# N331QS: 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: 50500183
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: July 12, 2018
- Certificate issued: November 24, 2025
- Expires: November 30, 2032
- Mode S code: A39AF5
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=331QS
- Page: https://openairdocs.org/aircraft/N331QS

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

None matched to N331QS.

## FAA accident and incident reports

None matched to N331QS.

## Service difficulty reports (18)

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 DXTA2026101910218](https://openairdocs.org/sdr/DXTA2026101910218), Oct 16, 2026: BRAKE ASSY. WEAK. BRAKES NOTICEABLY LESS RESPONSIVE AS NORMAL. FELT VERY SPONGEY AND WEAK BRAKE ACTION. UPON ARRIVAL TO AIRCRAFT, INSPECTED LT & RT MLG BRAKE ASSEMBLIES AND NOTED
- [SDR DXTA2026031907263](https://openairdocs.org/sdr/DXTA2026031907263), Mar 15, 2026: ENGINE. FAILED. DURING THE TAKE OFF ROLL AROUND 30 KNOTS WE EXPERIENCED A RIGHT ENGINE FAILURE. WE HEARD 4-5 COMPRESSOR STALLS. ENGINE SHUT DOWN ON ITS OWN. WE PULLED OFF THE R
- [SDR DXTA2025120205928](https://openairdocs.org/sdr/DXTA2025120205928), Dec 1, 2025: FUEL CONTROL. FAILED. FUEL FEED 1 FAULT & FUEL FEED 2 FAULT MESSAGES DISPLAYED IN FLT, ACCOMPANIED WITH YELLOW XS OVER MOTIVE FLOW PUMPS ON FUEL SYNOPTIC PAGE. NR 1 MESSAGE APPEARED 
- [SDR DXTA2025110705570](https://openairdocs.org/sdr/DXTA2025110705570), Nov 4, 2025: INTERFACE UNIT. DEFECTIVE. DESCENDING THROUGH FL240, RECEIVED OXY LO PRES, AND YELLOW XS THROUGH MULTIPLE INDICATORS: BAT 1 VOLTAGE, HYDRAULIC PRESSURE, FUEL FLOW, OIL TEMP/PRESSURE E1. O
- [SDR DXTA2025040702949](https://openairdocs.org/sdr/DXTA2025040702949), Apr 4, 2025: BATTERY. INOPERATIVE. DURING THE LANDING PHASE OF THE PREVIOUS LEG, WE NOTICED LIGHTS IN THE CABIN FLASHING ON AND OFF AND REALIZED THEY WERE THE EMERGENCY LIGHTS. DURING THE TAXI IN
- [SDR DXTA2024120401366](https://openairdocs.org/sdr/DXTA2024120401366), Dec 1, 2024: BATTERY PACK. INOPERATIVE. EMERG LIGHT SWITCH: EMERGENCY LIGHTS TURN ON ANY TIME SWITCH IS IN "ARM" POSITION. CORRECTIVE ACTION; REPLACED BOTH EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD.
- [SDR DXTA2024101100809](https://openairdocs.org/sdr/DXTA2024101100809), Oct 10, 2024: LIGHT. FAULTED. CABIN EMERG LIGHT: THE RED EMERGENCY FLOOR LIGHT LOCATED BY THE MED AND THE EMERGENCY WHITE FLOOR LIGHT LOCATED BY SEAT #1 OR OBSCURED BY THE AISLE FLOOR CARPET
- [SDR DXTA2023112110104](https://openairdocs.org/sdr/DXTA2023112110104), Nov 20, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR IS CLOSED AND LOCKED BUT NO GREEN FLAG INDICATION ON THE VISUAL SIGHT GLASS UPPER RIGHT CORNER AND RED PASSENGER SYNOPTIC DOOR SHOWS 
- [SDR DXTA2023082894030](https://openairdocs.org/sdr/DXTA2023082894030), Aug 27, 2023: HANDLE. BROKEN. UPON OPENING THE MAIN DOOR THE HANDLE DETACHED FROM THE AIRCRAFT. REMOVED TAPE & OPENED DOOR. REMOVED STEPS & ACCESSED THE INTERNAL PORTION OF THE DOOR HANDLE. 
- [SDR DXTA2023070390240](https://openairdocs.org/sdr/DXTA2023070390240), Jul 3, 2023: UNKNOWN. UNKNOWN. CABIN POWER (60 HZ): WHEN I OPENED THE AFT BAGGAGE COMPARTMENT AFTER A 3 HOUR FLIGHT THERE WAS A STRONG SMELL OF ELECTRICAL BURNING. WE REMOVED ALL LUGGAGE THE 
- [SDR DXTA2021113052780](https://openairdocs.org/sdr/DXTA2021113052780), Nov 29, 2021: BATTERY. DEFECTIVE. EMER LIGHT SWITCH: DURING BEFORE ENGINE START FLOW, SWITCH IS MOVED INTO ARM POSITION AND ALL AIRCRAFT EMERGENCY LIGHTS INCORRECTLY TURN ON BOTH INSIDE AND OUTS
- [SDR DXTA2021082547650](https://openairdocs.org/sdr/DXTA2021082547650), Aug 24, 2021: EVAPORATOR. CONTAMINATED. CABIN ODOR: STRONG MILDEW OR MUSTY SMELL IN CABIN WHEN THE VCS IS SELECTED ON. CLEANED DEBRIS FROM THE FORWARD AND AFT EVAPORATORS, RAN VCS AND CHECKED FOR WATE
- [SDR DXTA2021082447650](https://openairdocs.org/sdr/DXTA2021082447650), Aug 24, 2021: UNKNOWN. ODOR. CABIN ODOR: STRONG MILDEW OR MUSTY SMELL IN CABIN WHEN THE VCS IS SELECTED ON.
- [SDR DXTA2021060443170](https://openairdocs.org/sdr/DXTA2021060443170), Jun 4, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS BATTERY: AFTER TAKEOFF GEAR UP GOT THE EMERGENCY LIGHT NOT ARMED CAS MESSAGE ON THE ELECTRICAL PAGE BOTH BATT 1 & 2 WHERE SHOWING 25.1 AND 25.0
- [SDR DXTA2021011304591](https://openairdocs.org/sdr/DXTA2021011304591), Jan 13, 2021: PINION. DEFECTIVE. MAIN DOOR IS STUCK IN TRANSITION AND WE CAN NOT BRING IT BACK UP OR COMPLETELY LOWER IT. REMOVED AND REPLACE DEFECTIVE COUNTER BALANCE PINION. OPS CHECK GOOD.
- [SDR 2020FA0000429](https://openairdocs.org/sdr/2020FA0000429), Sep 29, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTA
- [SDR DXTA2019050702362](https://openairdocs.org/sdr/DXTA2019050702362), May 8, 2019: WIRE. PULLED. BOTH MLG BRAKE - ON CONSECUTIVE LANDINGS WITH FIRM BRAKE APPLICATION, THE BRAKES DID NOT APPLY EFFECTIVELY RESULTING IN A MUCH LONGER LANDING ROLLOUT. CORRECTIV
- [SDR DXTA2015102006112](https://openairdocs.org/sdr/DXTA2015102006112), Oct 22, 2015: SKIN. DENTED. BIRD STRIKE ON SHORT FINAL RESULTING IN A DENT ON RT WING LE. R & R THE RT WING OUTER LE & RT WING CTR WING SPLICE WITH NEW IAW MM 57-40-00.

## Service difficulty reports on N331QS not matched to an aircraft (13)

They name N331QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200702635](https://openairdocs.org/sdr/DXTA200702635), Nov 28, 2007: BRAKE ASSY. UNKNOWN. ON ROLL OUT, F/O LT BRAKE PEDAL WENT TO THE FLOOR. CAPTAIN`S BRAKES WORK NORMALLLY. BLEED LEFT AND RIGHT BRAKES IAW 32-42-00. OPS CK GOOD.
- [SDR DXTA200702472](https://openairdocs.org/sdr/DXTA200702472), Aug 10, 2007: FITTING. LEAKING. FIRST OFFICER RT BRAKE SLOW TO DEVELOP PRESSURE. INSPECTED CO-PILOTS MASTER CYLINDERS & FOUND TOP FITTING LEAKING & LOOSE, TIGHTENED & CLEANED, BLED BRAKES SEVE
- [SDR DXTA200702396](https://openairdocs.org/sdr/DXTA200702396), Aug 10, 2007: FITTING. LEAKING. FIRST OFFICER, RT BRAKE SLOW TO DEVELOP PRESSURE. INSPECTED CO-PILOTS MASTER CYLINDERS & FOUND TOP FITTING LEAKING & LOOSE, TIGHTENED & CLEANED, BLED BRAKES SEV
- [SDR DXTA200702424](https://openairdocs.org/sdr/DXTA200702424), Jul 27, 2007: MASTER CYLINDER. LEAKING. COPILOTS RT BRAKE PEDAL GOES TO FLOOR WITHOUT BRAKES. PEDAL PUMPS UP NORMALLY AND THEN BRAKE CATCHES. PERFORMED OPS CHECK OF CO-PILOTS R/H BRAKE PEDAL IAW CESSN
- [SDR DXTA200701981](https://openairdocs.org/sdr/DXTA200701981), Mar 1, 2007: ROLLER. LACK OF LUBE. AFTER GEAR RETRACTION, GEAR UNSAFE AND HYDRAULIC PRESS ON LIGHT REMAINED ILLUMINATED. NORMAL INDICATIONS ON GEAR EXTENSION. JACKED AIRCRAFT & DUPLICATED FAULT F
- [SDR DXTA200601680](https://openairdocs.org/sdr/DXTA200601680), Oct 23, 2006: CONNECTOR. DIRTY. AFTER TAKEOFF AND GEAR RETRACTION "GEAR UNLOCKED" AND "HYD PRESS" LIGHTS REMAINED ILLUMINATED. INSPECTED LANDING GEAR, INSPECTED UPLOCK SWITCHES. CLEANED CONNEC
- [SDR DXTA200601393](https://openairdocs.org/sdr/DXTA200601393), May 14, 2006: ACTUATOR. FAULTY. ON TAKEOFF DURING GEAR RETRACTION, GEAR UNLOCK LIGHT AND HYD PRESS LIGHT REMAINED ON. PULLED AND RESET LND GEAR CONTROL CB IAW CHECKLIST FOR HYD PRES ON RESET G
- [SDR DXTA200601386](https://openairdocs.org/sdr/DXTA200601386), May 9, 2006: UPLOCK SWITCH. OUT OF RIG. ON TAKEOFF GEAR UNSAFE LIGHT ILLUMINATED ALONG WITH HYD PRESS LIGHT. GEAR RECYCLED AND MALFUNCTION CLEARED. REMOVED AND REPLACED LT MAIN UPLOCK SWITCH, ADJUSTED
- [SDR DXTA200601330](https://openairdocs.org/sdr/DXTA200601330), Apr 4, 2006: UPLOCK SWITCH. DIRTY. AFTER TAKEOFF GEAR AND FLAPS WERE RETRACTED "HYD PRESS ON" LIGHT REMAINED ON AFTER ALL CYCLES COMPLETE. ALSO ILLUMINATED WAS THE RED GEAR UNSAFE LIGHT. CYCLED G
- [SDR DXTA200500984](https://openairdocs.org/sdr/DXTA200500984), Sep 25, 2005: BRAKE. MALFUNCTIONED. BRAKING PRESSURE ERRACTIC , BRAKES SEEM TO CATCH AND RELEASE, PRESSURE INCREASE AND DECREASE, FELT IN PEDALS.
- [SDR DXTA200500904](https://openairdocs.org/sdr/DXTA200500904), Aug 17, 2005: ANTI-SKID SYS. MALFUNCTIONED. ANTI SKID ACTIVATES INTERMITTANTLY BELOW 5KTS. COMPLETELY ACTIVATES WITH MODERATE BRAKE PRESSURE, RESULTING IN NO BRAKES AT ALL. ANTISKID OFF BRAKES NORMAL. ALL
- [SDR DXTA200300095](https://openairdocs.org/sdr/DXTA200300095), Aug 16, 2003: BRAKE ASSY. MALFUNCTIONED. PILOT REPORTED AT LOW SPEED TAXIING STRAIGHT AHEAD, ANTI SKID IS CYCLING MAKING THE BRAKES SLIP. AIRCRAFT RETURNED TO BLOCK. FOUND NO FAULTS ON ANTI SKID FAULT 
- [SDR 97ZZZX5206](https://openairdocs.org/sdr/97ZZZX5206), Dec 5, 1997: RELIEF VALVE. MALFUNCTION. TROUBLESHOOTING FOR INCOMPLETE RETRACT CYCLE FOUND HYDRAULIC RELIEF VALVE OPENING PREMATURELY.

## 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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