# N407QS: 2017 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: 50500405
- Year built: 2017
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: April 26, 2017
- Certificate issued: March 13, 2023
- Expires: March 31, 2030
- Mode S code: A4C811
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=407QS
- Page: https://openairdocs.org/aircraft/N407QS

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 N407QS.

## FAA accident and incident reports

None matched to N407QS.

## Reports on N407QS not matched to an aircraft (1)

They name N407QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20010105000299I](https://openairdocs.org/incident/20010105000299I), Jan 5, 2001: Gulstm GIV (N407QS), Pittsburgh, PA. (-23) On 01/05/01, a gl-iv-iv, registered as N407QS, was reported to have had a total electrical failure, and landed at Pittsburgh airport on runway 28L.…

## Service difficulty reports (23)

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 DXTA2026092909885](https://openairdocs.org/sdr/DXTA2026092909885), Sep 25, 2026: LANDING GEAR. MALFUNCTIONED. ON TAKEOFF WE GOT A RED CAS LG LEVER DISAG. WE RAN THE CHECKLIST. EXTENDED THE GEAR. GOT NORMAL EXTENSION. THEN RETRACTED THE GEAR AND RECEIVED THE SAME CAS MES
- [SDR DXTA2025092605073](https://openairdocs.org/sdr/DXTA2025092605073), Sep 24, 2025: BATTERY. INOPERATIVE. REPEAT WRITE-UP- FIRST FLIGHT WAS NORMAL. SECOND FLIGHT AFTER TAXING OUT TO THE RUNWAY THE EMER LIGHTS CAME ON IN THE CABIN. THEY DIDN`T EXTINGUISH UNTIL WE TUR
- [SDR DXTA2025092305050](https://openairdocs.org/sdr/DXTA2025092305050), Sep 22, 2025: LIGHT SYS. MALFUNCTIONED. CABIN EMERGENCY LIGHTS CAME ON BY THEMSELVES WITH SWITCH IN THE ARM POSITION. EXTINGUISHED BY THEMSELVES APPROX 5 MINS LATER DURING CLIMB. AFTER LANDING, WITH T
- [SDR DXTA2025061603872](https://openairdocs.org/sdr/DXTA2025061603872), Jun 12, 2025: RADAR. FAULTED. METALLIC SMELL PRESENT IN COCKPIT ON APPROACH. UNABLE TO LOCATE SOURCE, SMELL DISSIPATED ON GROUND. SHORTLY AFTER THE SMELL APPEARED WE NOTICED THE WX RADAR WAS
- [SDR DXTA2025030302515](https://openairdocs.org/sdr/DXTA2025030302515), Feb 25, 2025: CONTROL MODULE. DEFECTIVE. BRK FAIL YELLOW CAS: AFTER TAXING OUT THE BRAKES GRABBED AND THE YELLOW BRK FAIL CAS MESSAGE CAME ON AND WE LOST THE FOOT BRAKES. WE HAD TO USE THE EMERGENCY BR
- [SDR DXTA2024112501236](https://openairdocs.org/sdr/DXTA2024112501236), Nov 18, 2024: CONTROL MODULE. FAILED. ON TAXI OUT, BRK FAIL CAS ILLUMINATED AFTER TAXIING FOR 10 MIN. EMER BRAKE APPLIED. NO FLAT SPOTS ON MAINS. REPLACED BRAKE CONTROL MODULE. OPS CHECK GOOD. IAW P
- [SDR DXTA2024112101192](https://openairdocs.org/sdr/DXTA2024112101192), Nov 18, 2024: CONTROL MODULE. FAULTED. ON TAXI OUT, BRK FAIL CAS ILLUMINATED AFTER TAXIING FOR 10 MIN. EMER BRAKE APPLIED. NO FLAT SPOTS ON MAINS. REPLACED BRAKE CONTROL MODULE. OPS CHECK GOOD. IAW P
- [SDR DXTA2024101600829](https://openairdocs.org/sdr/DXTA2024101600829), Oct 12, 2024: CONTROL MODULE. ILLUMINATED. BRK FAIL YELLOW CAS CAME ON DURING TAXI OUT OF RAMP CORRECTIVE ACTION; REMOVED AND REPLACED BRAKE CONTROL MODULE !AW PHENOM 300 AMM 32-41-07. OPS CHECK GOOD. NO
- [SDR DXTA2024051511779](https://openairdocs.org/sdr/DXTA2024051511779), May 15, 2024: DOOR. OUT OF ALIGNMENT. MAIN DOOR: CAN NOT CLOSE MAIN ENTRY DOOR. THE DOOR APPEARS SAGGED DOWN OR OUT OF ALIGNMENT. PINS ARE RETRACTED AND THERE IS NOTHING VISIBLY OBSTRUCTING THE DOOR
- [SDR DXTA2024012910750](https://openairdocs.org/sdr/DXTA2024012910750), Jan 28, 2024: BRAKE ASSY. ABNORMAL. LEFT MLG BRAKE: WHILE TAXING, JUST BARELY TOUCHING THE BRAKES, THE BRAKES WOULD GRAB AND JERK THE AIRCRAFT! BOTH LEFT AND RIGHT SIDE! ALSO DURING SHARP TURNS, T
- [SDR DXTA2023121110307](https://openairdocs.org/sdr/DXTA2023121110307), Dec 10, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN ENTRY DOOR BINDS UPON CLOSURE.. WILL NOT CLOSE FULLY. OPEN MAIN CABIN DOOR, INSPECTED, PINS, SEALS, INSIDE AND OUTSIDE DOOR HANDLE. NO DISCREPAN
- [SDR DXTA2023102097380](https://openairdocs.org/sdr/DXTA2023102097380), Oct 6, 2023: UPLOCK. DEFECTIVE. AFTER TAKEOFF WE SELECTED GEAR UP. THE LEFT MAIN LANDING GEAR DIDN'T FULLY RETRACT (YELLOW CROSSHATCH ICON) THEN AN LG LEVER DISAG RED-CAS MESSAGE POSTED. WE FO
- [SDR DXTA2023082593860](https://openairdocs.org/sdr/DXTA2023082593860), Aug 25, 2023: POWER STRIP. INOPERATIVE. ENROUTE THE CABIN EMERGENCY LIGHTING BEGAN TO FLASH ON AND OFF. REMOVED AND REPLACED THE #1 AND# 2 EMERGENCY LIGHT POWER UNIT WITH A TESTED UNITS IAW EMB-505AMM
- [SDR DXTA2023071090560](https://openairdocs.org/sdr/DXTA2023071090560), Jul 7, 2023: CONTROL MODULE. DEFECTIVE. AFTER NORMAL START WITHOUT GPU, WE STARTED TAXIING AND DID THE NORMAL BRAKE CHECK. AFTER MOVING ABOUT 60' ONTO A TAXIWAY I GENTLY APPLIED THE BRAKES AND GOT A Y
- [SDR DXTA2023032883350](https://openairdocs.org/sdr/DXTA2023032883350), Mar 28, 2023: BATTERY. DEFECTIVE. CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT. EMOVED EMERGENCY POWER UNIT PN:7450LS-00 SN:005344. INSTALLED TESTED UNIT PN 7450LS-00 SN:005655. OPS CHECK GOOD NO D
- [SDR DXTA2022100371430](https://openairdocs.org/sdr/DXTA2022100371430), Oct 1, 2022: BATTERY PACK. DEFECTIVE. EMERG LIGHT SWITCH: EMER LIGHTS STAY ILLUMINATED WITH SWITCH IN ARM POSITION. REMOVED FAILED #I & #2 EMERGENCY BATTERIES AND INSTALLED SERVICEABLE #I & #2 EMERG
- [SDR DXTA2022060963570](https://openairdocs.org/sdr/DXTA2022060963570), Jun 8, 2022: NONE. DEFECTIVE. LEFT MLG BRAKE: LEFT BRAKE WAS VERY ON FIRST LANDING (LEFT SEAT). THE SECOND LANDING WAS OK (RIGHT SEAT). ON TAXI OUT, LEFT BRAKE IS EXTREMELY GRABBY AND JERKS 
- [SDR DXTA2021102550770](https://openairdocs.org/sdr/DXTA2021102550770), Oct 22, 2021: BATTERY. DEFECTIVE. COCKPIT EMERG LIGHT: EMERGENCY LIGHTS FLASHING DURING DECENT CYCLED SWITCH ON AND OFF. PUT SWITCHES IN ARM POSITION THEY STAYED ON DURING THE REST OF FLIGHT. //
- [SDR DXTA2021081246800](https://openairdocs.org/sdr/DXTA2021081246800), Aug 11, 2021: HANDLE. BROKEN. MAIN DOOR: RED HANDLE ON MAIN DOOR BROKE OFF. NORMAL FORCE WAS USED TO OPEN DOOR. REMOVED AND REPLACED MCD EXTERNAL HANDLE DUE TO HANDLE BROKEN, OPS CHECKS GOOD
- [SDR DXTA2021072144450](https://openairdocs.org/sdr/DXTA2021072144450), Jun 30, 2021: CONTROL MODULE. DEFECTIVE. BRK FAIL YELLOW CAS: ON TAXI OUT AT KASG WE HAD A BRAKE FAIL CAS MESSAGE ILLUMINATE. I ATTEMPTED TO USE THE MAIN BRAKES TOO SLOW THE AIRCRAFT TO A STOP AND GOT 
- [SDR DXTA2021072142760](https://openairdocs.org/sdr/DXTA2021072142760), May 27, 2021: CONTROL MODULE. DEFECTIVE. BRK FAIL YELLOW CAS: AFTER BLOCK OUT AND TAXIING 150 YARDS YELLOW CAS MESSAGE APPEARED. BRAKES FAILED ON BOTH SIDES . // SIGNOFF// -PERFORMED OPS CHECK OF THE H
- [SDR JGVR20200921001](https://openairdocs.org/sdr/JGVR20200921001), Sep 21, 2020: BALANCE WEIGHT. UNSERVICEABLE. WHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE PER SB AND REPLACED WITH NEW PARTS. ONE LT ELEVATO
- [SDR DXTA2018042000859](https://openairdocs.org/sdr/DXTA2018042000859), Apr 19, 2018: WARNING MESSAGE. FALSE ACTIVATION. BOTH FLAP EXTENSION FAIL, FCE FAULT. DURING CLIMB, AUTOPILOT DISENGAGED AND SWPS FAULT AND SPOILER FAULT CAS MESSAGES DISPLAYED. PERFORMED A FLAP SYSTEM OPERATI

## 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

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