAX200700331](https://openairdocs.org/sdr/TRAX200700331), Mar 7, 2007: DOOR. STIFF. EMERGENCY EXIT AT 1A IS DIFFICULT TO OPEN.
- [SDR TRAX200700146](https://openairdocs.org/sdr/TRAX200700146), Feb 1, 2007: LIGHT. INOPERATIVE. PAX DOOR STAIR EMERGENCY FLOODLIGHT INOP.
- [SDR TRAX200700023](https://openairdocs.org/sdr/TRAX200700023), Jan 3, 2007: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS CAME ON WHEN IN THE ARMED POSITION WITH GENERATOR RUNNING, WILL NOT RESET.
- [SDR TRAX200600906](https://openairdocs.org/sdr/TRAX200600906), Oct 22, 2006: LIGHT. INOPERATIVE. ASD STEP LIGHT INOP.
- [SDR TRAX200600801](https://openairdocs.org/sdr/TRAX200600801), Sep 26, 2006: BULB. INOPERATIVE. EMERGENCY LIGHT IN EXIT SIGN BY PAX DOOR HAS BULBS INOP.
- [SDR TRAX200600698](https://openairdocs.org/sdr/TRAX200600698), Sep 3, 2006: DOOR FRAME. CRACKED. SERVICE DOOR FWD DOOR FRAME BOTTOM STIFFENER CRACKED.
- [SDR TRAX200600190](https://openairdocs.org/sdr/TRAX200600190), May 4, 2006: LIGHT. INOPERATIVE. SEVERAL EMERGENCY LIGHT INOP.
- [SDR TRAX200600135](https://openairdocs.org/sdr/TRAX200600135), Apr 24, 2006: FLASHLIGHT. INOPERATIVE. FLASHLIGHT INOP.
- [SDR ASOA06335](https://openairdocs.org/sdr/ASOA06335), Mar 19, 2006: POWER SUPPLY. INOPERATIVE. DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS IN THE FRONT HALF OF THE AIRCRAFT STAYED ON WITH THE FLIGHT ATTENDANT’S SWITCH IN THE OFF POSITION AND THE COCK
- [SDR ASOA06286](https://openairdocs.org/sdr/ASOA06286), Mar 6, 2006: POWER SUPPLY. MALFUNCTIONED. DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT O
- [SDR ASOA06248](https://openairdocs.org/sdr/ASOA06248), Feb 27, 2006: LAMP. BURNED OUT. DURING A HANGAR INSPECTION, THE PASSENGER DOOR EMERGENCY STEP LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR

All 96: https://openairdocs.org/aircraft/N637AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (26)

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-Empresa Brasileira De EMB-500)

- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA02779SE](https://openairdocs.org/stc/SA02779SE): Installation of Gogo AVANCE L3 Inflight Connectivity System. AeroMech Incorporated
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA01933WI](https://openairdocs.org/stc/SA01933WI): Hardware and Software Update. Garmin International Inc
- [STC SA03009CE](https://openairdocs.org/stc/SA03009CE): Installation of a Honeywell Radar Altimeter System. Embraer Engineering & Technology Center - USA Inc
- [STC ST0321CE-A](https://openairdocs.org/stc/ST0321CE-A): Installation of L3 Communications Skywatch HP (TCAS I). Embraer Engineering & Technology Center - USA Inc
- [STC SA03007CE](https://openairdocs.org/stc/SA03007CE): Installation of Rockwell Collins Automatic Direction Finder (ADF). Embraer Engineering & Technology Center - USA Inc
- [STC SA03008CE](https://openairdocs.org/stc/SA03008CE): Installation of a Honeywell HF Communication System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA04171AT](https://openairdocs.org/stc/SA04171AT): Installation of Thrane and Thrane Aviator 200 Swiftbroadband System with Wireless Local Area Network (WLAN). Nextant Aerospace L.L.C
- [STC SA04145CH](https://openairdocs.org/stc/SA04145CH): Installation of a cosmetic threshold in the aft baggage compartment to protect interior coverings/materials from loading and removal of baggage. Elliott Aviation Technical Products Development, Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA01719WI](https://openairdocs.org/stc/SA01719WI): Installation of Aircell ATG 5000 with Aircell Axxess CTR Installation and Activation of WI-FI Provisions and Transmitting Portable Electronic Devices (T-PED) Aircraft Tolerance Testing. JetSuite, Inc
- [STC SA03230NY](https://openairdocs.org/stc/SA03230NY): Installation of RH Fwd Galley Drawer Inserts. Discovery Air Technical Services
- [STC SA03087CH](https://openairdocs.org/stc/SA03087CH): Installation of Cargo Restraint System. Eagle Creek Aviation Services
- [STC SA01633WI](https://openairdocs.org/stc/SA01633WI): Installation of Concorde RG-390E VRSLA Batteries in the Embraer 500 in accordance with Concorde Battery Corporation Master Drawing List, DWG No. 5-0359, Revision NC, dated August 25, 2010 or later FAA approved revisions. Concorde Battery Corporation

## Related

- Other Embraer-Empresa Brasileira De EMB-500 aircraft: https://openairdocs.org/model/embraer-empresa-brasileira-de-emb-500/aircraft.md
- The Pratt & Whitney Canada PW617F-E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw617f-e.md

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