# N353QS: 2014 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: 50500263 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: December 4, 2014 - Certificate issued: March 6, 2025 - Expires: March 31, 2032 - Mode S code: A3F161 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=353QS - Page: https://openairdocs.org/aircraft/N353QS 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 N353QS. ## FAA accident and incident reports None matched to N353QS. ## Reports on N353QS not matched to an aircraft (1) They name N353QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20040109002929I](https://openairdocs.org/incident/20040109002929I), Jan 9, 2004: Cessna 560CESSNA (N353QS), Albany, NY. (-23) At 1546E, executive jet aviation flight 353, a C560, landed on runway 1 and the tower observed smoke emitting from the left engine while exiting onto… ## 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 DXTA2026070908718](https://openairdocs.org/sdr/DXTA2026070908718), Jul 6, 2026: WIRE. BROKEN. DOOR PAX OPEN CAS MESSAGE DISPLAYED BRIEFLY WHILE CLIMBING THROUGH 11,000 FEET. CLIMBING THROUGH FL210 THE MESSAGE RETURNED. WE RAN THE QRH AND BEGAN THE REQUIR - [SDR DXTA2026070708691](https://openairdocs.org/sdr/DXTA2026070708691), Jul 5, 2026: PROXIMITY SWITCH. FAILED. RED WARNING CAS DOOR PAX OPEN CAME ON MULTIPLE TIMES WITHIN FLIGHT. ONCE AT FL380, ONCE AT FL400, BOTH TIME IT WENT AWAY WITHIN A COUPLE MINUTES. FOLLOWED THE Q - [SDR DXTA2025030402548](https://openairdocs.org/sdr/DXTA2025030402548), Mar 1, 2025: SEAL. UNSECURE. FUSELAGE PLATES / SKINS / PANELS: REPEAT WRITE UP, 3RD TIME. INTERMITTENT, LOUD, NOTICEABLE HUMMING SOUND AND VIBRATION COMING FROM THE RIGHT SIDE OF THE AIRCRA - [SDR DXTA2024121901538](https://openairdocs.org/sdr/DXTA2024121901538), Dec 15, 2024: SEAL. DAMAGED. DURING CLIMB OUT AROUND 25,000FT A VERY LOUD BUZZING/HUMMING NOISE WAS HEARD. WE COULD FEEL THE VIBRATIONS IN THE FLOOR BOARD IN THE COCKPIT. WHEN WE LEVELED OF - [SDR DXTA2023112210123](https://openairdocs.org/sdr/DXTA2023112210123), Nov 21, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: GO FROM THE OFF POSTION TO ARM POSITION THE EMR LIGHTS COME ON. THEY STAY ON FOR AROUND 3 SECONDS IN THE ARM POSITION THEN GO OFF. PERFORMED - [SDR DXTA2023062689580](https://openairdocs.org/sdr/DXTA2023062689580), Jun 26, 2023: UNKNOWN. UNKNOWN. IMMEDIATELY AFTER TAKEOFF "AUTO PILOT FAIL" "AUTO TRIM FAIL" AND "PICH TRIM NORM FAIL" EICAS MESSAGES ILLUMINATED. AIRCRAFT FLOWN TO A LANDING WITH THE BACKUP M - [SDR DXTA2023061288480](https://openairdocs.org/sdr/DXTA2023061288480), Jun 12, 2023: UNKNOWN. UNKNOWN. COCKPIT/CABIN NOISE: CLIMBING ABOVE 38000 FT THE CABIN CLIMB RATE BEGAN TO SPIKE AND DESCEND BETWEEN PLUS/MINUS APPROXIMATELY 1800 FT PER MIN FOLLOWED BY A LOUD - [SDR DXTA2022062464550](https://openairdocs.org/sdr/DXTA2022062464550), Jun 24, 2022: PROXIMITY SENSOR. OUT OF ADJUST. BOTH EMERGENCY AIRSTAIR STEP LIGHTS INOP WITH THE EMER LT SWITCH IN THE ON POSTION. // SIGNOFF// RESECURED FLOOR PROXIMITY LIGHT IN REFERENCE TO EMBRAER PHENOM - [SDR DXTA2022061964200](https://openairdocs.org/sdr/DXTA2022061964200), Jun 19, 2022: LANDING GEAR. WARNING LIGHT. LG LEVER DISAG RED CAS: RED CAS LG LEVER DISAG NOTED DURING GEAR RETRACTION AFTER T/O. NO ISSUES NOTED DURING EXTENSION AND RETURN LANDING.//CORRECTIVE ACTION// - [SDR DXTA2022040659730](https://openairdocs.org/sdr/DXTA2022040659730), Apr 5, 2022: NONE. NONE. RIGHT ENGINE ENGINE FAN BLADE: DURING TAKEOFF ROLL AT ROTATION, WE HAD A VERY LARGE BIRD STRIKE WITH INGESTION IN THE RIGHT ENGINE. - [SDR DXTA2021082447530](https://openairdocs.org/sdr/DXTA2021082447530), Aug 23, 2021: RELAY. ABNORMAL. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTING WAS OBSERVED TO BE BLINKING ON AND OFF DURING FLIGHT WITH THE EMER LIGHT IN THE ARMED POSITION. TROUBLESHOT DISCREPA - [SDR DXTA2021072945980](https://openairdocs.org/sdr/DXTA2021072945980), Jul 28, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: ENROUTE TO KADS THE CABIN EMERGENCY LIGHTING BEGAN FLASHING AND CONTINUED THROUGH THE DURATION OF THE FLIGHT. //SIGNOFF// T/S SYSTEM REMOVED - [SDR DXTA2021011804609](https://openairdocs.org/sdr/DXTA2021011804609), Jan 17, 2021: CONTROLLER. DEFECTIVE. IN LEVEL CRUISE AT 41,000 FEET, PRESSURIZATION STARTED TO CLIMB RATHER SWIFTLY. WITH O2 MASKS ON, WE STARTED AN EMERGENCY DECENT. WITH O2 MASK ON, CABIN PRESSUR - [SDR DXTA2020121604475](https://openairdocs.org/sdr/DXTA2020121604475), Dec 16, 2020: DOOR. OBSTRUCTED. MAIN CABIN DOOR WILL NOT OPEN HAD TO EXIT THE AIRPLANE THROUGH THE EMERGENCY EXIT DOOR. FOUND TRIM PIECE GETTING STUCK ON DOOR FRAME. REMOVED AND PROPERLY INSTA ## Service difficulty reports on N353QS not matched to an aircraft (10) They name N353QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2011100204741](https://openairdocs.org/sdr/DXTA2011100204741), Oct 2, 2011: ANTI-SKID VALVE. INOPERATIVE. BRAKES GRAB HARD WHEN PEDALS ARE APPLIED AND PULL ACFT TO THE LT. THE LT PULL IS MORE PROMINENT FROM THE RT SEAT. INSTALLED PRESS. GAGE'S FOUND RT SIDE ERRATIC. - [SDR DXTA2010112204316](https://openairdocs.org/sdr/DXTA2010112204316), Nov 21, 2010: BRAKE. DIRTY. THE LT BRAKE GRABBING WHEN PRESSURE IS APPLIED. BRAKE IS STILL SMOKING A LITTLE AFTER SHUTDOWN. REMOVED LEFT BRAKE ASSY, CLEANED AND REINSTALLED. PERFORMED HIGH - [SDR DXTA2010112204313](https://openairdocs.org/sdr/DXTA2010112204313), Nov 18, 2010: STRUT. LEAKING. ON LANDING ROLL, BRAKES FELT "GRABBY". UPON POST FLIGHT INSP, FOUND LT MAIN GEAR STRUT WET AND FLUID DRIPPING FROM MAIN STRUT INBD SIDE OF STRUT. LT STRUT IS LE - [SDR DXTA2009052803668](https://openairdocs.org/sdr/DXTA2009052803668), May 28, 2009: LINE. LEAKING. TROUBLE SHOT TO LEAKING FLEX LINE ON CO PILOTS STATIC PORT NR 2 SYSTEM. REPAIRED FLEX LINE AND COMPLIED WITH PITOT/STATIC SYSTEM LEAK CHECK/TEST IAW MM 34-11-25 - [SDR DXTA200905283668](https://openairdocs.org/sdr/DXTA200905283668), May 28, 2009: UNKNOWN. UNKNOWN. BOTH PFD'S DISPLAY IAS ALT ANNUNCIATORS. DURING CLIMB THE LT SIDE IAS ALT LAG BEHIND. DURING DESCENT THE LT SIDE IAS, ALT STAY HIGHER. ONCE LEVEL, THE LT SIDE S - [SDR DXTA200810123303](https://openairdocs.org/sdr/DXTA200810123303), Oct 12, 2008: ANTI-SKID SYS. MALFUNCTIONED. CO-PILOTS BRAKES LT PEDAL MOVES ABOUT 1 INCH THEN GRABS, RT PEDAL MOVES .5 INCH THEN GRABS. ABLE TO MAINTAIN DIRECTIONAL CONTROL, PILOTS BRAKES OK. BLED THE ANT - [SDR DXTA2008101303303](https://openairdocs.org/sdr/DXTA2008101303303), Oct 12, 2008: BRAKE SYS. MALFUNCTIONED. CO-PILOTS BRAKES LEFT PEDAL MOVES ABOUT 1 INCH THEN GRABS, RIGHT PEDAL MOVES .5 INCH THEN GRABS. - [SDR DXTA200802996](https://openairdocs.org/sdr/DXTA200802996), Apr 14, 2008: PUMP. INOPERATIVE. CREW REPORTED LIGHT ILLUMINATED AS SOON AS SQUAT SWITCH MADE ON LANDING, THEY ONLY GOT 2 GOOD APPLICATIONS BEFORE PREX DEPLETED. AFTER LANDING "POWER BRAKE LOW - [SDR DXTA200701869](https://openairdocs.org/sdr/DXTA200701869), Jan 19, 2007: ACTUATOR. INOPERATIVE. DURING CRUISE AT 17,00 AND 280 KIAS THE AIRCRAFT WOULD CLIMB +500'/MIN WITH FULL NOSE DOWN TRIM. REMOVED AND REPLACED ELEVATOR TRIM ACTUATOR. OPS CHECKS GOOD IA - [SDR DXTA200400215](https://openairdocs.org/sdr/DXTA200400215), Jan 9, 2004: ENGINE. SMOKE. AFTER LANDING AT ALB, DURING TAXIING TOWER INSTRUCTED FLIGHT CREW TO SHUTDOWN AIRCRAFT AND EVACUATE DUE TO SMOKE COMING OUT FROM LT ENGINE. DISCHARGED BOTH BOTT ## 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.