# N366QS: 2015 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: 50500268 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: April 30, 2015 - Certificate issued: March 30, 2026 - Expires: March 31, 2033 - Mode S code: A42405 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=366QS - Page: https://openairdocs.org/aircraft/N366QS 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 N366QS. ## FAA accident and incident reports None matched to N366QS. ## Service difficulty reports (13) 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 DXTA2025030502561](https://openairdocs.org/sdr/DXTA2025030502561), Mar 2, 2025: CONCENTRATOR. DEFECTIVE. CENTRAL WARNING SYSTEMS: AT 40,000 RECEIVED GOLDEN CASS MESSAGE GSD1 FAIL WITH MANY OTHER CASS MESSAGES. ALSO, RECEIVED A DATA PATH HAS FAILED IN THE GTC. LASTL - [SDR DXTA2025011501943](https://openairdocs.org/sdr/DXTA2025011501943), Jan 12, 2025: LIGHT. MALFUNCTIONED. CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT WITH THE EMER LT SWITCH IN ARM. THE LIGHTS STOPPED FLASHING WHEN WE TURNED THE SWITCH OFF. REPLACED BATTERY. OPS CHECK - [SDR DXTA2024090500416](https://openairdocs.org/sdr/DXTA2024090500416), Sep 2, 2024: SHIMMY DAMPENER. DEFECTIVE. RIGHT SEAT, RIGHT RUDDER PEDAL REQUIRES EXCESSIVE PRESSURE FOR A NORMAL CONTROL RESPONSE. MORE THAN NORMAL PRESSURE IS REQUIRED AT TAXI SPEEDS, EXCESSIVE PRESSU - [SDR DXTA2024081500198](https://openairdocs.org/sdr/DXTA2024081500198), Aug 12, 2024: BATTERY PACK. MALFUNCTIONED. EMERGENCY LIGHTS IN CABIN WERE FLICKERING WHILE TAXIING INTO FBO RAMP. AFTER SHUTDOWN, WE MOVED THE EMERGENCY-LIGHTS SWITCH TO ARM AND ALSO ON POSITIONS AND THE - [SDR DXTA2024022210976](https://openairdocs.org/sdr/DXTA2024022210976), Feb 20, 2024: INDICATOR. FOD. ON POSTFLIGHT, DISCOVERED THE LOWER RIGHT MAIN CABIN DOOR LOCK INDICATOR GREEN FLAG IS NO LONGER VISIBLE THROUGH THE LOCK VISOR. THERE IS A SILVER BLANKET/TAPE - [SDR DXTA2023071891210](https://openairdocs.org/sdr/DXTA2023071891210), Jul 17, 2023: UNKNOWN. DEFECTIVE. COMM 1 FAILED WITH VERY DISTINCTIVE ELECTRICAL ODOR IN FLIGHT. EVERY TIME YOU PUSHED TO TALK A YELLOW X WOULD APPEAR OVER COMM 1 IN BOTH GTCS ALONG WITH ELECTRI - [SDR DXTA2023051085770](https://openairdocs.org/sdr/DXTA2023051085770), May 9, 2023: UNKNOWN. UNKNOWN. EMERG EXIT SIGN/LIGHT: EMERGENCY "EXIT" SIGN OVER MAIN CABIN DOOR (ON CEILING). THE LEFT HALF OF THE LIGHT CLUSTER IS NOT WORKING (LOOKING FROM BOTTOM OF STAIRS - [SDR DXTA2022112874910](https://openairdocs.org/sdr/DXTA2022112874910), Nov 26, 2022: BATTERY PACK. FAILED. DURING FLIGHT CABIN EMERGENCY LIGHTS STARTED FLICKERING AND CONTINUED TO DESTINATION. THEY GOT MUCH DIMMER BY THE TIME OF LANDING. C/W FIM 488S-33-50-00-8 I 0-8 - [SDR DXTA2022102472670](https://openairdocs.org/sdr/DXTA2022102472670), Oct 23, 2022: BATTERY PACK. DISCONNECTED. EMERGENCY LIGHTS REMAIN ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE ARM POSITION. ACCESS FWD AND AFT EMERGENCY BATTERIES FOR TROUBLESHOOTING. NOTED WITH THE - [SDR DXTA2021061043460](https://openairdocs.org/sdr/DXTA2021061043460), Jun 9, 2021: UNKNOWN. NOISE. EMERGENCY EXIT DOORS: LOUD HUMMING NOISE HEARD IN THE CABIN DURING CRUISE FLIGHT AT FL290. THE NOISE STARTED AROUND 270K AND WAS CONSTANT AT SPEEDS ABOVE THAT. - [SDR 2020FA0000376](https://openairdocs.org/sdr/2020FA0000376), Aug 16, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING LEFT ELEVATOR MASS BALANCE WEIGHT BELOW TOLERANCE: P/N PE91510 - [SDR DXTA2019021802035](https://openairdocs.org/sdr/DXTA2019021802035), Feb 16, 2019: UPLOCK. CONTAMINATED. LOUD BANG WHEN SELECTED DOWN AND 8-10 SECONDS FOR GREEN INDICATION. BLED THE AIR FROM THE LANDING GEAR UPLOCK BOXES. CHECKED & ADJUSTED HYDRAULIC ACCUMULATOR NI - [SDR DXTAT2PL6D005FW9U](https://openairdocs.org/sdr/DXTAT2PL6D005FW9U), Oct 18, 2017: UNKNOWN. ODOR. DURING CRUISE FLIGHT, A STRONG ODOR WAS PRESENT PRIMARILY IN THE COCKPIT. THE ODOR IS MOST NOTICEABLE WHEN THE AIR SYSTEM IS CALLING FOR AN INCREASE IN TEMPERAT ## Service difficulty reports on N366QS not matched to an aircraft (12) They name N366QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2010030104008](https://openairdocs.org/sdr/DXTA2010030104008), Feb 26, 2010: BRAKE. WEAK. BOTH CO-PILOTS SIDE BRAKES ARE SOFT. INSPECTED COPILOTS PANELS ATTACHING POINTS, MASTER CYLINDERS, LINES AND FITTINGS NO DEFECTS NOTED AT THIS TIME BLED BRAKES - [SDR DXTA09F00143](https://openairdocs.org/sdr/DXTA09F00143), Dec 17, 2009: INDICATOR. FAILED. DURING CLIMBOUT AT APPROX 16,000' LT OIL TEMP GAUGE DROPPED TO ZERO ANDS THEN RETURNED TO NORMAL NUMEROUS TIMES. AFTER LEVELING AT 23,000' THE GAUGE DROPPED TO - [SDR DXTA2009113003871](https://openairdocs.org/sdr/DXTA2009113003871), Nov 28, 2009: SWITCH. MALFUNCTIONED. ON TAKEOFF ROLL, PWR APPROX 80-90 PERCENT, LT THRUST REVERSER ARM AND UNLOCK LIGHT CAME ON. AS WE TAXIED IN, FULL T/R DEPLOYMENT ON LT SIDE; EMER SWITCH STOWED - [SDR DXTA2008110303330](https://openairdocs.org/sdr/DXTA2008110303330), Oct 31, 2008: SLEEVE. DISLODGED. AT FL340 LOST PSI'T AT 2000 FPM TO MAX CAB ALT OF 12000. EMERGENCY ACTION TAKEN. TROUBLESHOT AND FOUND BYPASS DUCT SLEEVE BLOWNOFF OF CONDITIONED AIR DUCT IN TA - [SDR DXTA200702647](https://openairdocs.org/sdr/DXTA200702647), Dec 3, 2007: INDICATOR. OUT OF ADJUST. DURING TAKEOFF, AIRCRAFT REQUIRED SIGNIFICANT FOWARD PRESSURE DURING CLIMBOUT. ALL OTHER INDICATIONS WERE NORMAL EXCEPT NOSE TRIM WHEEL INDICATOR WAS BEYOND THE - [SDR DXTA200601308](https://openairdocs.org/sdr/DXTA200601308), Mar 20, 2006: SWITCH. FAULTY. ON FINAL APPROACH WITH LANDING GEAR DOWN AND LOCKED LOW PRESSURE POWER BRAKE AND ANTI-SKID LIGHTS ILLUMINATED. NORMAL LANDING WITH NO PRESSURE ON BRAKE PEDALS. - [SDR DXTA200501016](https://openairdocs.org/sdr/DXTA200501016), Oct 11, 2005: BRAKE ASSY. WEAK. ON TAXI OUT BRAKES FELT SOFT. BLED BRAKES PER CESSNA 560 ULTRA MM 32-42-00. BRAKES FUNCTION NORMALLY AT THIS TIME. - [SDR DXTA200500770](https://openairdocs.org/sdr/DXTA200500770), Jun 12, 2005: BRAKE. DAMAGED. CO-PILOTS LEFT PEDAL GOES TO THE FLOOR BEFORE ANY PRESSURE CAN BE BUILT UP. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200500586](https://openairdocs.org/sdr/DXTA200500586), Feb 11, 2005: HOSE. LEAKING. POWER BRAKE SYSTEM FAILURE ON TAXI. POWER BRAKE LOW PRESS AND ANTISKID INOP LIGHTS ON. NO BRAKE PRESSURE. TROUBLESHOT SYSTEM AND FOUND RT MAIN GEAR BRAKE LINE ( - [SDR DXTA200400493](https://openairdocs.org/sdr/DXTA200400493), Dec 23, 2004: PITCH CONTROL. FROZEN. DESCENDING THROUGH 18,000 FT, RECEIVED A PITCH MIS TRIM ANNUNCIATOR. ATTEMPTED TO HELP THE AUTOPILOT BY TRYING TO TRIM THE NOSE UP. DISCOVERED THAT THE PITCH WH - [SDR DXTA200400270](https://openairdocs.org/sdr/DXTA200400270), Mar 18, 2004: WARNING LIGHT. FALSE ACTIVATION. UPON GEAR RETRACTION THE GEAR UNLOCKED LIGHT WOULD NOT EXTINGUISH, GEAR EXTENDED NORMALLY ON RECYCLE WITH 3 GREEN LIGHTS, ACCOMPLISHED AIR TURN BACK TO TEB. PER - [SDR DXTA200300023](https://openairdocs.org/sdr/DXTA200300023), Apr 30, 2003: BULB. BURNED OUT. UNSAFE INDICATION ON LEFT MAIN GEAR, BLEW GEAR DOWN. FOUND BOTH LIGHT BULBS ON MLG PANLE BURNED OUT, REPLACED BULBS. ## 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.