# N367QS: 2015 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: 50500273
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: June 1, 2015
- Certificate issued: August 4, 2026
- Expires: August 31, 2033
- Mode S code: A427BC
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=367QS
- Page: https://openairdocs.org/aircraft/N367QS

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 N367QS.

## FAA accident and incident reports

None matched to N367QS.

## Reports on N367QS not matched to an aircraft (1)

They name N367QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19961210045769I](https://openairdocs.org/incident/19961210045769I), Dec 10, 1996: Gulstm 560 (N367QS), Chicago/Wheelin, IL, Minor damage. Narrative: crew mistook right runway edge lights for runway centerline. The airman mistook runway edge lights for centerline lighting which indicated a lack of…

## 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 DXTA2026010506415](https://openairdocs.org/sdr/DXTA2026010506415), Jan 2, 2026: DOOR. FAULTED. MED INTERIOR RED HANDLE DOES NOT EASILY GO TO THE FULL OPEN POSITION. IT MUST BE FORCED TO THE FULL OPEN POSITION AFTER THE DOOR IS DOWN OR ELSE THE 2 PINS CLOS
- [SDR DXTA2026010206415](https://openairdocs.org/sdr/DXTA2026010206415), Jan 2, 2026: HANDLE. BINDING. MED INTERIOR RED HANDLE DOES NOT EASILY GO TO THE FULL OPEN POSITION. IT MUST BE FORCED TO THE FULL OPEN POSITION AFTER THE DOOR IS DOWN OR ELSE THE 2 PINS CLOS
- [SDR DXTA2025120806001](https://openairdocs.org/sdr/DXTA2025120806001), Dec 5, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS TURN ON WHEN ARMED, & FLICKER IN FLT. REPLACED BOTH EMERGENCY LIGHT BATTERY PACKS DUE TO NOT HOLDING CHARGE & OPS CHKD GOOD IAW AMM 33-52-01.
- [SDR DXTA2024071112327](https://openairdocs.org/sdr/DXTA2024071112327), Jul 10, 2024: BATTERY. DEFECTIVE. EMER LIGHTS FLASH CONTINUOUSLY IN ARM POSITION. PERFORMED T/SHOOTING FOUND AFT CABIN(LAV AREA) EMERGENCY BATTERY INOP, MCC REQUESTED TO R/R BOTH EMER. BATTERY. 
- [SDR DXTA2023101197670](https://openairdocs.org/sdr/DXTA2023101197670), Oct 10, 2023: SHUTOFF VALVE. FAULTED. DURING CRUISE AT FL410 HAD EMER BRK LO PRESS YELLOW CAS MESSAGE. ACCUMULATOR PRESSURE BLED DOWN SLOWLY FROM 1600 PSI UNTIL APROX 1100 PSI THEN DROPPED TO 100 PS
- [SDR DXTA2022081668140](https://openairdocs.org/sdr/DXTA2022081668140), Aug 16, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: WHEN EMER LT SWITCH IS MOVED FROM THE OFF TO THE ARM POSITION, FOR ENGINE START, LIGHTS REMAIN ILLUMINATED FOR ABOUT 5 MINUTES BEFORE EXTINGU
- [SDR 2020FA0000496](https://openairdocs.org/sdr/2020FA0000496), Nov 9, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEV
- [SDR DXTA2020080503940](https://openairdocs.org/sdr/DXTA2020080503940), Aug 5, 2020: ELECTRONIC UNIT. FAULTED. CRUISE FLIGHT FL360, GOT THE FOLLOWING: SWPS FAULT EICAS, FLAP FAIL EICAS, PTRIM BKP FAIL EICAS, SPOILER FAULT WHITE EICAS. YELLOW X'S DISPLAYED IN FLAP INDICAT
- [SDR 2018FA0000491](https://openairdocs.org/sdr/2018FA0000491), Nov 27, 2018: CONTROL CABLE. CHAFED. DURING INSPECTION IT WAS FOUND THAT THE LH AND RH AFT UPPER SECTION OF RUDDER CABLES WERE CHAFED BEYOND LIMITS. IT WAS NOTED THAT THE CHAFING IS HAPPENING AT TH
- [SDR 2019F00019](https://openairdocs.org/sdr/2019F00019), May 23, 2018: SUPPORT. CRACKED. DURING SCHEDULED MAINTENANCE IT WAS NOTED THAT LEFT HAND ADJUSTABLE RUDDER TORQUE TUBE SUPPORT ROD WAS FOUND TO HAVE A 2 INCH LONGITUDINAL CRACK (SEPARATED). AF
- [SDR DXTA2016090606297](https://openairdocs.org/sdr/DXTA2016090606297), Sep 6, 2016: BRAKE ASSY. CONTAMINATED. AIRCRAFT PULLS TO THE LT WHILE APPLYING BRAKES. BIRD REMAINS DISCOVERED IN BRAKE FROM THE BIRD STRIKE THIS WORK ORDER. REMOVED BIRD REMAINS FROM AROUND BRAKE AR
- [SDR DXTA2016062406261](https://openairdocs.org/sdr/DXTA2016062406261), Jun 30, 2016: VALVE. INOPERATIVE. NR 1 DUCT OVERTEMP MESSAGE APPEARED WHILE LEVELING AT FL400. CREW PERFORMED QRH AND AFTER SWITCHING TO ECS 2, NR 2 DUCT OVERTEMP MESSAGE APPEARED. HAD BOTH NR 1

## Service difficulty reports on N367QS not matched to an aircraft (21)

They name N367QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200811193363](https://openairdocs.org/sdr/DXTA200811193363), Nov 19, 2008: RELIEF VALVE. INOPERATIVE. AT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND THE HYD PRESS LIGHT REMAINED ILLUMINATED. REPEAT WRITE UP
- [SDR DXTA2008111903363](https://openairdocs.org/sdr/DXTA2008111903363), Nov 19, 2008: WARNING SYSTEM. ACTIVATED. AT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED.
- [SDR DXTA200811173362](https://openairdocs.org/sdr/DXTA200811173362), Nov 17, 2008: PIVOT. LACK OF LUBE. ON LANDING ROLL RT THRUST REVERSER UNLOCKED BUT WOULD NOT DEPLOY, TRIED AGAIN ON TAXI & NO DEPLOY. ON THE THRUST REVERSER CHECK PRE-FLT, DEPLOYED. ACTUATED THRU
- [SDR DXTA2008111803362](https://openairdocs.org/sdr/DXTA2008111803362), Nov 17, 2008: WARNING SYSTEM. ACTIVATED. AT GEAR RETRACTION THE THREE GREEN LIGHTS EXTINGUISHED, BUT THE RED GEAR UNLOCKED LIGHT REMAINED ON.
- [SDR DXTA200803177](https://openairdocs.org/sdr/DXTA200803177), Jul 15, 2008: BRAKE. WEAK. BOTH F/O-SIDE BRAKE PEDALS ARE VERY MUSHY. THEY TRAVEL 3/4 OF THE WAY DOWN BEFORE BREAKING OCCURS. BLED ANTISKID BRAKE SYSTEM. CO-PILOT AND PILOT SIDE BRAKE PED
- [SDR DXTA20082877](https://openairdocs.org/sdr/DXTA20082877), Feb 14, 2008: UNKNOWN. WARNING LIGHT. AFTER GEAR RETRACTION WAS SELECTED RED INTRANSIT LIGHT REMAINED ON. JACKED AC, INSPECTED W/W AND WIRING CK'D SWITCHES IAW WDM 32-30-01-02 AND 32-60-01-04 ALL NO
- [SDR DXTA200702523](https://openairdocs.org/sdr/DXTA200702523), Oct 3, 2007: BRAKE ASSY. MALFUNCTIONED. CO-PILOT'S BRAKES WENT TO THE FLOOR TWICE AT THE END OF LANDING ROLLOUT. 10-29-07 ACCESSED BRAKE RESERVOIR, ATTACHED BRAKE BLEEDING KIT. BLED THE ANTI-ICE BRAKE
- [SDR DXTA200701838](https://openairdocs.org/sdr/DXTA200701838), Jan 5, 2007: UNKNOWN. UNKNOWN. UPON GEAR RETRACTION GEAR UNLOCKED LIGHT REMAINED ON AND HYD PRESS ON LIGHT REMAINED ON. GEAR EXTENDED NORMALLY. JACKED AND SWUNG THE GEAR OVER 12 TIMES OPS CHE
- [SDR DXTA200601810](https://openairdocs.org/sdr/DXTA200601810), Dec 21, 2006: SEAL. FAILED. CABIN DOOR PRIMARY SEAL FAILED AT FL 400, DOOR SEAL ANNUNC. ILLUMINATED. DOOR SEAL ANNUNC. EXTINGUISHED DURING DESCENT AT FL380. PURGED CABIN DOOR PRIMARY SEAL 
- [SDR DXTA200601668](https://openairdocs.org/sdr/DXTA200601668), Oct 18, 2006: WARNING MESSAGE. FALSE ACTIVATION. "POWER BRAKE LOW PRESS" AND "ANTI-SKID INOP" LIGHTS REMAINED ON AFTER GEAR WAS SELECTED DOWN. BOTH SETS BRAKE PEDALS HAD NO PRESSURE. GEAR WAS RAISED TO DIVERT 
- [SDR DXTA200601343](https://openairdocs.org/sdr/DXTA200601343), Apr 14, 2006: BRAKE. INTERMITTENT. DURING TAXI IN , AT APPROX 10 KTS AND DURING BRAKE APPLICATION, THE BRAKES (LET GO) FOR APPROX 1.5 SECONDS. THEY WERE COMPLETELY NORMAL AFTER THAT. CHECKED BRAK
- [SDR DXTA200601271](https://openairdocs.org/sdr/DXTA200601271), Feb 27, 2006: ACTUATOR. FAILED. THE RED -GEAR UNLOCKED- LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK ACUATOR REF CESSNA 560 ULTRA MM 32-31-05.
- [SDR DXTA200601252](https://openairdocs.org/sdr/DXTA200601252), Feb 19, 2006: UPLOCK. DIRTY. RED GEAR UNSAFE AND HYD PRESS ON LIGHT REMAINED ILLUM AFTER GEAR RETRACTION ON TAKEOFF. CKLST ISOLATED PROBLEM TO GEAR CONTROL CB, WHICH GAVE GREEN MAINS/RED UN
- [SDR DXTA200500810](https://openairdocs.org/sdr/DXTA200500810), Jun 29, 2005: BRAKE ASSY. MALFUNCTIONED. ON TAXI ZERO BRAKING FOR SEVERAL SECONDS, THEN BRAKES GRABBED. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200500801](https://openairdocs.org/sdr/DXTA200500801), Jun 23, 2005: ENGINE. MALFUNCTIONED. T/O N1 REQUIRED 96.1; AS POWER WAS ADVANCED FOR T/O AND GOING THRU APPROX 84-85 PERCENT RT ENGINE OIL PRESS EXCEEDED 95 PSI AND TEMP WAS APPROACHING 120 DEGREES
- [SDR DXTA200500581](https://openairdocs.org/sdr/DXTA200500581), Feb 9, 2005: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF GEAR RETRACTION RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND HYD PRESS ON LIGHT ILLUMINATED. GEAR WAS CYCLED BUT LIGHTS REMAINED ON. WHEN GEAR
- [SDR DXTA200500569](https://openairdocs.org/sdr/DXTA200500569), Jan 31, 2005: CONTROL CABLE. FRAYED. DURING INSPECTION FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLE FRAYED IN TAIL CONE. PIN BOTH FORE & AFT SECTIONS & USE CABLE BLOCKS TO REMOVE & REPLACE CABLE. PU
- [SDR DXTA200400510](https://openairdocs.org/sdr/DXTA200400510), Jan 3, 2005: ATTACH ANGLE. OUT OF ALIGNMENT. RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR AND CYCLED GEAR THREE GREEN, NO RED WHEN LOWERED. FOUND LT MLG DOOR ANGLE HITTIN
- [SDR DXTA200400351](https://openairdocs.org/sdr/DXTA200400351), Aug 1, 2004: CONNECTOR. DAMAGED. GEAR WOULD NOT RETRACT, GEAR INTRANSIT LIGHT STAYED ON AS WELL AS THE HYDRAULIC PRESSURE LIGHT. THE GEAR WAS CYCLED SEVERAL TIMES AND NO CHANGE. JACKED AIRCRAFT
- [SDR DXTA200400345](https://openairdocs.org/sdr/DXTA200400345), Jul 22, 2004: FIRE DETECTOR. MALFUNCTIONED. LT ENGINE FIRE LIGHT CAME ON DURING TAXI, BOTH FIRE BOTTLES BLOWN. NO INDICATION ON ENG FIRE UPON EVACUATION. INSPECTED ENGINE WITH NO EVIDENCE OF FIRE, REMOVED
- [SDR DXTA200400318](https://openairdocs.org/sdr/DXTA200400318), May 27, 2004: POSITION SWITCH. MALFUNCTIONED. CLIMBING 13,000 FT 265 KTS, LT THROTTLE SNATHER ENGAGED, BRINGING ENG BACK 1 INCH FROM STOPS. A LOUD RUSHING NOISE HEARD CONSISTENCE WITH T/R DEPLOYMENT. NO T/R

## 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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