# N304QS: 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: 50500143
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: June 14, 2013
- Certificate issued: September 27, 2023
- Expires: September 30, 2030
- Mode S code: A32F9D
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304QS
- Page: https://openairdocs.org/aircraft/N304QS

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS16IA008](https://openairdocs.org/ntsb/OPS16IA008), Apr 7, 2016: Embraer S A EMB-505 (N304QS), Dallas, TX, incident, no damage. Probable cause: The controller's miscommunication of a clearance and failure to recognize and correct the readback resulting in the flight crew initiating takeoff without a clearance.

## FAA accident and incident reports

None matched to N304QS.

## Service difficulty reports (16)

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 DXTA2026072008871](https://openairdocs.org/sdr/DXTA2026072008871), Jul 16, 2026: BRAKE. FAULTED. ON TAXI OUT WHILE MAKING A 90 DEGREE RIGHT TURN, THE RIGHT MAIN TIRE/BRAKE FELT LIKE IT WAS SKIDDING. AFTER DECIDING TO RETURN TO THE RAMP, PROBLEM PERSISTED AN
- [SDR DXTA2026032007308](https://openairdocs.org/sdr/DXTA2026032007308), Mar 18, 2026: BATTERY. DEFECTIVE. EMERGENCY LIGHTS FLICKERING AND EMER LT NOT ARM CAS MESSAGE DISPLAYED. REPLACED BATTERIES. OPS CHECK GOOD. IAW AMM 33-52-01.
- [SDR DXTA2025030302541](https://openairdocs.org/sdr/DXTA2025030302541), Feb 28, 2025: STRUT. ABNORMAL. MAIN DOOR: THE MAIN CABIN DOOR GAS STRUTS DO NOT APPPEAR TO BE OPERATIONAL. THE DOOR OPENS ABRUPTLY AND THE WIEGHT OF THE DOOR CAUSES IT TO SLAM OPEN. CORRECTIV
- [SDR DXTA2024122301578](https://openairdocs.org/sdr/DXTA2024122301578), Dec 17, 2024: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: DURING CRUISE FLIGHT AROUND 14,000' WE NOTICED THE CABIN EMERGENCY LIGHTS FLICKERING ON AND OFF RAPIDLY. WE ATTEMPTED TO CHECK THE PLACEMENT 
- [SDR DXTA2024092400636](https://openairdocs.org/sdr/DXTA2024092400636), Sep 22, 2024: HANDLE. BROKEN. WHILE OPENING THE MAIN CABIN DOOR, THE DOORHANDLE BROKE OFF. THE DOORHANDLE IS ON THE COUNTER DIRECTLY IN FRONT OF THE DOOR. CORRECTIVE ACTION: REMOVE AND REPLA
- [SDR DXTA2023122610408](https://openairdocs.org/sdr/DXTA2023122610408), Dec 22, 2023: BATTERY. FAULTED. CABIN EMERGENCY LIGHTS FLICKERING IN FLIGHT. REMOVED AND REPLACED BOTH EMERGENCY LIGHTING BATTERY PACKS DUE TO FLICKERING IN FLIGHT, OPS CHECKS GOOD, CHARGED BA
- [SDR DXTA2023030381740](https://openairdocs.org/sdr/DXTA2023030381740), Mar 2, 2023: SHIMMY DAMPENER. DEFECTIVE. ON LANDING AS BRAKES WERE APPLIED EXPERIENCED AN EXTREMELY VIOLENT VIBRATION COMING FROM THE NOSE LANDING GEAR ACCOMPANIED WITH EMERGENCY, BRAKE PRESSURE, LOW C
- [SDR DXTA2021120352890](https://openairdocs.org/sdr/DXTA2021120352890), Dec 2, 2021: BATTERY. DEFECTIVE. EMERG LIGHT SWITCH: UPON STARTUP EMERG LTSWITCH WAS PLACED TO ARM. EMERG LT NOT ARMED CAS MESSAGE EXTINGUISHED. AFTER STARTUP THE EMERG LT NOT ARMED CAS ILLUMIN
- [SDR DXTA2020121804491](https://openairdocs.org/sdr/DXTA2020121804491), Dec 18, 2020: OUTFLOW VALVE. DEFECTIVE. ON DEPARTURE WE EXPEREIENCED A RED CABIN RATE OF OF CLIMB OF 1000 FPM ON THE CAS. AT 13000 MSL, CABIN CONTINUED TO CLIMB TO 5600 BEFORE WE DECLARED EMERGENCY AN
- [SDR 2020FA0000375](https://openairdocs.org/sdr/2020FA0000375), Aug 16, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMB SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING LEFT ELEVATOR MASS BALANCE WEIGHTS BELOW TOLERANCE: P/N PE915109-L
- [SDR JGVR20200115002](https://openairdocs.org/sdr/JGVR20200115002), Jan 15, 2020: BALANCE WEIGHT. CORRODED. CORROSION ON RH ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS. REPLACED 2 EA RH ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS WITH NEW P/N PE915109-L33 IN SAME LOCATION. 
- [SDR DXTA2019100702923](https://openairdocs.org/sdr/DXTA2019100702923), Oct 6, 2019: VALVE. FAILED. AIR DUCT - DUCT 1 OVERTEMP CAME ON IN DESCENT TO KABE WITH ALL ENGINE AND WING ANTI ICE ON. COMPLIED WITH QRH CHECKLIST. OVERTEMP DID NOT GO OUT WITH IN THE TIM
- [SDR DXTA2016081306281](https://openairdocs.org/sdr/DXTA2016081306281), Aug 15, 2016: SKIN. DAMAGED. BIRD STRIKE ON L/E STARBOARD WING. EVALUATED AND MAPPED DAMAGE ON RT OTBD L/E SENT DESCRIPTION OF DAMAGE TO CONTACT CENTER FOR ANALYSIS. REMOVED RT OTBD L/E IAW
- [SDR DXTA2016081506281](https://openairdocs.org/sdr/DXTA2016081506281), Aug 15, 2016: SLAT. DAMAGED. BIRD STRIKE ON L/E STARBOARD WING.
- [SDR DXTA2016012406169](https://openairdocs.org/sdr/DXTA2016012406169), Jan 24, 2016: SWITCH. FAILED. BLEED LEAK 1, AMBER CAS MESSAGE ILLUMINATED, IN FLIGHT AT FL270. COMPLIED WITH QRH & QRC. SHUTDOWN NR 1 ENGINE & DIVERTED. R & R NR 1 ENGINE FWD BLEED LEAK THER
- [SDR DXTA2013102905549](https://openairdocs.org/sdr/DXTA2013102905549), Oct 17, 2013: SERVO. INOPERATIVE. DURING CRUISE AT 40,000 FEET, AUTOPILOT FAIL, YAW DAMPER FAIL AND VENTRAL RUDDER FAIL CAS MESSAGES ALL DISPLAYED AT THE SAME TIME. ACFT IMMEDIATELY STARTED TO D

## Service difficulty reports on N304QS not matched to an aircraft (9)

They name N304QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2008120203384](https://openairdocs.org/sdr/DXTA2008120203384), Dec 2, 2008: BULB. BURNED OUT. LT MLG INDICATOR LIGHT INOP. FOUND BULB IN INDICATOR TO BE BURNED OUT. REPLACED BULBS IN INDICATOR AS REQUIRED.
- [SDR DXTA2008120303384](https://openairdocs.org/sdr/DXTA2008120303384), Dec 2, 2008: INDICATOR. INOPERATIVE. LT MLG INDICATOR LIGHT INOP. USED NITROGEN TO BLOW GEAR DOWN.
- [SDR DXTA200803038](https://openairdocs.org/sdr/DXTA200803038), May 1, 2008: SENSOR. INOPERATIVE. DURING DESCENT, W/S AIR O HEAT ILLUMINATED THEN CYCLED OFF THEN ILLUMINATED AGAIN BUT CONTINUOUS. THE SWITCH WAS IN LOW AND COULD SMELL BURNING ODOR. REPLACE WI
- [SDR DXTA200702464](https://openairdocs.org/sdr/DXTA200702464), Sep 10, 2007: BRAKE ASSY. LOCKED. CO-PILOTS BRAKES GRAB UNEVENLY DURING HIGH SPEED APPLICATION. 09-27-07 BLEED OUT BRAKES ON COPILOTS SIDE AND FOUND AIR, SUSPECTED AIR CAME FROM COPILOTS LT AND 
- [SDR DXTA200701862](https://openairdocs.org/sdr/DXTA200701862), Jan 17, 2007: UNKNOWN. UNKNOWN. WHILE APPLYING BRAKE PRESSURE ON LANDING ROLLOUT THE BRAKE SYSTEM SURGES GIVING YOU THE SENSATION OF SLIPPING ON RUNWAY SURFACE.REMOVED ANTI-SKID TRANSDUCERS & 
- [SDR DXTA200601805](https://openairdocs.org/sdr/DXTA200601805), Dec 16, 2006: ACTUATOR. LEAKING. AT GEAR RETRACTION ON TAKEOFF, GEAR UNLOCK LIGHT (RED) AND HYD PRESS ON ILLUMINATED: PERFORMED K2 CHECKLIST, SPEEDBRAKE C/B + T/R C/B'S, NO CHANGE - GEAR C/B, G
- [SDR DXTA200601638](https://openairdocs.org/sdr/DXTA200601638), Oct 7, 2006: GYRO. INOPERATIVE. ON TAKE-OFF ROLL HEADING MODE FAILED ON CAPT SIDE. HEADING MODE REMAINED INOPERATIVE BACK TO SERVICE CENTER RAMP. REMOVED AND REPLACED NR 1DB IAW MM 34-21-05. O
- [SDR DXTA200500874](https://openairdocs.org/sdr/DXTA200500874), Jul 31, 2005: LINK. OUT OF ADJUST. AFTER GEAR RETRACTION NOTED EXCESSIVE AIR NOISE, EXTENDED GEAR, UPON RETRACTION HYD PRESS LIGHT REMAINED ON ALSO GEAR UNLOCK LIGHT STAYED ON. RE-EXTENDED GEAR A
- [SDR DXTA200300140](https://openairdocs.org/sdr/DXTA200300140), Oct 16, 2003: ODOR. DETECTED. ELECTRICAL ODOR ORIGINATING FROM CABIN AREA. SAME ODOR NOTICED IN BATTERY COMPARTMENT ON POST FLIGHT. - RAN AIRCRAFT AT CRUISE POWER FOR ONE HOUR, NO CIRCUIT BR

## 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

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