# N306FL: 2010 Embraer-Empresa Brasileira De EMB-505 - Status: Valid registration - Airframe: [Embraer-Empresa Brasileira De EMB-505](https://openairdocs.org/model/embraer-empresa-brasileira-de-emb-505) (registry code 3260407, 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: 50500030 - Year built: 2010 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: February 24, 2011 - Certificate issued: July 14, 2011 - Expires: July 31, 2027 - Mode S code: A33624 - Registered owner: [Rains Ronald D](https://openairdocs.org/faa-owner/RAINS%20RONALD%20D) - Location: [Odessa, TX](https://openairdocs.org/faa-place/TX/Odessa) - Owner type: Individual - Owner's area on the map: 31.9251° N, 102.3577° W: Placed by OpenAirDocs at the center of ZIP code 79762, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=306FL - Page: https://openairdocs.org/aircraft/N306FL 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-Empresa Brasileira De 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 N306FL. ## FAA accident and incident reports None matched to N306FL. ## Service difficulty reports (1) 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 DJFA2011026](https://openairdocs.org/sdr/DJFA2011026), Jun 6, 2011: INLET. CRACKED. DURING INSP OF RT ENGINE INLET, CRACKS, SCRATCHES, AND MISSING RIVETS WERE FOUND ON BOTH ENGINE INLETS. THE AIRCRAFT MANUFACTURER HAS DETERMINED THAT THE DAMAGE ## Service difficulty reports on N306FL not matched to an aircraft (24) They name N306FL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR F3LA200500011](https://openairdocs.org/sdr/F3LA200500011), Mar 8, 2005: ROLLER. WORN. MAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE P - [SDR F3LA200300191](https://openairdocs.org/sdr/F3LA200300191), Dec 31, 2003: ACTUATOR. INOPERATIVE. DURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOC - [SDR F3LA200300190](https://openairdocs.org/sdr/F3LA200300190), Dec 31, 2003: SKIN. DENTED. DURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202. - [SDR F3LA200300188](https://openairdocs.org/sdr/F3LA200300188), Dec 19, 2003: FLAP TRACK. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRA - [SDR F3LA200300187](https://openairdocs.org/sdr/F3LA200300187), Dec 19, 2003: BATTERY PACK. FAILED. DURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE. - [SDR F3LA200300186](https://openairdocs.org/sdr/F3LA200300186), Dec 19, 2003: INTERCOSTAL. CRACKED. DURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOST - [SDR F3LA200300185](https://openairdocs.org/sdr/F3LA200300185), Dec 19, 2003: OXYGEN BOTTLE. DISCHARGED. DURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-2 - [SDR F3LA200300184](https://openairdocs.org/sdr/F3LA200300184), Dec 19, 2003: MODULE. FAULTY. DURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G - [SDR F3LA200300183](https://openairdocs.org/sdr/F3LA200300183), Dec 19, 2003: FRAME. CRACKED. DURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1- - [SDR F3LA200300182](https://openairdocs.org/sdr/F3LA200300182), Dec 19, 2003: SHEAR TIE. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07. - [SDR F3LA200300181](https://openairdocs.org/sdr/F3LA200300181), Dec 19, 2003: SHEAR TIE. CORRODED. DURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07. - [SDR F3LA200200394](https://openairdocs.org/sdr/F3LA200200394), Dec 5, 2002: STRAP. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FILLER/STRAP PER SRM 51-40-02 AND 51-10-02. - [SDR F3LA200200393](https://openairdocs.org/sdr/F3LA200200393), Dec 5, 2002: STRAP. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED SILL STRAP PER SRM 51-40-07 AND 51-10-02. - [SDR F3LA200200392](https://openairdocs.org/sdr/F3LA200200392), Dec 5, 2002: WEB. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40 - [SDR F3LA200200391](https://openairdocs.org/sdr/F3LA200200391), Dec 3, 2002: ANGLE. CORRODED. DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIRED ANGLE PER SRM 51-40-02, 51-40-05 AND 5 - [SDR F3LA200200396](https://openairdocs.org/sdr/F3LA200200396), Dec 3, 2002: SUPPORT ANGLE. GOUGED. DURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 5 - [SDR F3LA200200395](https://openairdocs.org/sdr/F3LA200200395), Dec 3, 2002: COWL DOOR. CHAFED. DURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITIONAL DAMAGE FOUND AT EDGE OF PREVIOUS REPAI - [SDR F3LA200200250](https://openairdocs.org/sdr/F3LA200200250), Aug 21, 2002: SHUTOFF VALVE. FAILED. AIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, - [SDR F3LA200100123](https://openairdocs.org/sdr/F3LA200100123), Nov 25, 2001: WIRE. BROKEN. PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER STANDARD PRACTICES 20-30-12, PERFORMED OPER - [SDR F3LA200000277](https://openairdocs.org/sdr/F3LA200000277), Dec 28, 2000: FITTING. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND RT. AFT LAVATORY OTBD AFT FLOOR MOUNT. MAINTENANCE FABRICATED AND REPLACED NEW FITTING PER EA 25-737-108. - [SDR F3LA99050](https://openairdocs.org/sdr/F3LA99050), May 19, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X) - [SDR F3LA99049](https://openairdocs.org/sdr/F3LA99049), May 19, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,660. (X) - [SDR F3LA99048](https://openairdocs.org/sdr/F3LA99048), May 19, 1999: BATTERY. DISCHARGED. DEN - DURING C-CHECK INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X) - [SDR F3LA97145](https://openairdocs.org/sdr/F3LA97145), Sep 13, 1997: WIRE. LOOSE. DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED WIRES DISCONNECTED FROM FLOOR PROXIMITY LIGHTING AT ROW 13. MAINTENANCE RECONNECTED WIRES AND SYSTEM CHECKED OK ## 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-Empresa Brasileira De 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-Empresa Brasileira De EMB-505 aircraft: https://openairdocs.org/model/embraer-empresa-brasileira-de-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.