# N344QS: 2014 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: 50500219 - Year built: 2014 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: September 9, 2014 - Certificate issued: June 2, 2026 - Expires: June 30, 2033 - Mode S code: A3CD99 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=344QS - Page: https://openairdocs.org/aircraft/N344QS 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 N344QS. ## FAA accident and incident reports None matched to N344QS. ## Service difficulty reports (10) 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 DXTA2026082709432](https://openairdocs.org/sdr/DXTA2026082709432), Aug 25, 2026: PRESSURE SWITCH. FAULTY. ON ARRIVAL, FUEL 1 FEED FAULT CAS MESSAGE DISPLAYED, STAYED ON DURATION OF FLIGHT. DID NOT HAVE TIME TO CONTACT FODM IN FLIGHT. GAINED ACCESS TO FUEL FEED 1 PRE - [SDR DXTA2026011906568](https://openairdocs.org/sdr/DXTA2026011906568), Jan 16, 2026: BATTERY PACK. DEFECTIVE. WHILE ENROUTE THE CABIN EMERGENCY LIGHTING CAME ON AND BEGAN TO FLASH. REMOVED AND REPLACED THE NR 1 AND 2 EMERGENCY BATTIERIES IAW AMM 33-52-01, OPS CHKD GOOD. - [SDR DXTA2025061903943](https://openairdocs.org/sdr/DXTA2025061903943), Jun 18, 2025: BATTERY. FAULTED. DURING FLIGHT WE NOTICED THE EMER LIGHTS WERE ILLUMINATED, THE SWITCH WAS IN THE ARM NOT ON POSITION. REPLACED EMERGENCY BATTERY. PERFORMED CHARGE AND OPS CHECK - [SDR DXTA2024090300409](https://openairdocs.org/sdr/DXTA2024090300409), Sep 2, 2024: LIGHT. DISLODGED. FLOOR EMERG EXIT LIGHT: ON CABIN CLEAN UP/POST FLIGHT DISCOVERED FLOOR EMER LIGHT DISLODGED AND LOOSE IN THE FLOOR TRENCH CORRECTIVE ACTION: REINSTALLED R/H FLO - [SDR DXTA2023122610417](https://openairdocs.org/sdr/DXTA2023122610417), Dec 23, 2023: BATTERY. FAILED. THE EMER LIGHTS INSIDE THE CABIN STARTING FLASHING DURING OUR DESCENT. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY LIGHTS BATTERIES IAW AMM 33-52-01. OPERATI - [SDR DXTA2022061663990](https://openairdocs.org/sdr/DXTA2022061663990), Jun 16, 2022: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: AIRCRAFT EMERGENCY LIGHTS ILLUMINATE IN THE SWITCH ARM POSITION.//CORRECTIVE ACTION// CONFIRMED WITH SWITCH IN ARM POSITION EMERGENCY LIGHTS - [SDR DXTA2021122754060](https://openairdocs.org/sdr/DXTA2021122754060), Dec 23, 2021: NONE. DEFECTIVE. FUSELAGE STRUCTURE: REPEAT WRITE-UP . LOUD HOWLING WITH VIBRATION FELT UNDER COCKPIT AREA . STARTED DURING CLIMBOUT THRU 2000 FEET AND STOPPED ONCE IN LEVEL CRU - [SDR DXTA2021062844310](https://openairdocs.org/sdr/DXTA2021062844310), Jun 26, 2021: UNKNOWN. ODOR. COCKPIT ODOR: REPEAT WRITE UP. STRONG MOLDY, MILDEW ODOR IN COCKPIT PERMEATING THROUGH CABIN. COCKPIT FAN HAS UNUSUAL NOISE WHEN SELECTED TO HIGH MODE. WHEN PER - [SDR DXTA2017012806364](https://openairdocs.org/sdr/DXTA2017012806364), Jan 28, 2017: BRAKE. FIRE. UPON ARRIVAL ON THE RAMP, PERSONNEL CAME RUNNING OUT WITH FIRE EXTINGUISHERS , SAID LEFT BRAKE ASSEMBLY WAS ON FIRE. IT WAS OUT BY THE TIME WE EXITED, BUT THERE - [SDR DXTA2016060306248](https://openairdocs.org/sdr/DXTA2016060306248), Jun 3, 2016: RADIO. ODOR. AT APPROX 3000 DESCENDING, SMELLED ELEC BURNING. THE ODOR CONTINUED WITH NOW A HAZY SMOKE VIEW. THE NR 1 COMM WENT YELLOW X, SWITCHED TO COMM 2. MADE ALL RADIO ## Service difficulty reports on N344QS not matched to an aircraft (15) They name N344QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200811193364](https://openairdocs.org/sdr/DXTA200811193364), Nov 19, 2008: WIRE. DAMAGED. LT GEAR INDICATION LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE RED GEAR UNSAFE LIGHT NEVER ILLUMINATED AND THERE WAS NO GEAR WARNING HORN. CREW DID A M - [SDR DXTA2008111903364](https://openairdocs.org/sdr/DXTA2008111903364), Nov 19, 2008: LIGHT. MALFUNCTIONED. LT GEAR INDICATION LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. - [SDR DXTA200702435](https://openairdocs.org/sdr/DXTA200702435), Aug 29, 2007: THROTTLE CABLE. BINDING. DURING SPEEDBRAKE TEST, LT ENGINE POWER LEVER WAS ADVANCED AND BROUGHT TO IDLE STOP. LT ENGINE FLAMEOUT. LT ENGINE WOULD NOT RESTART. LARGE PUDDLE OF FUEL FORME - [SDR DXTA200702009](https://openairdocs.org/sdr/DXTA200702009), Mar 9, 2007: BRAKE ASSY. MALFUNCTIONED. LITTLE OR NO BRAKE PRESSURE ON RT SIDE (FO SEAT). NO LEAKING FLUID NOTED. BLED SYSTEM SEVERAL TIMES AND REMOVED ALL AIR IN THE SYSTEM IAW MM, CH 32-42-00. - [SDR DXTA200601575](https://openairdocs.org/sdr/DXTA200601575), Aug 24, 2006: GROUND WIRE. BROKEN. GEAR UNSAFE INDICATION WITH GEAR HANDLE DOWN ONLY NOSE PLUS LEFT MAIN INDICATE DOWN AND LOCKED. NO OTHER UNSAFE WARNINGS. BLEW GEAR DOWN AND OBTAINED SAFE LANDI - [SDR DXTA200601535](https://openairdocs.org/sdr/DXTA200601535), Aug 5, 2006: ACM. OVERSERVICED. DURING T/O HEAVY AROMA OF BURNING MINERAL TYPE OIL SUSPECT ACM BEARINGS SMELL DISSIPATES 20 MINUTES AFTER T/O. INSPECTED ACM FOR OIL & AIR LEAKS FOUND NO LEAKS - [SDR DXTA200601340](https://openairdocs.org/sdr/DXTA200601340), Apr 10, 2006: WIRE. BROKEN. R MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION, GEAR BLOWN DOWN. LIGHT DID ILLUMINATE SEVERAL MINUTES AFTER "BLOWDOWN". FOUND BROKEN WIRE IN RIGHT - [SDR DXTA200501125](https://openairdocs.org/sdr/DXTA200501125), Dec 1, 2005: POSITION SWITCH. OUT OF ADJUST. LEFT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON LOWERING THE GEAR. DID CHECKS AND EMER EXTENSION DID FLICKER BRIEFLY BUT WENT OUT. SHOWED NO RED LI - [SDR DXTA200500854](https://openairdocs.org/sdr/DXTA200500854), Jul 23, 2005: ENGINE. POWER LOSS. DURING POWER UP FOR TAKEOFF RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER. PUSHED RIGHT POWER LEVER TO STOP ONLY GOT 96.0 PERCENT N1, NEEDED 96.7 PERCENT N1 FOR TAK - [SDR DXTA200500812](https://openairdocs.org/sdr/DXTA200500812), Jun 30, 2005: WIRE. BROKEN. STICK SHAKER INOP DURING ROTARY TEST. A LIGHT TAP ON THE YOKE CAUSED A SPARK AND A SMALL PUFF OF SMOKE. AOA CIRCUIT BREAKER POPPED. FOUND WIRE BROKEN ON CONNECT - [SDR DXTA200300202](https://openairdocs.org/sdr/DXTA200300202), Dec 15, 2003: BRAKE. MALFUNCTIONED. ON LANDING, PILOT’S FELT BRAKES WERE HARD WITH LITTLE OR NO BRAKING, TRANSFERRED BRAKES TO CO-PILOT, HAD HARD BRAKES THEN THE BRAKES STARTED TO WORK ON THE ROLL - [SDR DXTA200300096](https://openairdocs.org/sdr/DXTA200300096), Aug 19, 2003: SWITCH. MALFUNCTIONED. RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED BELOW 70K ON TAKEOFF ROLL. TAKEOFF ABORTED W/O INCIDENT, T/R DID NOT DEPLOY, LIGHT WOULD NOT CLEAR BY PUSHING T/R PA - [SDR 99ZZZX8](https://openairdocs.org/sdr/99ZZZX8), Jun 25, 1998: WIRE. CHAFED. LEFT ENGINE THRUST REVERSER CIRCUIT BREAKER TRIPPED IN-FLIGHT. TROUBLESHOT AND DETERMINED THAT WIRE RELATED TO THAT SYSTEM WAS CHAFING ON THE OIL RPESSURE INDIC - [SDR 97ZZZX1033](https://openairdocs.org/sdr/97ZZZX1033), Feb 25, 1997: AILERON. CHAFING. AFTER A CONTINUOUS INSPECTION PHASE 1-5 WAS C/W, THE AIRCRAFT WAS RELEASED FOR A MAINTENANCE CHECK FLIGHT. A POST-FLIGHT SQUAWK WAS WRITTEN 'ON TEST FLIGHT, AIL - [SDR 96ZZZX6179](https://openairdocs.org/sdr/96ZZZX6179), Oct 28, 1996: RUDDER SKIN. CRACKED. A LT RUDDER SKIN CRACK. HORIZONTAL, ABOUT 2 INCHES LONG, AND ALONG THE RIB LINE OF THE RUDDER RIB BELOW THE TRIM TAB. ## 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.