# N327QS: 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: 50500170 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: November 22, 2013 - Certificate issued: December 12, 2023 - Expires: December 31, 2030 - Mode S code: A389C0 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=327QS - Page: https://openairdocs.org/aircraft/N327QS 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 N327QS. ## FAA accident and incident reports None matched to N327QS. ## Service difficulty reports (24) 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 DXTA2026081409271](https://openairdocs.org/sdr/DXTA2026081409271), Aug 13, 2026: PRESSURE SWITCH. FAILED. DURING THE APPROACH APPROXIMATELY FIVE SECONDS AFTER THE LANDING GEAR WAS FULLY EXTENDED AND INDICATED DOWN AND LOCKED, A BRAKE FAIL CASS MESSAGE ILLUMINATED. T - [SDR DXTA2025112605809](https://openairdocs.org/sdr/DXTA2025112605809), Nov 23, 2025: BATTERY. INOPERATIVE. EMERGENCY LIGHTS FLICKERING CONSISTENTLY IN FLIGHT WITH EMER LIGHT SWITCH IN ARMED POSITION CORRECTIVE ACTION: REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY P - [SDR DXTR2025102901](https://openairdocs.org/sdr/DXTR2025102901), Oct 29, 2025: WIRE HARNESS. FAULTED. DURING APPROACH WHILE HANDFLYING, THERE HAD TO BE SIGNIFICANT INPUT IN AILERON TO MAINTAIN LEVEL FLIGHT. FUEL INDICATIONS OF BOTH FUEL FLOW, QUANTITY, AND BALAN - [SDR DXTA2025100205139](https://openairdocs.org/sdr/DXTA2025100205139), Sep 29, 2025: WIRE HARNESS. DAMAGED. DURING APPROACH WHILE HANDFLYING, THERE HAD TO BE SIGNIFICANT INPUT IN AILERON TO MAINTAIN LEVEL FLIGHT. FUEL INDICATIONS OF BOTH FUEL FLOW, QUANTITY, AND BALAN - [SDR DXTA2025092905114](https://openairdocs.org/sdr/DXTA2025092905114), Sep 27, 2025: ACTUATOR. FAULTY. REPEAT WRITE UP, DURING CLIMB, CRUISE, AND DESCENT THERE WERE FUEL IMBALANCES. WE HAD TO CROSSFESD MULTIPLE TIMES TO EQUALIZE THE WEIGHT. DURING CLIMB AND CRUIS - [SDR DXTA2024110701042](https://openairdocs.org/sdr/DXTA2024110701042), Nov 3, 2024: TRANSDUCER. DEFECTIVE. BRK FAIL YELLOW CAS: ON CLIMB OUT OUT OF MSY WE GOT A BRK FAIL CAS THAT NEVER EXTIGUISHED. WE DIVERTED TO KIND, FOLLOWED QRH PROCEDURES AND LANDED WITH EMERGENC - [SDR DXTA2023080292120](https://openairdocs.org/sdr/DXTA2023080292120), Aug 2, 2023: UNKNOWN. UNKNOWN. ELEVATOR CONTROL/TRIM: ON ON FLIGHT CONTROL CHECK, CONTROLS FELT FINE. BUT WHEN YOKE IS HELD FULL AFT AND RELEASED, IT STAYS FULL BACK. REMOVED AND REPLACED ELE - [SDR DXTA2023060788060](https://openairdocs.org/sdr/DXTA2023060788060), Jun 6, 2023: UNKNOWN. UNKNOWN. FLOOR EMERG EXIT LIGHT: FLOOR EMERGENCY LIGHT IS LOOSE AND EXTENDED INTO THE MIDDLE OF THE AISLE. RESECURED FLOOR EMERGENCY LIGHT AS REQUIRED OPS CHECK GOOD AT - [SDR DXTA2022092370990](https://openairdocs.org/sdr/DXTA2022092370990), Sep 23, 2022: LIGHT. MISSING. FLOOR EMERG EXIT LIGHT: TWO FLOOR/ AISLE LIGHTS MISSING. THE HOLES WHERE THE LIGHTS SHOULD BE ARE IN PLACE BUT THEY HAD FORGOTTEN TO PUT IN THE LIGHTS AFTER REF - [SDR DXTA2022081668170](https://openairdocs.org/sdr/DXTA2022081668170), Aug 16, 2022: PLUG. DETACHED. EMERG EXIT SIGN/LIGHT: EXIT SIGN LIGHT ABOVE WINDOW EXIT INOPERATIVE.//CORRECITVE ACTION//FOUND LIGHT PLUG OUT 180 DEGRE RESET PLUG OPS CHECK GOOD. REF EMB505 W - [SDR DXTA2022010354590](https://openairdocs.org/sdr/DXTA2022010354590), Dec 31, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS STARTED FLASHING DURING FLIGHT. AFTER RESETTING EMER LIGHT SWITCH IN COCKPIT, EMERGENCY LIGHTS REMAINED ILLUMINATED FOR THE - [SDR DXTA2021101950540](https://openairdocs.org/sdr/DXTA2021101950540), Oct 18, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS BLINKING CONSTANTLY IN FLIGHT. // SIGNOFF// REMOVED AND REPLACED FWD EMER BATTERY AND PERFORMED OPS CHECK. EMERGENCY LIGHTS - [SDR DXTA202101314659](https://openairdocs.org/sdr/DXTA202101314659), Jan 31, 2021: PIN. STIFF. UPON LANDING WE WERE UNABLE TO OPEN MAIN CABIN DOOR. THE MECHANICS WERE ABLE TO OPEN FROM THE OUTSIDE. DOOR APPEARED TO HAVE BEEN FROZEN IN PLACE. CORRECTIVE AC - [SDR DXTA2021013104659](https://openairdocs.org/sdr/DXTA2021013104659), Jan 29, 2021: PIN. STIFF. UPON LANDING WE WERE UNABLE TO OPEN MAIN CABIN DOOR. THE MECHANICS WERE ABLE TO OPEN FROM THE OUTSIDE. DOOR APPEARED TO HAVE BEEN FROZEN IN PLACE. CORRECTIVE AC - [SDR DXTA202101310465](https://openairdocs.org/sdr/DXTA202101310465), Jan 29, 2021: DOOR. MALFUNCTIONED. UPON LANDING WE WERE UNABLE TO OPEN MAIN CABIN DOOR. THE MECHANICS WERE ABLE TO OPEN FROM THE OUTSIDE. DOOR APPEARED TO HAVE BEEN FROZEN IN PLACE. CORRECTIVE AC - [SDR DXTA2020091094077](https://openairdocs.org/sdr/DXTA2020091094077), Sep 9, 2020: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH WITH LANDING GEAR EXTENDED AND FLAPS 2, APPROX 145 KIAS SELECTED FLAPS FULL AND SOON AFTER FLAPS FAIL YELLOW CAS ILLUMINATED. RAN QRC TO INCLUDE CYC - [SDR EBVR20191215001](https://openairdocs.org/sdr/EBVR20191215001), Dec 15, 2019: BALANCE WEIGHT. CORRODED. COMPLYING WITH SB505-55-004R3 FOUND CORROSION ON 7 EACH L/H ELEVATOR 9 EACH ON R/H ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS P/N PE915109-L33 AND 1 EACH R/H ELEV - [SDR DXTA2019080502704](https://openairdocs.org/sdr/DXTA2019080502704), Aug 2, 2019: SWITCH. OUT OF ADJUST. AT 40K FEET GOT A YELLOW CAS DOORBAG LH OPEN. INSPECTED DOOR AFTER LANDING AND IT WAS CLOSED AND LOCKED. PERFORMED FORWARD BAGGAGE DOOR MICOSWITCH ADJUSTMENT IA - [SDR DXTA2019062802551](https://openairdocs.org/sdr/DXTA2019062802551), Jun 28, 2019: ECU. MALFUNCTIONED. FLAP FAIL YELLOW CAS ILLUMINATED - WHILE PASSING THROUGH FL230 THE YELLOW "FLAPS FAIL" CAS CAME ON ALONG WITH THE LOSS OF THE AUTO PILOT, AND CAS MESSAGES "SWPS - [SDR DXTA2018010800456](https://openairdocs.org/sdr/DXTA2018010800456), Jan 8, 2018: ANTI-ICE SYSTEM. MALFUNCTIONED. DURING CLIMB OUT THROUGH 7000 FEET, WITH BOTH ENGINE ANTI-ICE AND WING STAB ANTI-ICE SWITCHES ON, THE NR 2 BLEED FAIL AMBER CAS MESSAGE ILLUMINATED. AN ODOR SIM - [SDR DXTA2015101906109](https://openairdocs.org/sdr/DXTA2015101906109), Oct 18, 2015: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB OUT, PASSING 26,000 FT, ECS 1 VALVE FAIL CAS MESSAGE DISPLAYED. NOTICED A GREASE ODOR IN THE COCKPIT. PERFORMED MX RUNS OF BOTH NR 1 & 2 ENGINES AT - [SDR DXTA2015013005973](https://openairdocs.org/sdr/DXTA2015013005973), Jan 29, 2015: DISPLAY. MALFUNCTIONED. CENTER MFD BEGAN TO SWITCH BACK & FORTH BETWEEN DIFFERENT MODES NUMEROUS TIMES. ELEC SMOKE WAS THEN SMELLED & SEEN ON RT SIDE UNDER INSTRUMENT PANEL. REMOVED AN - [SDR DXTA2014122905955](https://openairdocs.org/sdr/DXTA2014122905955), Dec 28, 2014: FAN. FAILED. AIRCRAFT POWERED WITH GPU RECEIVED A BATTERY EXCEEDENCE CAS MESSAGE. LIGHTS FLICKERED IN CABIN & A BURNING ODOR WAS NOTICED. IMMEDIATELY REMOVED POWER FROM ACFT - [SDR DXTA2014042105736](https://openairdocs.org/sdr/DXTA2014042105736), Apr 15, 2014: ANTENNA. FAILED. DURING FLIGHT AT FL350, BOTH COMMS 1 & 2 DEVELOPED LOUD STATIC. COMMUNICATION WITH ATC WAS LOST. NEITHER COMMS 1 OR 2 COULD TRANSMIT OR RECEIVE, INTERCOM WAS OK ## Service difficulty reports on N327QS not matched to an aircraft (9) They name N327QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2010101804265](https://openairdocs.org/sdr/DXTA2010101804265), Oct 17, 2010: UPLOCK SWITCH. INOPERATIVE. ENROUTE TO KERI AFTER REACHING CRUISE SPEED NOSE GEAR UNSAFE LIGHT ILLUMINATED SEVERAL TIMES AND HYD SYS ACTIVATED. HYD SYS RESSURIZED EMERGENCY CHECKLIST" J5" - [SDR DXTA2010101204261](https://openairdocs.org/sdr/DXTA2010101204261), Oct 9, 2010: BRAKE ASSY. FAILED. DURING LANDING ROLLOUT, WHEN BRAKES APPLIED EVENLY, AIRPLANE PULLED HARD TO LEFT THEN TO RIGHT. BRAKE PEDALS FELT NORMAL. REPLACED LT BRAKE ASSY IAW MM 33-42-01 - [SDR CWQR200907](https://openairdocs.org/sdr/CWQR200907), Oct 13, 2009: FITTING. DAMAGED. DURING A PHASE 50 INSPECTION, OUR NDI VENDOR , PARAGON SERVICES INC., DETECTED A FLAW ON THE LEFT WING LOWER FORWARD SPAR FITTING ASSEMBLY.THIS WING ATTACH FITT - [SDR DXTA200803108](https://openairdocs.org/sdr/DXTA200803108), Jun 8, 2008: UNKNOWN. ODOR. BURNING ODOR IN CABIN. REMOVED GNS-XL FMS CDU. INSTALLED CUSTOMER SUPPLIED (REPAIRED) UNIT. SYS OPS CK GOOD IAW GNS-XL FMS INSTALLATION MANUAL. - [SDR DXTA200803098](https://openairdocs.org/sdr/DXTA200803098), Jun 5, 2008: BRAKE SYS. MALFUNCTIONED. BRAKE APPLICATION FROM THE CO-PILOT`S SEAT ARE SLUGGISH, BRAKES FEEL SOFT. BLED BRAKES IAW MM 32-42-00 AND BRAKE BLEEDING PROCEDURE MEMO M344-08-10OPS CHECK GOO - [SDR DXTA200702580](https://openairdocs.org/sdr/DXTA200702580), Oct 28, 2007: FLOW DIVIDER. MALFUNCTIONED. DURING SPEED BRAKE CHECK THE LT ENGINE SHUTDOWN. REMOVED AND REPLACED FLOW DIVIDER PERFORMED OPS CK AND LEAK CHECK NO DEFECTS FOUND OPS CHECK SPEED BRAKE SYSTEM - [SDR DXTA200601449](https://openairdocs.org/sdr/DXTA200601449), Jun 21, 2006: UPLOCK. LACK OF LUBE. AFTER TAKEOFF WHEN GEAR LEVER WAS SELECTED UP THE RED GEAR UNLOCKED REMAINED ILLUMINATED AND THE HYDRAULIC LIGHT ALSO REMAINED ILLUMINATED. PERFORMED A FUNCTION - [SDR DXTA200501146](https://openairdocs.org/sdr/DXTA200501146), Dec 15, 2005: ACTUATOR. INOPERATIVE. RIGHT GREEN LANDING GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR EXTENDED. GEAR APPEARED DOWN VISUALLY. ALSO ROTARY TEST, GEAR HORN TEST INDICATED FAULTY LIGHT. HOWE - [SDR 96ZZZX6170](https://openairdocs.org/sdr/96ZZZX6170), Dec 3, 1996: SKIN. CRACKED. LT SIDE OF BOTTOM L/E SKIN HAS A CRACK ALONG THE RIVET LINE THAT IS 2.25 INCHES LONG. THIS IS THE 7TH OCCURRENCE OF THIS PROBLEM. ## 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.