# N303QS: 2013 Embraer S A EMB-505 - Status: Valid registration - Airframe: [Embraer S A EMB-505](https://openairdocs.org/model/embraer-s-a-emb-505) (registry code 326040C, 9 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: 50500141 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: May 29, 2013 - Certificate issued: January 13, 2026 - Expires: January 31, 2033 - Mode S code: A32BE6 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=303QS - Page: https://openairdocs.org/aircraft/N303QS 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 S A 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 N303QS. ## FAA accident and incident reports None matched to N303QS. ## Service difficulty reports (20) 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 DXTA2026071508807](https://openairdocs.org/sdr/DXTA2026071508807), Jul 13, 2026: AXLE. WORN. DURING TAKEOFF AND LANDING ROLL AT HIGHER SPEEDS THERE IS A LOUD GRINDING/SQUEAKING NOISE COMING FROM THE NOSEWHEEL ACCOMPANIED BY A STRONG NOSEWHEEL SHIMMY. RE - [SDR DXTA2026012806680](https://openairdocs.org/sdr/DXTA2026012806680), Jan 26, 2026: GPS. MALFUNCTIONED. ON DEPARTURE FROM DTW DURING THE INITIAL CLIMB WE EXPERIENCED GPS LOI AND GPS LOSS OF POSITION. SHORTLY THEREAFTER WE ENTERED IMC AND RECEIVED AHRS 1 AND 2 FAUL - [SDR DXTA2026012106597](https://openairdocs.org/sdr/DXTA2026012106597), Jan 19, 2026: DOOR. FROZEN. MAIN DOOR HAVING ISSUES TO OPEN & CLOSE. WILL NOT LATCH COMPLETLY. GREEN FLAG NOT SHOWING. CAS MESS DOOR OPEN. OPENED DOOR, NO DEFECTS. POWERED ACFT & CLOSED DO - [SDR DXTA2025122306203](https://openairdocs.org/sdr/DXTA2025122306203), Dec 19, 2025: BATTERY. INOPERATIVE. CABIN EMERGENCY LIGHTS ARE ILLUMINATED WITH THE AIRCRAFT BATTERIES ON AND THE EMER LIGHT SWITCH IN THE ARMED POSITION. EMER LT NOT ARM CAS MESSAGE STAYS ILLUMIN - [SDR DXTA2025102005339](https://openairdocs.org/sdr/DXTA2025102005339), Oct 16, 2025: SELECTOR VALVE. INOPERATIVE. AFTER TAKEOFF ,LANDING GEAR WOULD NOT RETRACK. PERFORMED FIM-4885 - 32-61-00-810-815-A - LG SLOW TO EXTEND OR RETRACT. 32-31-00-720-801-A - EXTENSION AND RETRAC - [SDR DXTA2025030502576](https://openairdocs.org/sdr/DXTA2025030502576), Mar 4, 2025: FLAP. NONE. ON ARRIVAL INTO DFW WE HAD A WINDSHEAR WARNING. WE EXECUTED THE EXCAPE MANUVER AS CONFIGURED. AFTER THE EVENT WE WERE CLEANING UP THE AIRCRAFT AND HIT ANOTHER W - [SDR DXTA2024081900253](https://openairdocs.org/sdr/DXTA2024081900253), Aug 16, 2024: CONTROL MODULE. FAILED. AFTER GETTING CLEARANCE TO TAXI, WE BOTH CHECK OUR BRAKES AND SEEM TO OPERATE. ABOUT 20 SECONDS LATER WE RECEIVED THE BKF FAIL YELLOW CAS. WE LOST THE BRAKES AN - [SDR DXTA2024022811030](https://openairdocs.org/sdr/DXTA2024022811030), Feb 27, 2024: ADC. FAILED. AIR DATA COMPUTER: GEA 1 FAIL CAS DURING FLIGHT. THIS CAUSED LOSS OF MANY INDICATIONS INCLUDING GEAR DOWN AND LOCKED. POWERED AIRCRAFT AND IT POWERED NORMALLY W - [SDR DXTA2023020680030](https://openairdocs.org/sdr/DXTA2023020680030), Feb 5, 2023: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: CABIN EMER LIGHTS WERE ILLUMINATED WITH BOTH ENGINES RUNNING AND EMER LT SWITCH IN ARM. EMER LT NOT ARM CAS WAS ALSO ILLUMINATED WITH THE SWI - [SDR DXTA2022112975090](https://openairdocs.org/sdr/DXTA2022112975090), Nov 28, 2022: BATTERY PACK. INOPERATIVE. IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS REMAIN ON, THEY GO OFF IN THE OFF POSITION. REMOVED FAULTING AFT EMER BATTERY AND INSTALLED TESTED EMER BATTERY. - [SDR DXTA2022110773470](https://openairdocs.org/sdr/DXTA2022110773470), Nov 6, 2022: LIGHT. DEFECTIVE. EMERGENCY LIGHTING: WHITE EMERGENCY LIGHT ON THE ISLE NEXT TO SEAT 6 IS BROKEN COMPLETELY OFF. CABLES ARE EXPOSED AND THE LIGHT IS DETACHED. // SIGNOFF// TECH R - [SDR DXTA2021062844380](https://openairdocs.org/sdr/DXTA2021062844380), Jun 28, 2021: CLAMP. LEAKING. BLEED 2 LEAK YELLOW CAS: AFTER TAKEOFF ON CLIMB OUT GOT A BLEED 2 LEAK CAS. FOLLOWED QRH AND CAS EXTINGUISHED. WHILE BURNING OFF FUEL FOR RETURN LANDING BLEED 2 - [SDR 2021F00149](https://openairdocs.org/sdr/2021F00149), Jun 7, 2021: LIGHT. INOPERATIVE. DURING PREFLIGHT CHECK, THE AIRCREW NOTED THE CABIN EMERGENCY EXIT LIGHT ON CABIN SIDEWALL NOT OPERATING. TROUBLESHOT TO ELECTRICAL CONNECTOR NOT CONNECTED. RE- - [SDR DXTA2021011304589](https://openairdocs.org/sdr/DXTA2021011304589), Jan 13, 2021: BATTERY. DEFECTIVE. WHEN EMERGENCY LIGHT SWITCH IS IN ARM & ON POSITION, CABIN EMERGENCY OVERHEAD LIGHTS, AND EXIT SIGN LIGHT PULSATES. CONTACTED EMB FOR MORE INFORMATION ON THE EM - [SDR 2020FA0000420](https://openairdocs.org/sdr/2020FA0000420), Sep 22, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LT ELEVATOR: ADJUSTABL - [SDR DXTA2016091006298](https://openairdocs.org/sdr/DXTA2016091006298), Sep 10, 2016: UNKNOWN. ODOR. BURNING RUBBER ODOR ON APPROACH AND DURING TAXI. SUSPECT ENVIRO SYSTEM. OPERATIONALLY CHECKED ECS AND BLEED AIR SYS AND COULD NOT NOTICE UNUSUAL ODORS. CHECKED - [SDR DXTA2015072706049](https://openairdocs.org/sdr/DXTA2015072706049), Jul 24, 2015: POWER SUPPLY. FAILED. STRANGE ODOR AT CRUISE ALTITUDE. EMERGENCY LIGHTS TRIGGER ON, RIGHT STAIR LIGHT WAS OUT. EXERCISED A PRECAUTIONARY LANDING. TROUBLESHOT EMERGENCY LIGHTS AND FOU - [SDR CWQD2015061002](https://openairdocs.org/sdr/CWQD2015061002), Jun 10, 2015: BRAKE ASSY. DAMAGED. DURING MX CHECKLIST FOUND RT MLG BRAKE ASSEMBLY ROTOR PLATE RIVETS MISSING & OTHERS COMING OUT. - [SDR CWQD2015061001](https://openairdocs.org/sdr/CWQD2015061001), Jun 10, 2015: BRAKE ASSY. DAMAGED. DURING MX CHECKLIST FOUND LT MLG BRAKE ASSEMBLY ROTOR PLATE RIVETS MISSING & OTHERS COMING OUT. - [SDR DXTA2014031405686](https://openairdocs.org/sdr/DXTA2014031405686), Mar 13, 2014: ELECTRONIC UNIT. FAILED. DURING FLIGHT, YELLOW X'S WERE DISPLAYED OVER THE FLAP INDICATOR & SPOILER INDICATOR. NO FLAP FAIL MESSAGE DISPLAYED. TRIED FLAPS 1 BUT THEY DID NOT WORK. COMPL ## Service difficulty reports on N303QS not matched to an aircraft (10) They name N303QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200809153275](https://openairdocs.org/sdr/DXTA200809153275), Sep 15, 2008: BUSHING. DETERIORATED. STARTED BOTH ENGINES UNEVENTFULLY THEN LT ENGINE UNEXPECTEDLY STOPPED RUNNING. FOUND RUBBER BUSHING ON LT ENGINE BELLCRANK DETERIORATED. REPLACED BUSHING. C/W G - [SDR DXTA200803210](https://openairdocs.org/sdr/DXTA200803210), Jul 31, 2008: BRAKE SYS. MALFUNCTIONED. F/O BRAKE PEDALS ARE SOFT. CHECKED RUDDER WEBBING FOR CRACKS. NONE FOUND. BLED BRAKES IAW AN E-MAIL & MM 32-42-00, OPS CHECKS OK. - [SDR DXTA200802794](https://openairdocs.org/sdr/DXTA200802794), Jan 24, 2008: ENGINE. VIBRATION. WHEN INCREASING POWER TO INITIATE CLIMB FROM 17000FT WE ENCOUNTERED LOUD NOISE FOLLOWED BY STRONG ODOR. REMOVED AND REPLACED NR1 ENGINE WITH REPAIRED UNIT IAW M - [SDR DXTA200702370](https://openairdocs.org/sdr/DXTA200702370), Jul 31, 2007: ENGINE. MALFUNCTIONED. LT ENGINE QUIT AFTER NORMAL START SEQUENCE AND STABILIZATION. AFTER PERFORMING GENERATOR CHECK NOTICED LT FUEL BOOST PUMP ANNUNCIATOR ON, THEN N2 ROLLING DOWN. - [SDR DXTA200702259](https://openairdocs.org/sdr/DXTA200702259), Jun 12, 2007: UNKNOWN. UNKNOWN. ON TAKEOFF WHEN CONTROL YOKE PULLED BACK FOR ROTATION , SOMETHING APPARENTLY TRIED TO JAM CAUSING MOMENTARY INCREASE IN RESISTANCE. JAM STOPPED AND CONTROLS BRO - [SDR DXTA200701932](https://openairdocs.org/sdr/DXTA200701932), Feb 13, 2007: UNKNOWN. UNKNOWN. LT FUEL BOOST PUMP CB POPED DURING LT FUEL X FEED OPERATION. REMOVED UNSERVICEABLE FUEL BOOST PUMP P/N 1C7-12 S/N BB18 AND INSTALLED OVERHAULED PUMP P/N 1C7-12- - [SDR DXTA200601624](https://openairdocs.org/sdr/DXTA200601624), Sep 30, 2006: BRAKE ASSY. WEAK. LEFT CAPTAINS BRAKE PEDAL VERY SPONGY. BLED LEFT AND RIGHT BRAKE SYSTEMS PER 560 M/M 32-42-00. TAXI AND LEAK CHECKS ARE GOOD. - [SDR DXTA200601606](https://openairdocs.org/sdr/DXTA200601606), Sep 18, 2006: BOLT. UNKNOWN. LT AILERON SEEM TO BIND SLIGHTLY AND MAKES `CLUCKING` SOUND WHEN MOVING UP AND DOWN. REMOVED AND REPLACED LT AILERON YOKE BEARINGS AND ALL BOLTS. OPS CHECKS GOO - [SDR DXTA200300057](https://openairdocs.org/sdr/DXTA200300057), Jul 4, 2003: LANDING GEAR. INOPERATIVE. NORMAL GEAR EXTENSION INOPOPERATIVE, HANDLE DOWN WITH NO HYDRAULIC PRESSURE INDICATOR , NO GEAR UNLOCK EMERGENCY EXTENSION COMPLIED WITH IAW CHECKLIST, LANDING - [SDR DXT200300057](https://openairdocs.org/sdr/DXT200300057), Jul 4, 2003: LANDING GEAR. INOPERATIVE. NORMAL GEAR EXTENSION INOPERATIVE, HANDLE DOWN WITH NO HYDRAULIC PRESSURE INDICATOR , NO GEAR UNLOCK EMERGENCY EXTENSION COMPLIED WITH IAW CHECKLIST, LANDING UN ## 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 S A 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 S A EMB-505 aircraft: https://openairdocs.org/model/embraer-s-a-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.