# N340QS: 2014 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: 50500189
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: April 3, 2014
- Certificate issued: October 15, 2026
- Expires: October 31, 2033
- Mode S code: A3BEBD
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=340QS
- Page: https://openairdocs.org/aircraft/N340QS

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 N340QS.

## FAA accident and incident reports

None matched to N340QS.

## Reports on N340QS not matched to an aircraft (1)

They name N340QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20020516018989I](https://openairdocs.org/incident/20020516018989I), May 16, 2002: Cessna 560CESSNA (N340QS), Buffalo, NY. (-23) On Thursday, may 16, 2002, while on approach to landing at the Buffalo niagara international airport, the left main gear light did not indicate down and…

## Service difficulty reports (12)

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 DXTA2026031007159](https://openairdocs.org/sdr/DXTA2026031007159), Mar 7, 2026: BRAKE SYS. FAULTED. DURING TAXI RIGHT BRAKE SHUTTER. PERFORMED BLEEDING OF THE R/H BRAKE ASSY, REMOVED SMALL AMOUNT OF AIR, PERFORMED TAXI CHECK, NO DEFECTS NOTED. ALL WORK IN REF 
- [SDR DXTA2025050403346](https://openairdocs.org/sdr/DXTA2025050403346), May 4, 2025: INDICATOR. FALSE INDICATION. RIGHT ENGINE ENGINE FUEL FLOW INDICATION: RIGHT ENGINE FUEL FLOW NOT SHOWING CORRECT NUMBER IN CLIMB, CRUISE, DESCENT, OR ENGINE OFF POSITION AFTER LAND. FUEL F
- [SDR DXTA2024092000583](https://openairdocs.org/sdr/DXTA2024092000583), Sep 17, 2024: BATTERY PACK. FAULTED. CABIN EMERG LIGHT: CABIN EMER LIGHTS ILLUMINATED AFTER T/O. REMAINED ILLUMINATED FOR DURATION OF FLIGHT. CORRECTIVE ACTION: REMOVED AND REPLACED #1 AND #2 EMERG
- [SDR DXTA2024072212423](https://openairdocs.org/sdr/DXTA2024072212423), Jul 20, 2024: PIN. DEFECTIVE. ON PREFLIGHT, FOUND THE LOWER (WHEN DOOR IS CLOSED) DOOR LOCK INDICATION IS COVERED BY INSULATION AND UNABLE TO SEE GREEN FLAG. REMOVED AND REPLACED WITH A NEW 
- [SDR DXTA2024061912097](https://openairdocs.org/sdr/DXTA2024061912097), Jun 19, 2024: SHUTOFF VALVE. ODOR. BLEED 2 FAIL YELLOW CAS: UPON LANDING IN TORRANCE, SLIGHT BURNING SMELL IN THE COCKPIT, BLEED 2 FAIL YELLOW CAS MESSAGE APPEARED, YELLOW X OVER THE PRSOV NUMBER
- [SDR DXTA2024061712076](https://openairdocs.org/sdr/DXTA2024061712076), Jun 17, 2024: VALVE. DEFECTIVE. BLEED AIR: NOTICED A SLIGHT BURNING SMELL ON TAKEOFF, WENT AWAY QUICKLY. SHORLTY BEFORE LEVELING OFF AROUND FL230, THE BURNING SMELL CAME BACK AND WAS STRONGER.
- [SDR DXTA2024022210974](https://openairdocs.org/sdr/DXTA2024022210974), Feb 20, 2024: FUEL SYS. WARNING MESSAGE. FUEL DISTRIBUTION: FUEL 1 FEED FAULT CAS MESSAGE. LEFT FEED EJECTOR PUMP HAD YELLOW X. PERFORMED THREE POWER UP AND ENGINE RUN CYCLES AND COULD NOT DUPLICATE TH
- [SDR DXTA2024012510727](https://openairdocs.org/sdr/DXTA2024012510727), Jan 25, 2024: CONTROL UNIT. DEFECTIVE. BRK FAIL YELLOW CAS ON TAXI OUT. FAULT CONDITION FOR BRK FAIL RESET DOES NOT MEET RESET CRITERIA AS IT HAPPENED ON TAXI NOT AIRCRAFT STARTUP. BRAKES APPLICATION
- [SDR DXTA2024012210680](https://openairdocs.org/sdr/DXTA2024012210680), Jan 21, 2024: BATTERY PACK. INOPERATIVE. DURING FLIGHT WHILE THE EMER LT SWITCH WAS IN THE ARM POSITION THE EMERGENCY LIGHT CAME ON IN THE CABIN AND THEN STARTED TO RAPIDLY FLASH FOR THE REMAINDER OF F
- [SDR DXTA2020113004398](https://openairdocs.org/sdr/DXTA2020113004398), Nov 26, 2020: BATTERY. DEFECTIVE. DURING CRUISE FLIGHT THE CABIN EMERGENCY LIGHTS ILLUMINATED WITHOUT BEING COMMANDED BY THE SWITCH POSITION. REMOVED FAULTY EMERGENCY BATTERY NR 1 FWD PN:6450LS-
- [SDR DXTA2019071902643](https://openairdocs.org/sdr/DXTA2019071902643), Jul 19, 2019: ELECTRONIC UNIT. UNSERVICEABLE. DURING CRUISE AT FL410, THE AMBER SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND WHITE SPOILER FAULT CAS MESSAGES ILLUMINATED. WE COMPLIED WITH THE FLAP FAIL QRC AND
- [SDR DXTA2019052002416](https://openairdocs.org/sdr/DXTA2019052002416), May 19, 2019: COMPUTER. MALFUNCTIONED. GEA 2 FAIL WHITE CAS ILLUMINATED - WHILE IN CRUISE FLIGHT. RECEIVED ENG NO DISPATCH CAS MESSAGE, FOLLOWED BY A-I E1 FAIL THEN GEA 2 FAIL CAS. ON APPROACH WE KNE

## Service difficulty reports on N340QS not matched to an aircraft (15)

They name N340QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2011101904755](https://openairdocs.org/sdr/DXTA2011101904755), Oct 18, 2011: ACTUATOR. MALFUNCTIONED. ON APPROACH AT GEAR EXTENSION, ONLY THE NOSE AND RT MAIN GREEN CAME ON, NO LT GREEN AND THE RED UNLOCK STAYED ON. CYCLED THE GEAR UP AND DOWN, THE RESULT WAS 3 
- [SDR DXTA2011060604606](https://openairdocs.org/sdr/DXTA2011060604606), Jun 3, 2011: CONTROL CABLE. OUT OF ADJUST. ON TAKEOFF, LT ENGINE N1 REACHED 97.0 PERCENT AT FIREWALL. PERFORMED ENGINE RUN, FOUND THAT ENGINE DID MAKE POWER BUT HAD LITTLE CUSHION. ADJUSTED CABLE AT THE 
- [SDR DXTA2011021404466](https://openairdocs.org/sdr/DXTA2011021404466), Feb 12, 2011: STRUT. OUT OF LIMITS. AFTER LANDING FROM THE RT SEAT, BRAKE PEDALS WENT TO THE FLOOR. THEY EVENTUALLY GRABBED BUT LOW TO THE FLOOR. ON TAXI IN FROM THE LT SEAT, THE BRAKES PULLED HAR
- [SDR DXTA2010122704379](https://openairdocs.org/sdr/DXTA2010122704379), Dec 26, 2010: LINE. LEAKING. AFTER LOWERING LANDING GEAR, POWER BRAKE LOW PRESSURE CAUTION LIGHT AND ANTISKID INOP CAUTION LIGHTS ILLUMINATED. RESET THE SKID CONTROL C/B. BOTH CAUTION LIGHT
- [SDR DXTA2010122704382](https://openairdocs.org/sdr/DXTA2010122704382), Dec 23, 2010: RELAY. MALFUNCTIONED. AFTER LOWERING LANDING GEAR, POWER BRAKE PRESSURE LOW AND ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. RESET ANTISKID CONTROL CIRCUIT BREAKER AND BOTH CAUTION LIGHT
- [SDR DXTA2009122803915](https://openairdocs.org/sdr/DXTA2009122803915), Dec 27, 2009: OUTFLOW VALVE. MALFUNCTIONED. EMERGENCY PRESSURE LIGHT AFTER TAKEOFF. LOUD RUSH SOUND JUST BEFORE PRESSURE SPIKE 2500FPM DOWN THEN EMERGENCY PRESSURE CAME ON. DID EMERGENCY CHECKLIST AND SEL
- [SDR DXTA2009120203877](https://openairdocs.org/sdr/DXTA2009120203877), Dec 1, 2009: BRAKE SYS. MALFUNCTIONED. LT BRAKE IS GRABING ON TAXI PULLING THE NOSE LT (BOTH PILOTS AND CO PILOTS SIDE). REPLACED BOTH MAIN WHEEL BRAKE ASSY W/ O/H UNITS IAW MM CHP 32-42-01 & 32-42-0
- [SDR DXTA200803152](https://openairdocs.org/sdr/DXTA200803152), Jun 28, 2008: WIRE. CHAFED. WHEN SELECTING FLAPS FROM 0 DEG TO 15 DEG THERE WAS NO MOVEMENT ON FLAP INDICATOR. ADDITIONALLY NOTED WAS THE FLAP CNTRL C/B WAS OUT. FOUND WIRE CHAFING IN LT F
- [SDR DXTA200702731](https://openairdocs.org/sdr/DXTA200702731), Dec 31, 2007: WIRE HARNESS. CHAFED. LANDING GEAR WILL NOT RETRACT. FOUND WIRE BUNDLE CHAFED IN 2 LOCATIONS JUST AFT OF WHEEL WELL. REPAIRED DAMAGED WIRES IAW CE560 M/M CHAP 32-01-00. OPERATIONAL C
- [SDR DXTA200702725](https://openairdocs.org/sdr/DXTA200702725), Dec 28, 2007: UNKNOWN. MALFUNCTIONED. AFTER ESTABLISHING A POSITIVE RATE FOR TAKEOFF, ATTEMPTED TO RETRACT MLG. MLG HANDLE WOULD NOT RETRACT. NOTICED ALL LIGHTS EXTINGUISHED AND CB BREAKER POPPED. M
- [SDR DXTA200702453](https://openairdocs.org/sdr/DXTA200702453), Sep 7, 2007: MOTOR. SMOKE. HEAVY SMOKE AND BURNING ODOR DISCOVERED IN THE BATTERY COMPARTMENT 7 MINUTES AFTER HOOKING UP GPU AND RUNNING AIR CONDITIONER. REMOVED AND REPLACED AC COMPRESSO
- [SDR DXTA200702409](https://openairdocs.org/sdr/DXTA200702409), Aug 16, 2007: FUEL CONTROL. OUT OF RIG. RIGHT FUEL BOOST PUMP CAME ON AND THEN RIGHT ENGINE SHUTDOWN. RAN ENGINE, VERIFIED ENGINE SQK, FOUND THROTTLE CABLE TO FCU OUT OF RIG. RERIGGED THROTTLE CABLE &
- [SDR DXTA200601459](https://openairdocs.org/sdr/DXTA200601459), Jun 27, 2006: PITOT SYSTEM. CONTAMINATED. DURING T/O ROLL, IAS FLAGGED ON BOTH PILOT AND COPILOT AIRSPEED INDICATOR. T/O WAS ABORTED. PURGED NR 1 AND NR 2 PITOT SYSTEMS IAW CESSNA 560 MM 34-11-10. FOUND
- [SDR DXTA200500661](https://openairdocs.org/sdr/DXTA200500661), Apr 4, 2005: STRUCTURE. BIRD STRIKE. BIRD STRIKE ON TAKEOFF. DAMAGE TO RIGHT HORIZONTAL STAB APPROX 8 INCHES WIDE & 2 INCHES DEEP.
- [SDR CWQR2004001](https://openairdocs.org/sdr/CWQR2004001), Aug 26, 2004: WIRE HARNESS. BURNED. DURING INSPECTION, FOUND LEFT WING OUTBOARD FUEL QUANTITY TRANSMITTER WIRING HARNESS INSOLATION BURNT BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITI

## 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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