# N373QS: 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: 50500275
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: June 12, 2015
- Certificate issued: February 25, 2026
- Expires: February 28, 2033
- Mode S code: A4405F
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=373QS
- Page: https://openairdocs.org/aircraft/N373QS

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 N373QS.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20260202000389I](https://openairdocs.org/incident/20260202000389I), Feb 2, 2026: Embraer Executive Aircraft Inc EMB-505 (N373QS), Dallas, TX, Minor damage. During approach a bird struck the left engine cowl starter generator inlet duct. No other observed damage or remains was found. Damage was minor.

## Service difficulty reports (20)

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 DXTA2026082109357](https://openairdocs.org/sdr/DXTA2026082109357), Aug 20, 2026: WIRE HARNESS. FAULTED. UPON EXITING THE RUNWAY, WE FELT A GRINDING/ SHUTTERING NOISE/ GRABBING COME FROM THE RIGHT BRAKE/WHEEL. REMOVED RT MLG WOW/WST WIRE HARNESS AND INSTALLED A NEW
- [SDR DXTA2026042007680](https://openairdocs.org/sdr/DXTA2026042007680), Apr 17, 2026: LIGHT. FAULTY. WHILE IN CRUISE WE NOTICED THE EMER LIGHTS WERE ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. REMAINED ILLUMINATED FOR THE REST OF THE FLIGHT. REMOVED EMERGE
- [SDR DXTA2026033007436](https://openairdocs.org/sdr/DXTA2026033007436), Mar 27, 2026: FLAP SYSTEM. VIBRATION. DURING DESCENT FOR LANDING IN NORMAL CONFIGURATION; FLAPS & GEAR UP, SPEED BRAKES RETRACTED, 175KTS, BOTH PILOTS FELT A VIBRATION AND ASSOCIATION SOUND WHEN FLA
- [SDR DXTA2025101305263](https://openairdocs.org/sdr/DXTA2025101305263), Oct 10, 2025: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHT SWITCH IN ARM POSITION. ALL EMERGENCY LIGHTS WERE ON IN THE CABIN. TOWARDS THE END OF THE FLIGHT, THE EMERGENCY LIGHTS STARTED TO FLICKER. CORRE
- [SDR DXTA2025071804260](https://openairdocs.org/sdr/DXTA2025071804260), Jul 15, 2025: MICROPHONE. ODOR. COM 1 YELLOW X AS SOON AS WE KEYED THE MIC. SUSPECTED SHORT SMELLED IN COCKPIT ELECTRICAL BURNING SMELL. MM 31-41..05. AFTER ALL WORK COMPLETE, WE FULLY POWERED
- [SDR DXTA2025071404190](https://openairdocs.org/sdr/DXTA2025071404190), Jul 9, 2025: DOOR. OUT OF ADJUST. DOOR IS EXTREMELY DIFFICULT TO CLOSE. ACCOMPLISHED CHECK OF THE MAIN-DOOR INTERNAL HANDLE OPENING AND CLOSING FORCES (AMM TASK 52-11-23-720-801-A/500). INTERNAL
- [SDR DXTA2025070304117](https://openairdocs.org/sdr/DXTA2025070304117), Jul 2, 2025: DOOR. BINDING. ATTEMPTING TO CLOSE THE MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE. MY FO IS PHYSCIALLY UNABLE TO CLOSE THE AIRCRAFT DOOR. CORRECTIVE ACTION: THE ARRIVAL AT THE A
- [SDR DXTA2025040402946](https://openairdocs.org/sdr/DXTA2025040402946), Apr 4, 2025: HANDLE. BINDING. MAIN CABIN ENTRY DOOR, EXTERIOR HANDLE DOES NOT STOW WHEN DOOR IS CLOSED WHEN USING THE INTERIOR LOCK/LATCH HANDLE. PHOTO ATTACHED CORRECTIVE ACTION: INSPECTED 
- [SDR DXTA2025032702826](https://openairdocs.org/sdr/DXTA2025032702826), Mar 26, 2025: HANDLE. LACK OF LUBE. MAIN DOOR HANDLE DIFFICULT TO MOVE. ADJUSTED LOCKING TAB OF DOOR HANDLE AND LUBRICATED MED DOOR HANDLE, OPERATION IS NOW SMOOTH AND REQUIRES LESS EFFORT TO OPEN
- [SDR DXTA2025013102128](https://openairdocs.org/sdr/DXTA2025013102128), Jan 27, 2025: HANDLE. DEFECTIVE. MAIN DOOR: MAIN ENTRY DOOR HANDLE IS BROKEN OFF. UNABLE TO OPEN OR CLOSE DOOR CORRECTIVE ACTION: REPLACED DOOR HANDLE. OPS CHECK GOOD. EMBRAER PHENOM 300 AMM CH
- [SDR DXTA2023090894820](https://openairdocs.org/sdr/DXTA2023090894820), Sep 7, 2023: BATTERY. DEFECTIVE. REPEAT WRITE UP. IN-FLIGHT EMERGENCY, LIGHTS ILLUMINATED, THEN STARTED TO FLICKER. COMPLIED WITH FIM 32-50-00-810-802A INCORRECT FUNCTIONING OF THE EMERGENCY LI
- [SDR DXTA2023081492910](https://openairdocs.org/sdr/DXTA2023081492910), Aug 12, 2023: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: 30 MINUTES INTO FLIGHT UPON LOOKING AFT INTO CABIN WE DISCOVERED THE EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. WE CO
- [SDR DXTA2023042184600](https://openairdocs.org/sdr/DXTA2023042184600), Apr 20, 2023: BRAKE ASSY. INOPERATIVE. RIGHT MLG BRAKE: UPON LANDING WITH A LONG ROLLOUT AND MINIMAL BRAKING. THE RIGHT LANDING GEAR WAS SMOKING FOR OVER TEN MINUTES. NO ADVERSE PULLING OR SHUDDERING
- [SDR DXTA2022112874800](https://openairdocs.org/sdr/DXTA2022112874800), Nov 25, 2022: BATTERY PACK. INOPERATIVE. IN FLIGHT THE CABIN EMERGENCY LIGHTS AS WELL AS THE ENTRY LIGHT IN THE CEILING WERE FLASHING. TURNING THE EMER LIGHT SWITCH TO OFF TURNED THEM OFF. REMOVED & RE
- [SDR DXTA2022072066320](https://openairdocs.org/sdr/DXTA2022072066320), Jul 19, 2022: TORSION BAR. BENT. MAIN DOOR: THE MAIN ENTRY PASSENGER DOOR SLAMS DOWN WHEN OPENING FROM THE INSIDE. THE DOOR ACTUATORS ARE NOT ASSISTING THE MAIN ENTRY DOOR DURING THE OPEN FREE 
- [SDR 2020FA0000444](https://openairdocs.org/sdr/2020FA0000444), Oct 10, 2020: BATTERY PACK. FAILED. DISCREPANCY: IN ZONE 122, COCKPIT EMERGENCY BATTERY FAILED FUNCTIONAL CHECKS AT 18:20 MINUTES. CORRECTIVE ACTION: PERFORMED REPLACEMENT NR 1 (FORWARD) EMERGENCY
- [SDR 2020FA0000443](https://openairdocs.org/sdr/2020FA0000443), Oct 10, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 PART I, II, III (DATED 06/24/2020), WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT E
- [SDR DXTA2020091004078](https://openairdocs.org/sdr/DXTA2020091004078), Sep 10, 2020: DOOR. BINDING. MAIN CABIN DOOR WILL NOT OPEN. CORRECTIVE ACTION, VERIFIED DISCREPANCY, FOUND AFT MAIN CABIN DOOR TRIM LOOSE AND WEDGED BETWEEN DOOR FRAME AND MED CAUSING IT TO
- [SDR DXTA2019080502703](https://openairdocs.org/sdr/DXTA2019080502703), Aug 2, 2019: STARTER GEN. FAILED. GEN 2 OFF BUS YELLOW CAS ILLUMINATED - 45,000 FEET, -65 DEGREES GEN 2 OFF MESSAGE. RAN QRC AND IT WOULDN'T COME BACK ONLINE. DIVERTED TO KIWA. AT APPROXIMATELY 
- [SDR DXTA2016051206240](https://openairdocs.org/sdr/DXTA2016051206240), May 12, 2016: SKIN. DAMAGED. BIRD STRIKE LT WING ROOT, DENT OVER 12" LONG & 3" DEEP. REMAINS IN & AROUND ENG NACELLE. CRACK ON LT OTBD ENG NACELLE. R&R LT WING INBD LE ASSY & PICCOLO TUBE. 

## Service difficulty reports on N373QS not matched to an aircraft (15)

They name N373QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010110504291](https://openairdocs.org/sdr/DXTA2010110504291), Nov 4, 2010: LANDING GEAR. MALFUNCTIONED. AFTER SUCCESSFUL COMPLETION OF 1ST LEG AND 1 COMPLETE CYCLE OF THE GEAR, TOOK OFF ON SECOND LEG. WHEN GEAR HANDLE WAS RAISED GEAR DID NOT COME UP. GEAR CONTROL 
- [SDR DXTA2010070604143](https://openairdocs.org/sdr/DXTA2010070604143), Jul 2, 2010: ANTI-SKID SYS. MALFUNCTIONED. PRESS LIGHT FOLLOWED BY AN ANTI SKID INOP LIGHT. WE LANDED AND USED THE EMERGENCY BRAKING SYSTEM. UNABLE TO DUPLICATE. SERVICED GEAR/ BRAKE ACCUMULATOR. BLED BR
- [SDR DXTA2010051204093](https://openairdocs.org/sdr/DXTA2010051204093), May 11, 2010: THROTTLE CABLE. FAILED. DURING AN OCF FOR THE RT ENG, THE ENG QUIT AFTER PULLING THE POWER LEVER BACK TO IDLE QUICKLY. ALSO, AFTER LANDING IT QUIT AGAIN AFTER A RAPID POWER LEVER REDUC
- [SDR DXTA2009062503699](https://openairdocs.org/sdr/DXTA2009062503699), Jun 23, 2009: THROTTLE CABLE. OUT OF ADJUST. DURING SPEED BRAKE TEST, RT ENGINE SHUTDOWN. NORMAL FORCE USED DURING TEST. (REPEAT WRITE UP). REMOVED RT LWR COWLING ADJUSTED THROTTLE CABLE FRICTION BLOCKS. C
- [SDR DXTA2009062503701](https://openairdocs.org/sdr/DXTA2009062503701), Jun 22, 2009: ENGINE. UNKNOWN. DURING SPEED BRAKE TEST (USING NORMAL FORCE) THE RT ENGINE SHUTDOWN. RAN BOTH ENGINES AND PERFORMED SPEED BRAKE SYS OPS CHECK SEVERAL TIMES WHILE GRADUALLY INCR
- [SDR DXTA20082926](https://openairdocs.org/sdr/DXTA20082926), Mar 9, 2008: UNKNOWN. SMOKE. AFTER TAKE OFF SMOKE SMELL - (NO SIGN OF VISUAL SMOKE) APPEARED.
- [SDR DXTA20082875](https://openairdocs.org/sdr/DXTA20082875), Feb 14, 2008: STARTER GEN. VIBRATION. BUFFETING/GRINDING NOISE INTERMITTENT AT ALL ALTITUDES AND SPEEDS. FOUND STARTER/GENERATOR ON LT ENGINE VIBRATING EXCESSIVELY. REMOVED AND REPLACED GENERATOR IA
- [SDR DXTA200702605](https://openairdocs.org/sdr/DXTA200702605), Nov 11, 2007: SWITCH. MALFUNCTIONED. CABIN DOOR LIGHT ILLUMINATED IN FLIGHT. REMOVED CABIN DOOR SWITCH P/N P18M30 S/N 1020. INSTALLED NEW PART P/N P18M30 S/N 4317. OPERATIONAL AND LEAK CHECK GOOD. 
- [SDR DXTA200601742](https://openairdocs.org/sdr/DXTA200601742), Nov 19, 2006: RESERVOIR. LOW. ALL 4 BRAKE PEDALS TRAVEL ABOUT 2 TO 3 INCHES BEFORE BRAKE PRESSURE CAN BE FELT. PRESSURE AT THAT POINT IS ABOUT 70 PERCENT OF NORMAL. TROUBLESHOT LT AND RT PIL
- [SDR DXTA200400471](https://openairdocs.org/sdr/DXTA200400471), Dec 8, 2004: MASTER CYLINDER. FAILED. COPILOTS BRAKES SPONGY. LEFT PEDAL REQUIRES SIGNIFICANTLY MORE TRAVEL TO ENGAGE BRAKE (ABOUT 2 INCHES). TROUBLESHOT BRAKE SYSTEM A FAULTY CO-PILOT LT BRAKE MAST
- [SDR DXTA200400353](https://openairdocs.org/sdr/DXTA200400353), Aug 3, 2004: PRESSURE VALVE. FAILED. DURING TAXIING THE F/O'S BRAKES FELT SOFT, CAPTAIN'S SIDE WAS GOOD. AFTER TAKEOFF CONTINUED TO OBSERVE BRAKE PRESSURE, ALL NORMAL. AT CRUISE NOTICED A VIBRATION
- [SDR DXTA200400274](https://openairdocs.org/sdr/DXTA200400274), Mar 24, 2004: UPLOCK. MALFUNCTIONED. CLIMBING THROUGH 12,000 FEET AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWED DOWN BELOW 250 KNOTS THEN THE PROBLE
- [SDR DXTA200400174](https://openairdocs.org/sdr/DXTA200400174), Mar 24, 2004: STRUCTURE. NOISY. CLIMBING THROUGH 12,000 FT AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWED DOWN BELOW 250 KNOTS THEN THE PROBLEM 
- [SDR CWQ2004F00001](https://openairdocs.org/sdr/CWQ2004F00001), May 13, 2003: DUCT. CRACKED. DURING ROUTINE INSPECTION LOOKED INTO DORSAL NACA SCOOP AND SAW THE LOWER AIR VANE WITH A 1.5 INCH CRACK STARTING FROM THE CENTER OF THE (V) CUT TOWARD THE OB E
- [SDR 20010613CW020](https://openairdocs.org/sdr/20010613CW020), Jan 10, 2001: HOSE. LEAKING. DURING TEST OF BOTH STATIC SYSTEMS ON AIRCRAFT, FOUND EXCESSIVE STATIC LEAK IN BOTH NR1 AND NR2 SYSTEMS. FOUND STATIC HOSE IN BOTH SIDES LEAKING IN EXCESS OF FA

## 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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