# N319QS: 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: 50500164 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: September 23, 2013 - Certificate issued: September 10, 2026 - Expires: September 30, 2033 - Mode S code: A369AF - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=319QS - Page: https://openairdocs.org/aircraft/N319QS 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 N319QS. ## FAA accident and incident reports None matched to N319QS. ## Service difficulty reports (21) 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 DXTA2026072108881](https://openairdocs.org/sdr/DXTA2026072108881), Jul 17, 2026: LATCH. LACK OF LUBE. CARGO DOOR LIGHT OPEN CAS CAME ON IN FLIGHT. SCHEMATIC SHOWED IT AS LT FRONT BAGGAGE DOOR. CLEANED AND LUBRICATED THE LH NOSE DOOR LATCH DUE TO OPEN CAS MESSAGE - [SDR DXTA2025092305031](https://openairdocs.org/sdr/DXTA2025092305031), Sep 20, 2025: BATTERY. INOPERATIVE. NOTICED THE CABIN ROOF AND EXIT LIGHTS BLINKING DURING THE FLIGHT. CYCLED THE EMER LT SWITCH AND THE CABIN ROOF LIGHTS, EXIT SIGNS, AND ONE RED AND ONE WHITE FL - [SDR DXTA2025032602793](https://openairdocs.org/sdr/DXTA2025032602793), Mar 23, 2025: BLOWER. FAILED. AVIONICS FAN FAIL(AVNX FAN FAIL) CAS MESSAGE ILLUMINATED DURING COCKPIT SETUP. STRONG BURNING ODOR NOTICABLE IN COCKPIT AND CABIN. OCCURRED WITH & WITHOUT GROUN - [SDR DXTA2024110801066](https://openairdocs.org/sdr/DXTA2024110801066), Nov 5, 2024: PRESSURE SWITCH. DEFECTIVE. FUEL PUMP 1 FAIL YELLOW CAS: NUMBER 1 FUEL PUMP FAIL INFLIGHT WITH ASSOC. #1 FUEL PRESS. CORRECTIVE ACTION; REMOVED AND REPLACED THE #1 {LH) FUEL SYSTEM LOW PRE - [SDR DXTA2024070112227](https://openairdocs.org/sdr/DXTA2024070112227), Jun 30, 2024: TAPE. DETACHED. ON CLIMB OUT PASSING 14000 FT, WE GOT A RED CAS MESSAGE : DOOR PAX OPEN. FOLLOWED THE QRH AND DIVERTED TO ALB. ON FINAL PASSING 1800 FT THE CAS MESSAGE EXTINGUI - [SDR DXTA2024030111045](https://openairdocs.org/sdr/DXTA2024030111045), Feb 29, 2024: LOCK. OUT OF ADJUST. MAIN DOOR OPEN INDICATIONS ON MFD. VISUAL INSPECTION OF THE DOOR SHOWED TOP RT FLAG NOT FULLY SEATED IN PLACE. WHILE TECH WAS CHECKING THE MEASUREMENT OF THE GA - [SDR DXTA2024021310883](https://openairdocs.org/sdr/DXTA2024021310883), Feb 12, 2024: DOOR. LACK OF LUBE. DOOR PAX OPEN WARNING CAS CLIMBING THROUGH FL190. MESSAGE WOULD COME AND GO FOR A MINUTE OR SO AT A TIME. NO PRESSURIZATION ISSUES NOTED. UPON LANDING, RED HAND - [SDR DXTA2023120410228](https://openairdocs.org/sdr/DXTA2023120410228), Dec 3, 2023: BATTERY. FAULTED. ENROUTE FROM KLGB TO KDAL EMERGENCY CABIN LIGHTS BLINKING ON AND OFF. PERFORMED TROUBLESHOOTING IAW FIM 33-50-00-801-802-A FOUND AFT EMERGENCY LIGHT BATTERY AT - [SDR EBVR20231012001](https://openairdocs.org/sdr/EBVR20231012001), Oct 12, 2023: SKIN. CORRODED. CORROSION FOUND ON THE LH WING TRAILING EDGE , PERFORM LH WING TRAILING EDGE REPAIR DOUBLER. REPAIRED BLENDED AREAS ON TRAILING EDGE OF L/H WING IAW NETJETS RFT - [SDR DXTA2023091595450](https://openairdocs.org/sdr/DXTA2023091595450), Sep 14, 2023: UNKNOWN. UNKNOWN. DURING CLIMB WE RECEIVED A DOORBAG (RH) OPEN CAS MESSAGE AND RAN THE CHECK LIST IN THE QRH. WE LANDED AT KHPN. PERFORMED FIM TASK 52-72-00-810-802-A AND FIM TAS - [SDR DXTA2022032959200](https://openairdocs.org/sdr/DXTA2022032959200), Mar 29, 2022: LIGHT. MALFUNCTIONED. CABIN EMERG LIGHT: DURING FLIGHT NOTICED THAT THE CABIN EMER LIGHTS WERE ILLUMINATED WITH THE EMER LT SWITCH IN THE ARM POSITION. THE EMER LIGHTS STARTED TO FLI - [SDR DXTA2022021556770](https://openairdocs.org/sdr/DXTA2022021556770), Feb 14, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR HANDLE: MAIN DOOR HANDLE SNAPPED OFF WHILE OPENING FROM OUTSIDE. "CORRECTIVE ACTION" REMOVED AND REPLACED EXTERNAL HANDLE ASSY WITH NO DEFECTS NOTED A - [SDR DXTA2021121353450](https://openairdocs.org/sdr/DXTA2021121353450), Dec 12, 2021: NONE. NONE. FLOOR EMERG EXIT LIGHT: RED FLOOR EMERGENCY EXIT LIGHT BELOW THE EMERGENCY EXIT IS INOP // SIGNOFF// VERIFIED THE RED FLOOR EMER AISLE LIGHT DID NOT ILLUMINATE, - [SDR DXTA2021032239820](https://openairdocs.org/sdr/DXTA2021032239820), Mar 22, 2021: SWITCH. OUT OF POSITION. PTRIM MNL FAIL YELLOW CAS: SHORTLY AFTER INITIATING DESCENT FROM FL410, WE OBSERVED A PTRIM NML FAIL AMBER CAS. WE COMPLIED WITH QRH. CAS MESSAGE REMAINED ILLUM - [SDR DXTA2020111104329](https://openairdocs.org/sdr/DXTA2020111104329), Nov 10, 2020: INDICATOR. DEFECTIVE. SHORTLY AFTER TAKEOFF AND AFTER WE HAD RECEIVED AHRS 2 FAULT WE RECEIVED AHRS 1 FAULT. IT WAS INTERMITTENT UNTIL LANDING AND THEN RETURNED TO NORMAL. REMOVED IN - [SDR 2020FA0000486](https://openairdocs.org/sdr/2020FA0000486), Oct 30, 2020: 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 LEFT ELEV - [SDR JGVR20200115001](https://openairdocs.org/sdr/JGVR20200115001), Jan 15, 2020: BALANCE WEIGHT. CORRODED. CORROSION ON RH ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS. REPLACED 9 EA RH ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS WITH NEW IN SAME LOCATION P/N PE915109-L33. - [SDR DXTA2019121203191](https://openairdocs.org/sdr/DXTA2019121203191), Dec 12, 2019: MODULATING VALVE. DEFECTIVE. DUCT 1 OVER TEMP YELLOW CAS ILLUMINATED - DUCT 1 OVER TEMP CAS ILLUMINATED CLIMBING IN THE MID 20S FLIGHT LEVEL. FOLLOWED QRH, WENT TO MANUAL HEAT, BLEED ONE OF - [SDR DXTA2018022300629](https://openairdocs.org/sdr/DXTA2018022300629), Feb 23, 2018: UNKNOWN. ODOR. ELECTRICAL ODOR COINCIDING WITH THE GEN2 FAIL MESSAGE. PERFORMED FIM4885 21-20-00-810-801A SMOKE/ABNORMAL ODOR IN THE CABIN/COCKPIT-UNKNOWN SOURCE. OPERATED ACS - [SDR 2014FA0000720](https://openairdocs.org/sdr/2014FA0000720), Dec 23, 2014: KEY. BROKEN. POST MAINTENANCE GROUND RUNUP OF NR 1 ENGINE, THERE WAS NO OIL PRESSURE. ENGINE WAS SHUTDOWN IMMEDIATELY. REMOVED OIL FILTER AND CHIP DETECTOR. NO DEFECTS NOTED - [SDR DXTA2014021305653](https://openairdocs.org/sdr/DXTA2014021305653), Feb 12, 2014: SWITCH. OUT OF ADJUST. CLIMBING OUT OF 34,500 THE RED CAS MESSAGE, PAX DOOR OPEN, ILLUMINATED. WE RAN THE QRH CHECKLIST & DIVERTED TO KPBI. UPON DESCENDING TO 5000 WHEN THE CABIN PRES ## Service difficulty reports on N319QS not matched to an aircraft (15) They name N319QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2010060404112](https://openairdocs.org/sdr/DXTA2010060404112), Jun 3, 2010: CONNECTOR. LOOSE. DURING LANDING AND ARRIVAL AT DESTINATION, LANDING GEAR FAILED TO EXTEND. ACCOMPLISHED THE EMERGENCY CHECKLIST ITEMS AND THE GEAR EXTENDED WITHOUT ANY PROBLEMS. - [SDR DXTA2010030404012](https://openairdocs.org/sdr/DXTA2010030404012), Mar 3, 2010: UNKNOWN. MALFUNCTIONED. DESCENDING THROUGH FL400, THE CABIN RATE OF CLIMB INDICATOR SPIKED AND REMAINED AT MAX RATE OF CLIMB (6000 FPM); THE SAFETY VALVES LIMITED THE CABIN ALTITUDE TO - [SDR DXTA2010F00037](https://openairdocs.org/sdr/DXTA2010F00037), Feb 11, 2010: WARNING LIGHT. ILLUMINATED. ON APPROACH TO ASE, EXT FLAPS TO 15, HYD PUMP REMAINED ILLUMINATED. REPOSITIONED FLAPS AND THE LIGHT REMAINED ON. IMMEDIATELY EXT GEAR AND FULL FLAPS. THE HYD L - [SDR DXTA2009072003732](https://openairdocs.org/sdr/DXTA2009072003732), Jul 19, 2009: BUSHING. WORN. LT ENGINE SHUTDOWN ON CONTROLS AND SPEED BRAKE TEST. FOUND BUSHING IN RT ENGINE BELLCRANK WORN. REPLACED BUSHING. C/W RIGGING CHECK OF LT FCU, FLOW DIVIDER AND - [SDR DXTA2008120203385](https://openairdocs.org/sdr/DXTA2008120203385), Dec 2, 2008: BRAKE ASSY. WEAK. BRAKES ARE SPONGY ON BOTH SIDES. COPILOTS SIDE BRAKES ARE WORSE. FOUND CO-PILOTS LT BRAKE PEDAL A LITTLE SPONGY. C/W BRAKE BLEEDING PROCEDURES IAW MM 32-42-00 R - [SDR DXTA2008120303385](https://openairdocs.org/sdr/DXTA2008120303385), Dec 2, 2008: BRAKE ASSY. WEAK. BRAKES ARE SPONGY ON BOTH SIDES. COPILOTS SIDE BRAKES ARE WORSE. - [SDR DXTA200802772](https://openairdocs.org/sdr/DXTA200802772), Jan 16, 2008: SQUAT SWITCH. INOPERATIVE. IMMEDIATELY AFTER T/O GEAR HANDLE WOULD NOT RELEASE TO RETRACT GEAR. FOUND LEFT SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED LT SQUAT SWITCH. SYSTEM OPERATION CHECK - [SDR DXTA200702708](https://openairdocs.org/sdr/DXTA200702708), Dec 22, 2007: CONTROL BOX. INOPERATIVE. ON LANDING AND AFTER APPLYING THE BRAKES, THE BRAKES SEEMED TO GRAB AND WE BEGAN TO SKID. THE RT MAIN TIRE BLEW. AIRCRAFT VEERED TO THE RT SKIDDING OFF THE RWY. - [SDR DXTA200702538](https://openairdocs.org/sdr/DXTA200702538), Oct 12, 2007: UNKNOWN. ODOR. THERE IS A BURNING ELECTRICAL ODOR IN COCKPIT WHEN DEFOG FAN IS SELECTED ON. REMOVED & REPLACED DEFOG BLOWER WITH OVERHAULED UNIT IAW CE-560 MM CH 21-21-01. OPS - [SDR DXTA200702314](https://openairdocs.org/sdr/DXTA200702314), Jul 2, 2007: BRAKE ASSY. WEAK. CO-PILOTS BRAKE PEDALS ARE SPONGY. REQUIRES THE BRAKE PEDALS TO BE PUMPED (2) TO (3) TIMES TO BUILD PRESSURE. BLED BRAKES. LT AND RT SIDE, TAXI CHECKED FOR BRAK - [SDR DXTA200702181](https://openairdocs.org/sdr/DXTA200702181), May 8, 2007: HUB. OUT OF LIMITS. WHILE DECELERATING STRAIGHT AHEAD ON THE RUNWAY, AT APPROX 20 KNOTS, BRAKES RELEASED MOMENTARILY THEM FUNCTIONED NORMALLY. AIRCRAFT WAS NOT IN A TURN. FOUND ANT - [SDR DXTA200701997](https://openairdocs.org/sdr/DXTA200701997), Mar 4, 2007: SQUAT SWITCH. OUT OF RIG. SQUAT SWITCH INOPERATIVE ON TAKEOFF , LANDING GEAR WOULD NOT RETRACT, FLIGHT TIMER INOPERATIVE, AOA INDEXER INOPERATIVE, LOW SPEED AWARENESS, TAPE INOPERATIVE. - [SDR DXTA200601427](https://openairdocs.org/sdr/DXTA200601427), Jun 5, 2006: ANTI-SKID SYS. MALFUNCTIONED. AT APPROXIMATELY 20 KNOTS THE ANTISKID ACTIVES FOR ABOUT 2 SECONDS AND THERE IS NO BRAKES. AT TIME OF OCCURANCE, BRAKES WERE NOT BEING APPLIED FORCEFULLY. PERFO - [SDR DXTA200500850](https://openairdocs.org/sdr/DXTA200500850), Jul 20, 2005: BRAKE ASSY. MALFUNCTIONED. DURING LANDING MINOR APPLICATION OF THE BRAKES WOULD LOCK UP TIRES. IT TOOK 6000 FT OF RUNWAY TO STOP. ANTI-SKID TESTS NORMALLY. ALL FLUIDS FULL. WHEN THE TIRES - [SDR DXTA200300074](https://openairdocs.org/sdr/DXTA200300074), Jul 29, 2003: BLEED VALVE. INOPERATIVE. POWER BRAKE LOW PRESS LIGHT AND ANTI SKID INOP. LIGHT ILLUMINATED DURING TAXI, LIGHTS STAYED ILLUMINATED AFTER CESSNA EMERGENCY CHECK LIST COMPLETED. - TROUBLES ## 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.