# N322QS: 2016 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: 50500383 - Year built: 2016 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: November 16, 2016 - Certificate issued: March 31, 2022 - Expires: March 31, 2029 - Mode S code: A3772D - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=322QS - Page: https://openairdocs.org/aircraft/N322QS 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 N322QS. ## NTSB investigations on N322QS not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN14FA505](https://openairdocs.org/ntsb/CEN14FA505), Sep 19, 2014: Embraer EMB 505 (N322QS), Conroe, TX, substantial damage. Probable cause: The second-in-command's (SIC) engagement of the emergency parking brake (EPB), which decreased the airplane's braking performance and prevented it from stopping on the available runway. Contributing… ## FAA accident and incident reports None matched to N322QS. ## Reports on N322QS not matched to an aircraft (1) They name N322QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 20140919016989A](https://openairdocs.org/incident/20140919016989A), Sep 19, 2014: Embraer S A EMB-505 (N322QS), Conroe, TX, Substantial damage. On September 19, 2014 at 08:47 local time aircraft N322QS completed an instrument approach to landing on runway 1 at Lone Star Executive Airport. The SIC was… ## Service difficulty reports (9) 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 DXTA2025110705582](https://openairdocs.org/sdr/DXTA2025110705582), Nov 5, 2025: SOCKET. NOT SEATED. EXIT LIGHT AT MAIN ENTRANCE NOT ILLUMINATED WHEN EMERGENCY LIGHTING IS ACTIVATED. RESEATED SOCKET. OPS CHECK GOOD. IAW EMB505 AMM 33-52-13 - [SDR DXTA2024120401354](https://openairdocs.org/sdr/DXTA2024120401354), Dec 1, 2024: BATTERY PACK. MALFUNCTIONED. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLICKERING WHEN EMER LT SWITCH IN ARM POSITION. CORRECTIVE ACTION; REPLACED BOTH EMERGENCY BATTERIES IN REF. TO EMB-50 - [SDR DXTA2024120201300](https://openairdocs.org/sdr/DXTA2024120201300), Nov 26, 2024: LIGHT. NO DISCREPANCY. CABIN EMERGENCY LIGHTS STAYS ON WITH SWITCH IN THE ARM POSITION AND MAIN DC POWER ON. ACCOMPLISHED THE EMERGENCY LIGHT INADVERTENTLY OPERATIVE IAW EMB-505 FIM 3 - [SDR DXTA2023122610416](https://openairdocs.org/sdr/DXTA2023122610416), Dec 23, 2023: BATTERY. FAILED. EMERGENCY LIGHTS COME ON WHEN AN ARM POSITION AND STAY ON. PERFORMED EMER LT BATTERY TOP CHARGE IN REF TO FORM TC-505-33-200403. OPS CHECK OF EMER LT SWITCH IN - [SDR DXTA2021101150160](https://openairdocs.org/sdr/DXTA2021101150160), Oct 10, 2021: NONE. NONE. LEFT MLG BRAKE: WHITE SMOKE IS EMANATING FROM LEFT MLG BRAKE AFTER BLOCK-IN. COPILOT ACCOMPLISHED THE LANDING, AND REPORTED FEELING "SPONGINESS" IN THE LEFT BRA - [SDR DXTA2021101150170](https://openairdocs.org/sdr/DXTA2021101150170), Oct 10, 2021: NONE. NONE. FLOOR EMERG EXIT LIGHT: FORWARDMOST (WHITE) LIGHT WILL NOT ILLUMINATE. //SIGNOFF// C/W EMERGENCY LIGHT OPERATIONAL TEST VERIFIED EXIT IDENTIFIER SIGN, EXIT MARK - [SDR DXTA2019071202605](https://openairdocs.org/sdr/DXTA2019071202605), Jul 11, 2019: ELECTRONIC UNIT. MALFUNCTIONED. FLAP FAIL YELLOW CAS ILLUMINATED - FLAP FAIL YELLOW CAS MESSAGE ILLUMINATED IN FLIGHT AT CRUISE ALTITUDE. ACCOMPANIED BY SWPS FAULT YELLOW CAS MESSAGE, PTRIM BK - [SDR DXTR2019051001](https://openairdocs.org/sdr/DXTR2019051001), May 8, 2019: HYDRAULIC LINE. CRACKED. DURING RIGHT ENGINE START NO HYDRAULIC PRESSURE WAS INDICATED. SHUT DOWN ENGINE AND FOUND HYDRAULIC FLUID LEAKING FROM UNDER AC. FOUND RT ENGINE HYD EDP PRESSUR - [SDR DXTA2017110600001](https://openairdocs.org/sdr/DXTA2017110600001), Nov 3, 2017: PROXIMITY SWITCH. FAULTY. LANDING GEAR LEVER DISAGREE CAS MESSAGE ON GEAR RETRACTION ALONG WITH NOSE GEAR UNSAFE INDICATION. COMPLIED WITH QRH AND GEAR EXTENDED NORMALLY. REMOVED DEFECTI ## Service difficulty reports on N322QS not matched to an aircraft (18) They name N322QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2014091905888](https://openairdocs.org/sdr/DXTA2014091905888), Sep 19, 2014: BRAKE SYS. MALFUNCTIONED. LOSS OF BRAKING DURING LANDING ROLLOUT. - [SDR DXTA2010031004023](https://openairdocs.org/sdr/DXTA2010031004023), Mar 9, 2010: BRAKE SYS. WEAK. BOTH COPILOT BRAKE PEDAL ARE SOFT, TRAVEL 75 PERCENT THEN BRAKES GRAB; ALSO PULLS LT. PILOT SIDE BRAKE PRESSURES SEEM OK BUT HAVE A SLIGHT DELAY FOR BRAKING. FO - [SDR DXTA2010011403944](https://openairdocs.org/sdr/DXTA2010011403944), Jan 13, 2010: LANDING GEAR. MALFUNCTIONED. WHILE ATTEMPTING TO EXTEND THE LANDING GEAR, THE RED UNLOCK CAME ON FOR 3 SECONDS WITH NO AUDIBLE GEAR EXTENSION SOUNDS. THE AFTER 3 SECONDS THE GEAR EXTENDED N - [SDR DXTA2010011103942](https://openairdocs.org/sdr/DXTA2010011103942), Jan 9, 2010: ROD END. OUT OF ADJUST. BOTH THROTTLE LEVERS AT ALTITUDE BECOME EXTREMELY DIFFICULT TO MOVE. THE LT THROTTLE LEVER TAKES 2 HANDS AND EXCESSIVE FORCE TO MAKE ANY TYPE OF POWER CHANGE. A - [SDR DXTA2010011103936](https://openairdocs.org/sdr/DXTA2010011103936), Jan 9, 2010: BRAKE ASSY. MALFUNCTIONED. BOTH PILOT AND CO-PILOT LT BRAKE PEDAL REQUIRES EXCESSIVE TRAVEL/FORCE. BLED BRAKES AND AFTER BLEEDING BRAKES SYS NOTED A PUDDLE OF HYD FLUID UNDER PILOTS LT BR - [SDR DXTA2009051403650](https://openairdocs.org/sdr/DXTA2009051403650), May 13, 2009: CAM. LOOSE. LT ENGINE T/R ARM LIGHT CAME ON IN FLIGHT AND ON THE GROUND. THE T/R'S WOULD NOT STOW IMMEDIATLY-ONCE STOWED, THE LT T/R WOULD DEPLOY EVERYTIME THE POWER LEVER - [SDR DXTA2009042003607](https://openairdocs.org/sdr/DXTA2009042003607), Apr 19, 2009: DISPLAY. BURNED. STRONG SYNTHETIC BURNING ODOR FROM COCKPIT WAS FOLLOWED MINUTES LATER BY FMS SCREEN GOING BLANK. FMS UNIT STILL DISPLAYED DATA ON MFD. BURNING ODOR FILLED ACFT. - [SDR DXTA200802962](https://openairdocs.org/sdr/DXTA200802962), Mar 24, 2008: THROTTLE CABLE. FROZEN. LT (NR 1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW M - [SDR DXTA20082962](https://openairdocs.org/sdr/DXTA20082962), Mar 24, 2008: THROTTLE CABLE. FROZEN. LT (NR1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW MM - [SDR DXTA20082873](https://openairdocs.org/sdr/DXTA20082873), Feb 13, 2008: BRAKE. WEAK. BOTH LT BRAKES REQUIRE MORE PRESSURE THAN THE RT. REMOVED AND REPLACED LT AND RT BRAKE ASSY'S IAW MM CH. 32-42-00. BLED BRAKES IAW MM CH 32-42-00. TAXI CHECK GO - [SDR DXTA200702706](https://openairdocs.org/sdr/DXTA200702706), Dec 22, 2007: GYRO. INOPERATIVE. NR 1 HEADING INDICATOR FAILED. 1 PFD, STANDBY HEADING INDICATOR AND MFD HEADING INDICATOR FAILED. REMOVED & REPLACED NR 1 DG IAW CE560 MM CHAPTER 34-21-05. OPS - [SDR DXTA200702402](https://openairdocs.org/sdr/DXTA200702402), Aug 14, 2007: RESERVOIR. OVERSERVICED. DURING ROLL OUT, THE BRAKES FAILED MOMENTARILY BUT HAD PRESSURE AT THE PEDALS. TROUBLESHOT SYSTEM AND FOUND BRAKE RESERVOIR TO BE OVERSERVICED. REMOVED SOME OF - [SDR DXTA200702379](https://openairdocs.org/sdr/DXTA200702379), Aug 2, 2007: PEDAL. STIFF. RT SEAT BRAKE PEDALS REQUIRE LARGE AMOUNT OF MOVEMENT TO WORK. RT PEDAL TRAVELS HALFWAY TO THE FLOOR BEFORE ANY PRESSURE IS FELT. BLED BRAKE SYSTEM IAW 560 MM 3 - [SDR DXTA200601662](https://openairdocs.org/sdr/DXTA200601662), Oct 16, 2006: BRAKE. MALFUNCTIONED. CO-PILOTS BRAKE PEDALS (LT AND RT) ARE SPONGY. IT TAKES APPROXIMATLEY 2 INCHES OF TRAVEL TO GET ANY BRAKING ACTION. VERIFIED DISCREPANCY FOUND BLEEDER SCREW LOO - [SDR DXTA200601558](https://openairdocs.org/sdr/DXTA200601558), Aug 16, 2006: LINK. OUT OF ADJUST. UPON APPLYING STATIC TAKEOFF POWER, NR1 ENGINE (LT SIDE) ONLY MADE 95.1 N1. THE BOOK CALLED FOR 96.7 PERCENT N1. OAT WAS 28 DEGREES C. CHECKED NR 1 ENGINE THROT - [SDR DXTA200601475](https://openairdocs.org/sdr/DXTA200601475), Jul 1, 2006: TRANSDUCER. INOPERATIVE. LEFT SIDE BRAKES FEEL VERY HARD ON LANDING. CONSTANT PRESSURE FELT THEN GRADUAL SOFT PRESSURE (DIFFERENT FROM ANTI-SKID RELEASE) HIGH SPEED TEST: SOFTER W/ANTI- - [SDR DXTA200500600](https://openairdocs.org/sdr/DXTA200500600), Feb 18, 2005: SWITCH. FAILED. AT FL 410 RECEIVED THE EMERGENCY PRESS LIGHT. RAN THE CHECKLIST AND RESET THE SYSTEM BACK TO NORMAL. THE CABIN ALTITUDE WENT TO 9000 FEET. THE RATE CONTROLLER S - [SDR DXTA200400414](https://openairdocs.org/sdr/DXTA200400414), Oct 5, 2004: ENGINE. SHUTDOWN. WHILE BEING VECTORED FOR A VISUAL APPROACH, THE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED, FOLLOWED BY THE LEFT ENGINE UNCOMMANDED SHUT DOWN. DECLARED EMERGENCY ## 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.