# N426QS: 2018 Embraer Executive EMB-505

- Status: Valid registration
- Airframe: [Embraer Executive EMB-505](https://openairdocs.org/model/embraer-executive-emb-505) (registry code 3260390, 8 seats)
- Engine: [Pratt & Whitney Canada PW535E](https://openairdocs.org/engine/pratt-whitney-canada-pw535e) (registry code 52297)
- Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE) (Embraer S.A.), [TCDS E00053EN](https://openairdocs.org/tcds/E00053EN) (Pratt & Whitney Canada Inc.) (OpenAirDocs)
- Serial number: 50500483
- Year built: 2018
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: October 18, 2018
- Certificate issued: August 6, 2026
- Expires: August 31, 2033
- Mode S code: A51358
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=426QS
- Page: https://openairdocs.org/aircraft/N426QS

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 Executive EMB-505)

- [AD 2026-10-18](https://openairdocs.org/ad/2026-10-18): Flight Control System · Embraer EMB-505. Effective Jul 6, 2026
- [AD 2026-03-05](https://openairdocs.org/ad/2026-03-05): Autopilot Main Servo · Embraer EMB-505. Effective Mar 31, 2026
- [AD 2024-22-06](https://openairdocs.org/ad/2024-22-06): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Jan 2, 2025
- [AD 2024-17-09](https://openairdocs.org/ad/2024-17-09): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Nov 12, 2024
- [AD 2023-21-04](https://openairdocs.org/ad/2023-21-04): Indicating/recording system · Embraer EMB-505. Effective Dec 11, 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 2022-05-12](https://openairdocs.org/ad/2022-05-12): Elevator Structure, Rudder Structure, Ailerons · Embraer EMB-505. Effective Apr 13, 2022
- [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 2014-19-01](https://openairdocs.org/ad/2014-19-01): Landing Gear · Embraer EMB-505. Effective Oct 22, 2014
- [AD 2012-13-04](https://openairdocs.org/ad/2012-13-04): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Aug 6, 2012

### Matched by engine (Pratt & Whitney Canada PW535E)

- [AD 2025-05-13](https://openairdocs.org/ad/2025-05-13): Turbine Section · Pratt & Whitney Canada PW535E and PW535E1. Effective Apr 23, 2025

### Historical (superseded or no longer in force)

- [AD 2023-22-11](https://openairdocs.org/ad/2023-22-11) (historical): Autopilot Main Servo · Embraer EMB-505. Effective Dec 26, 2023
- [AD 2023-21-06](https://openairdocs.org/ad/2023-21-06) (historical): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Dec 11, 2023
- [AD 2020-12-08](https://openairdocs.org/ad/2020-12-08) (historical): Elevator Structure; Rudder Structure; Ailerons · Embraer EMB-505. Effective Jul 1, 2020
- [AD 2013-22-20](https://openairdocs.org/ad/2013-22-20) (historical): Landing Gear · Embraer EMB-505. Effective Nov 8, 2013
- [AD 2011-20-01](https://openairdocs.org/ad/2011-20-01) (historical): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Oct 31, 2011

## Information bulletins (advisory) (2 in force)

- [SAIB CE-16-23](https://openairdocs.org/saib/CE-16-23): Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) Signal. Issued Sep 7, 2016
- [SAIB CE-10-46](https://openairdocs.org/saib/CE-10-46): Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight Manual. Issued Aug 16, 2010

## NTSB investigations

None matched to N426QS.

## FAA accident and incident reports

None matched to N426QS.

## Service difficulty reports (14)

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 DXTA2025120806026](https://openairdocs.org/sdr/DXTA2025120806026), Dec 7, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN SWITCH IS IN ON POSITION. CONTACTED MCC, THEY REQUESTED BOTH FWD AND AFT EMERGENCY BATTERIES BE REPLACED. GAINED ACCES
- [SDR DXTA2025082904731](https://openairdocs.org/sdr/DXTA2025082904731), Aug 26, 2025: WARNING MESSAGE. ILLUMINATED. FLAP FAIL YELLOW CAS. CYCLED TWICE, SAME INDICATION AT 0. 3RD CYCLE FLAPS FUNCTIONED NORMAL. AFTER LANDING, FLAPS RETRACTED TO 0. POWERED ACFT. NO FAULT MESSAGE
- [SDR DXTA2025060903780](https://openairdocs.org/sdr/DXTA2025060903780), Jun 4, 2025: CONTROL UNIT. DEFECTIVE. BRK FAIL YELLOW CAS: YELLOW BRAKE FAIL CAS MESSAGE APPEARED AFTER ENTERING A RUNWAY FOR TAKEOFF. BRAKES STARTING GRABBING THEN FAILED. I SLOWLY TAXIED OFF OF TH
- [SDR DXTA2025021902399](https://openairdocs.org/sdr/DXTA2025021902399), Feb 16, 2025: HANDLE. BROKEN. THE MAIN CABIN DOOR HANDLE BROKE RIGHT OFF THE DOOR. MAIN DOOR HANDLE: THE MAIN CABIN DOOR HANDLE BROKE RIGHT OFF THE DOOR. PICTURES ARE ATTACHED. REMOVED BROKE
- [SDR DXTA2025013002159](https://openairdocs.org/sdr/DXTA2025013002159), Jan 29, 2025: CABLE. LOOSE. MAIN DOOR CABLE: TENSION ON MAIN CABIN DOOR IS LOOSE. WHEN OPENED, THE DOOR WILL TRY TO FALL COMPLETELY OPEN WITH LITTLE TO NO RESISTANCE. CORRECTIVE ACTION: MA
- [SDR DXTA2024061912093](https://openairdocs.org/sdr/DXTA2024061912093), Jun 18, 2024: DOOR. LEAKING. HIGH FREQUENCY VIBRATION & NOISE FROM RT OF FUSELAGE. EMERGENCY EXIT HANDLE RATTLES & EXIT DOOR NOISE. INSPECTED LATERAL SEAL FOUND LIFTNG ON BOTH LT & RT OF AC
- [SDR DXTA2024012610734](https://openairdocs.org/sdr/DXTA2024012610734), Jan 25, 2024: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS BEGAN FLASHING 1.5 HOURS INTO THE FLIGHT. EMER LT SWITCH WAS IN THE ARM POSITION. REMOVED AND REPLACED FWD (1) AND AFT (2) E
- [SDR DXTA2024011910663](https://openairdocs.org/sdr/DXTA2024011910663), Jan 18, 2024: BATTERY. DEFECTIVE. EMERG EXIT SIGN/LIGHT: DURING FLIGHT THE CABIN EMERGENCY LIGHTS AND SIGNS WERE FLASHING. THEY THEN WENT OFF AND REMAINED OFF. LATER THE EMERGENCY LIGHTS AND SIG
- [SDR DXTA2022070765410](https://openairdocs.org/sdr/DXTA2022070765410), Jul 7, 2022: LANDING GEAR. NOISY. NOSE GEAR: WHILE BEING VECTORED FOR THE APPROACH AT 3000 FEET A LOUD THUMP CAME FROM THE NOSE AREA. A BANG COULD ALSO BE FELT THROUGH THE FLOOR. THE NOISE AND V
- [SDR DXTA2021051041740](https://openairdocs.org/sdr/DXTA2021051041740), May 8, 2021: VHF COMM. DEFECTIVE. COM1 VHF COMM: CREW EXPERIENCED A VERY BRIEF ELECTRICAL BURNING SMELL IN THE COCKPIT. SHORTLY THEREAFTER, FOUND THAT COM 1 WAS NOT TRANSMITTING, BUT WAS ABLE TO
- [SDR DXTA030120213868](https://openairdocs.org/sdr/DXTA030120213868), Feb 26, 2021: WIRE. CHAFED. WHILE CLIMBING THROUGH 10K, TURN ON WINDSHIELD HEAT. RECEIVED AMBER WINDSHIELD FAIL 1 & 2 & SMELLED A BURNING ODOR. TURNED BOTH WINDSHIELD HEAT SWITCHES OFF & T
- [SDR 2021FA0000019](https://openairdocs.org/sdr/2021FA0000019), Jan 24, 2021: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT RIGHT ELE
- [SDR DXTA2020082004000](https://openairdocs.org/sdr/DXTA2020082004000), Aug 20, 2020: LIGHT. UNKNOWN. IN FLIGHT THE EMERGENCY LIGHTS BEGAN FLASHING. COMPLIED WITH EMBRAER CONTACT CENTER RECOMMENDATION. POWERED UP AIRCRAFT AND NO DEFECTS NOTED WITH EMERGENCY LIGH
- [SDR DXTA2018122801842](https://openairdocs.org/sdr/DXTA2018122801842), Dec 27, 2018: UNKNOWN. MALFUNCTIONED. NOSE GEAR WOULD NOT EXTEND. FOLLOWED CHECKLIST AND PERFORMED MANUAL EXTENSION. TOWER VERIFIED ON FLY BY THAT THERE WAS NO NOSE GEAR EXTENDED. "SUPPLEMENTAL INFO

## Service difficulty reports on N426QS not matched to an aircraft (21)

They name N426QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTAT2PL6D0059ZEU](https://openairdocs.org/sdr/DXTAT2PL6D0059ZEU), Jul 27, 2017: VALVE. FAILED. FUEL COCK WOULD NOT GO OFF ON RIGHT ENGINE. SEVERAL ATTEMPTS FAILED. AFTER TROUBLESHOOTING FUEL COCK HANDLE NOT SHUTTING OFF ON RIGHT ENGING. FOUND OPERATING LE
- [SDR G02R20170322004](https://openairdocs.org/sdr/G02R20170322004), Mar 22, 2017: HINGE. CORRODED. LEFT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT BORE.
- [SDR G02R20170322003](https://openairdocs.org/sdr/G02R20170322003), Mar 22, 2017: ATTACH FITTING. CORRODED. NR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BORE.
- [SDR G02R20170322002](https://openairdocs.org/sdr/G02R20170322002), Mar 22, 2017: ATTACH FITTING. CORRODED. NR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BOLT HOLE.
- [SDR G02R20170322001](https://openairdocs.org/sdr/G02R20170322001), Mar 22, 2017: STRUCTURE. CORRODED. RIGHT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT HOLE BORE.
- [SDR 2017FA0000116](https://openairdocs.org/sdr/2017FA0000116), Mar 21, 2017: HINGE. CORRODED. RIGHT HAND ELEVATOR, NUMBER 4 HINGE HAS CORROSION IN BORE.
- [SDR DXTA2016030706203](https://openairdocs.org/sdr/DXTA2016030706203), Mar 7, 2016: FLAP TRACK. CORRODED. RIGHT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEM
- [SDR DXTA2016030706202](https://openairdocs.org/sdr/DXTA2016030706202), Mar 7, 2016: FLAP TRACK. CORRODED. RIGHT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEM
- [SDR DXTA2016030706201](https://openairdocs.org/sdr/DXTA2016030706201), Mar 7, 2016: FLAP TRACK. CORRODED. RIGHT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEM
- [SDR DXTA2016030706200](https://openairdocs.org/sdr/DXTA2016030706200), Mar 7, 2016: FLAP TRACK. CORRODED. RIGHT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "A" FLAP TRACK UPPER ASSEM
- [SDR DXTA2016030706199](https://openairdocs.org/sdr/DXTA2016030706199), Mar 7, 2016: FLAP TRACK. CORRODED. LEFT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEMB
- [SDR DXTA2016030706198](https://openairdocs.org/sdr/DXTA2016030706198), Mar 7, 2016: FLAP TRACK. CORRODED. LEFT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEMB
- [SDR DXTA2016030706197](https://openairdocs.org/sdr/DXTA2016030706197), Mar 7, 2016: FLAP TRACK. CORRODED. LEFT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEMB
- [SDR DXTA2016030806196](https://openairdocs.org/sdr/DXTA2016030806196), Mar 7, 2016: SUPPORT FITTING. CORRODED. LEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF A FLAP TRACK UPPER ASSEMBLY
- [SDR DXTA2016030706196](https://openairdocs.org/sdr/DXTA2016030706196), Mar 7, 2016: SUPPORT FITTING. CORRODED. LEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE.
- [SDR DXTA2015121706139](https://openairdocs.org/sdr/DXTA2015121706139), Dec 16, 2015: APU. UNSERVICEABLE. DURING POST FLIGHT, ACFT CABIN FILLED WITH ENVIRONMENTAL SYS SMOKE. SWITCHED OFF THE APU AIR & AFTER 15 MINUTES THE SMOKE DISSIPATED. REMOVED ACCESS PANELS, REM
- [SDR DXTA2013091005497](https://openairdocs.org/sdr/DXTA2013091005497), Sep 9, 2013: BRAKE. MALFUNCTIONED. DURING LANDING, LT PEDAL BRAKE PRESSURE DROPPED AROUND 95KTS, LT BRAKE GRABS AND LT BRAKE TEMP ROSE TO 200 DEGREES C, WHILE THE RT SIDE REMAINS AROUND 80 DEGREE
- [SDR N93A08082010](https://openairdocs.org/sdr/N93A08082010), Aug 8, 2010: MICROWAVE OVEN. SMOKE. F/A WAS HEATING PLATES IN THE MICROWAVE OVEN AND SMOKE AND ELECTRICAL SMELL WAS EMITTING FROM THE OVEN. DISCONTINUED USE AND PULLED CIRCUIT BREAKER AND COLLARED
- [SDR 142604082006](https://openairdocs.org/sdr/142604082006), Apr 8, 2006: POTENTIOMETER. MALFUNCTIONED. NWS FAIL MESSAGE APPEARS RIGHT BEFORE T/O.
- [SDR 142601012006](https://openairdocs.org/sdr/142601012006), Jan 1, 2006: WINDSHIELD. CRACKED. RIGHT WINDSHIELD CRACKED.
- [SDR GAC081601](https://openairdocs.org/sdr/GAC081601), Aug 16, 2001: CHARGER. FAILED. DURING NORMAL MAINTENANCE WHILE ON THE GROUND THE BATTERY CHARGER BEGAN TO SMOKE AND THE CIRCUIT BREAKER POPPED. REMOVED AND REPLACED BATTERY CHARGER WITH REPAI

## STCs that may be installed (OpenAirDocs) (47)

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 Executive EMB-505)

- [STC SA12141IB](https://openairdocs.org/stc/SA12141IB): GOGO HDX antenna systems integration. FTI ENGINEERING NETWORK GmbH
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04761NY](https://openairdocs.org/stc/SA04761NY): True Blue TS56 Emergency Battery Power Supply Replacement. Mid-Continent Instrument Co. Inc
- [STC SA12286AT](https://openairdocs.org/stc/SA12286AT): Installation of a LEO Connectivity System. Embraer Engineering & Technology Center, USA, Inc
- [STC SA12143CH](https://openairdocs.org/stc/SA12143CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [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 SA12140IB](https://openairdocs.org/stc/SA12140IB): Mechanical provisions for the installation of a GOGO HDX antenna. FTI ENGINEERING NETWORK GmbH
- [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 SA09942AC](https://openairdocs.org/stc/SA09942AC): Installation of Schatz Bearing Corporation, Radial Bearing P/N’s : KP60BHT-H-OPG and KP64BHT-H-OPG. AV8 PMA LLC
- [STC SA00087IB](https://openairdocs.org/stc/SA00087IB): Medical reconfiguration of the EMB-505. UMLAUT ENGINEERING GMBH
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA04552AT](https://openairdocs.org/stc/SA04552AT): Installation of cargo compartment floor covering. Embraer Engineering and Technology Center, USA, Inc
- [STC SA04548AT](https://openairdocs.org/stc/SA04548AT): Installation of an Avionica, LLC Quick Access Recorder/Data Concentrator model avRDC MAX (QAR) P/N 804-1250-32 and optional Avionica, LLC Cellular Module LTE (avCM LTE) P/N 650-0100-05. Aircraft Systems and Manufacturing Inc
- [STC SA00038IB](https://openairdocs.org/stc/SA00038IB): Replacement of the Passenger Seat Cushion Covers and Foams on the Embraer S.A. EMB-505. Waypoint Aerotec Limited
- [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 SA01727WI](https://openairdocs.org/stc/SA01727WI): Interior Alteration for Installation of a Coffee Maker and Modification of No Smoking Signs. Netjets Aviation Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA04463AT](https://openairdocs.org/stc/SA04463AT): Installation of a Gogo Business Aviation Avance L5 Air To Ground (ATG) In-Flight Entertainment and Connectivity (IFEC) System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03010CE](https://openairdocs.org/stc/SA03010CE): Installation of a Lacobucci HF Electronics Nespresso Machine PIN HFE96-28T-10 and/or Monogram System -TIA Division Wavejet Microwave Oven PIN 400-1860-01. Embraer Engineering & Technology Center - USA Inc
- [STC SA04397NY](https://openairdocs.org/stc/SA04397NY): Installation of Satcom system. 328 Support Services GmbH
- [STC SA03003CE](https://openairdocs.org/stc/SA03003CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03005CE](https://openairdocs.org/stc/SA03005CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03001CE](https://openairdocs.org/stc/SA03001CE): Installation of Honeywell High Frequency (HF) Communication System, model KHF1050HF, and AvTec Selective Calling (SELCAL), model CSD-714. Embraer Engineering & Technology Center - USA Inc
- [STC SA03006CE](https://openairdocs.org/stc/SA03006CE): Installation of a Medical Evacuation Configuration (Medevac). Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA00959DE](https://openairdocs.org/stc/SA00959DE): Installation of Concorde valve regulated Lead-Acid batteries in replacement of aircraft main batteries. Concorde Battery Corporation
- [STC SA00901DE](https://openairdocs.org/stc/SA00901DE): Installation of up to Two Exxternally Mounted Gimbal Systems. Straight Flight Inc
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA03004CE](https://openairdocs.org/stc/SA03004CE): In accordance with Part 23 regulations specified in the current certification basis of Type Certificate Number A60CE, installation of pilot's new, extended seat tracks. Embraer S.A
- [STC SA03956AT](https://openairdocs.org/stc/SA03956AT): Installation of Aircell ATG-4000 High Speed Internet System (AHSI) and Aircell Axxess II Iridium Satcom or Aircell Aviator 200 SBB Satcom, Aircell ATG 5000 High Speed Internet System (AHSI) all with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA03764NY](https://openairdocs.org/stc/SA03764NY): Installation of the Low Gain Satcom Antenna. Roeder Praezision GMBH
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC SA04278AT](https://openairdocs.org/stc/SA04278AT): Installation of a cabin In-Flight Entertainment & Passenger Audio System. Embraer Engineering & Technology Center - USA Inc
- [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 SA04260AT](https://openairdocs.org/stc/SA04260AT): Installation of an 802.11 Wireless Internet System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04243AT](https://openairdocs.org/stc/SA04243AT): Installation of AFT Lavatory Coat Hanger Support. Embraer Engineering & Technology Center - USA Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA03352CH](https://openairdocs.org/stc/SA03352CH): Activation of an 802.11 a/b/g and n Wi-Fi System. Elliott Aviation Technical Products Development, Inc
- [STC SA01789WI](https://openairdocs.org/stc/SA01789WI): Quasar II Cabin Lighting with eConnect and Noise Mitigation. Duncan Aviation Inc
- [STC SA01760WI](https://openairdocs.org/stc/SA01760WI): Installation of an Aircell Universal Cabin System (UCS) 5000 with Wireless Local Area Network (WLAN). Duncan Aviation Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA01703WI](https://openairdocs.org/stc/SA01703WI): Installation of Concorde RG-380E/44 and RG-390E VRSLA Batteries. Concorde Battery Corporation
- [STC SA01692WI](https://openairdocs.org/stc/SA01692WI): Installation of Aircell High Speed Internet (AHSI) System with Wireless Local Area Network (WLAN) capability. Duncan Aviation Inc

## Related

- Other Embraer Executive EMB-505 aircraft: https://openairdocs.org/model/embraer-executive-emb-505/aircraft.md
- The Pratt & Whitney Canada PW535E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535e.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.