# N386QS: 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: 50500309
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: November 16, 2015
- Certificate issued: September 2, 2025
- Expires: September 30, 2032
- Mode S code: A47303
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=386QS
- Page: https://openairdocs.org/aircraft/N386QS

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 N386QS.

## 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 20260521004589I](https://openairdocs.org/incident/20260521004589I), May 21, 2026: Embraer Executive Aircraft Inc EMB-505 (N386QS), Miami, FL, Minor damage. The aircraft struck a bird on landing rollout causing minor damage to the right-wing leading edge.

## Reports on N386QS not matched to an aircraft (1)

They name N386QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20011116038069I](https://openairdocs.org/incident/20011116038069I), Nov 16, 2001: Cessna 560CESSNA (N386QS), Fort Wayne, IN. (-23) Engine removed and sent to pratt & whitney Canada for teardown and no report has been received as of this date. A/c experienced engine failure during…

## Service difficulty reports (23)

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 DXTA2026082609410](https://openairdocs.org/sdr/DXTA2026082609410), Aug 23, 2026: LANDING GEAR. LACK OF LUBE. ON TAKE OFF ROLL, RIGHT ABOUT V1, THE PLANE JERKED VIOLENTLY TO THE LEFT. WE KEPT PLANE UNDER CONTROL AND ROTATED. IT DID NOT DO ANYTHING ODD ON LANDING. WE ALS
- [SDR DXTA2026032707403](https://openairdocs.org/sdr/DXTA2026032707403), Mar 25, 2026: LIGHT. DEFECTIVE. WHILE CHECKING THE EMERGENCY LIGHTS THERE WERE 3 RED LIGHTS AND 3 WHITE LIGHTS FOR THE FLOOR ESCAPE PATH LIGHTS. THERE ARE SUPPOSED TO BE 4 WHITE LIGHTS AND THE
- [SDR DXTA2026031207224](https://openairdocs.org/sdr/DXTA2026031207224), Mar 11, 2026: AHRS. FAILED. AHRS 2 FAIL AT 32000', ACCOMPANIED BY AP FAIL AND YD FAIL. PFD 2 AUTO REVERTED TO AHRS 1. AFTER SEVERAL MINUTES AHRS 2 FAIL CAS CLEARED. POSSIBLY ASSOCIATED, AH
- [SDR DXTA2026010506418](https://openairdocs.org/sdr/DXTA2026010506418), Jan 3, 2026: LIGHT. INOPERATIVE. DURING PREFLIGHT LIGHT CHECK, THE CENTER FLOOR EMERGENCY LIGHT WAS FOUND TO BE NOT LIT UP. REPLACED CENTER FLOOR EMERGENCY LIGHT DUE TO LIGHT BEING INOP. REPLAC
- [SDR DXTA2025102705400](https://openairdocs.org/sdr/DXTA2025102705400), Oct 22, 2025: UNKNOWN. ODOR. NOTICED OIL/GREASE ODOR UPON TAKEOFF UNTIL LEVEL OFF (STRONG) AND THEN INTERMITTENTLY THE REST OF FLIGHT (FAINT). REPOSITIONED AIRCRAFT OUT OF HANGAR, RAN ENGIN
- [SDR DXTA2025101705320](https://openairdocs.org/sdr/DXTA2025101705320), Oct 15, 2025: UNKNOWN. ODOR. JUST PRIOR TO DECENT & THEN DURING DESCENT, A SLIGHT ELECTRICAL METALLIC ODOR WAS PRESENT IN COCKPIT. COULD NOT TELL WHERE IT WAS COMING FROM. THERE WAS NO SMOK
- [SDR DXTA2025091104918](https://openairdocs.org/sdr/DXTA2025091104918), Sep 11, 2025: PDU. DEFECTIVE. FLAP FAIL YELLOW CAS DISPLAYED ON APPROACH. RUNNING THE QRH FAILED TO RESTORE OPERATION. THEY APPEAR TO BE STUCK AT THE FLAPS 1 POSITION GAINED ACCESS TO AIRCRA
- [SDR DXTA2024071012313](https://openairdocs.org/sdr/DXTA2024071012313), Jul 9, 2024: BATTERY. DISCHARGED. WHEN ARMING LIGHTS ON GROUND DURING BEFORE START FLOW, LIGHTS MOMENTARILY ILLUMINATE AND THEN EXTINGUISH PERFORMED FIM 33-50-00-810-801 AND FOUND THE BATTERIES 
- [SDR DXTA2023082393720](https://openairdocs.org/sdr/DXTA2023082393720), Aug 23, 2023: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY ASSY IAW PHENOM 300 AMM CH 33-52-01. OPERATIONAL CH
- [SDR DXTA2023070390180](https://openairdocs.org/sdr/DXTA2023070390180), Jul 3, 2023: UNKNOWN. UNKNOWN. ENTRANCE STAIR EXTENSION: THE ENTRY DOOR SLAMS OPEN WITH ZERO TENSION TO SUPPORT IT//CORRECTIVE ACTION//CHECKED ALL HARDWARE AND CABLES AND VERIFIED NO BROKEN C
- [SDR DXTA2023031082320](https://openairdocs.org/sdr/DXTA2023031082320), Mar 10, 2023: NONE. NONE. EMERG EXIT SIGN/LIGHT: EMER EXIT SIGN LIGHT ABOVE THE EXIT WINDOW IS NOT WORKING. NO BULBS LIGHT UP WHEN THE EMER LIGHT SWITCH IS ON.//CORRECTIVE ACTION// FOUND
- [SDR DXTA2023011678500](https://openairdocs.org/sdr/DXTA2023011678500), Jan 14, 2023: ROD. FROZEN. MAIN ENTRANCE DOOR BINDING WHILE OPENING AND CLOSING. UPON ARRIVAL FOUND MAIN CABIN DOOR OPERATING NORMALLY FROM OUTSIDE AND INSIDE AIRCRAFT, NO DEFECTS NOTED. 
- [SDR DXTA2022121576200](https://openairdocs.org/sdr/DXTA2022121576200), Dec 14, 2022: BATTERY PACK. DEFECTIVE. EMERG EXIT SIGN/LIGHT: WHITE EXIT LIGHT ADJACENT TO THE MAIN ENTRANCE DOORWAY WILL NOT ILLUMINATE. REPLACED EMER EXIT LIGHT ASSV IAW EMB 505 AMM 33-52-13. OPS C
- [SDR DXTA2022112875040](https://openairdocs.org/sdr/DXTA2022112875040), Nov 28, 2022: SUPPORT. DEFECTIVE. MAIN CABIN ENTRY DOOR CABLE INOPERATIVE. LOUD BANG WAS HEARD AND BOTH CABLES WENT SLACK. UNABLE TO CLOSE DOOR FROM THE INSIDE DUE TO EXCESSIVE WEIGHT. REMOVED A
- [SDR DXTA2022080467310](https://openairdocs.org/sdr/DXTA2022080467310), Aug 3, 2022: NONE. NONE. CABIN EMERG LIGHT: EMER LT FLICKERS CONSTANTLY ON THE ARM AND ON POSITION
- [SDR DXTA2022072566650](https://openairdocs.org/sdr/DXTA2022072566650), Jul 24, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS ARE ON AND STAY ON WITH THE SWITCH IN THE ARMED POSITION // SIGNOFF // REMOVED FUALTY EMERGENCY BATTERY AND REPLACED W
- [SDR 2021FA0000022](https://openairdocs.org/sdr/2021FA0000022), Jan 26, 2021: POWER CABLE. DAMAGED. DISCREPANCY: AFT BAGGAGE COMPRESSOR DRIVE MODULE POSITIVE POWER CABLE ELECTRICALLY DAMAGED AND RUBBED ON BELOW RIB. CORRECTIVE ACTION: AFTER AEROSPACE QUALITY R
- [SDR DXTA2019061762504](https://openairdocs.org/sdr/DXTA2019061762504), Jun 16, 2019: O-RING. LEAKING. AROUND FL350 WE GOT A HYDRAULIC SYSTEM FAULT STATUS MSG, FOLLOW BY A NO DISPATCH STATUS MSG. DECENDING THROUGH FL240 THE NUMBER 1(LEFT) ENGINE FAILED. NO FIRE O
- [SDR 2017FA0000650](https://openairdocs.org/sdr/2017FA0000650), Dec 15, 2017: WIRE. SHORTED. UPON INSPECTION OF RH COCKPIT AREA FOUND SPLICE SP1474 AND SP4273 BURNT AND FUSED TOGETHER. ALSO FOUND WIRES W201-11086-16 AND W201-11087-16 BURNT AND DAMAGED F
- [SDR 2017FA0000652](https://openairdocs.org/sdr/2017FA0000652), Dec 14, 2017: TORQUE TUBE. LOOSE. COPILOT RUDDER PEDAL TORQUE TUBE BASE SHOWS MOVEMENT WHEN FORCE IS APPLIED TO THE RUDDER PEDALS ON THE COPILOT SIDE. AN ABNORMAL SOUND IS HEARD AND THE MOUNTING
- [SDR DXTA2017061706412](https://openairdocs.org/sdr/DXTA2017061706412), Jun 17, 2017: PUMP. INOPERATIVE. HYDRAULIC LOW PRESSURE CASS MESSAGE . ALONG WITH PUSHER FAIL, BRAKE FAIL CASS MESSAGES IN FLIGHT. REMOVED AND REPLACED THE LT ENGINE HYD PUMP IAW AMM 29-12-01. 
- [SDR DXTR2016F00136](https://openairdocs.org/sdr/DXTR2016F00136), Jun 8, 2016: GEAR. CRACKED. THIS AIRCRAFT WAS IN THE PROCESS OF MAINTENANCE FOR A PASSENGER DOOR ISSUE. UPON REMOVAL OF THE ACFT MAIN PASSENGER DOOR AND SUBSEQUENT RE-INSTALLATION AND RIGG
- [SDR DXTA2016021006182](https://openairdocs.org/sdr/DXTA2016021006182), Feb 10, 2016: WARNING SYSTEM. ACTIVATED. WHILE EN-ROUTE AT FL400 WE RECEIVED THE WHITE CAS MSG AHARS 1 & 2 FAULT. UNDER THE MSG PAGE ON THE GTC WAS INDICATING GPS NAVIGATION SIGNALS WERE LOST. APPROX 1

## Service difficulty reports on N386QS not matched to an aircraft (3)

They name N386QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR JGVR20201214001](https://openairdocs.org/sdr/JGVR20201214001), Dec 14, 2020: SPAR CAP. CORRODED. REMOVED EXISTING HI-LOC FASTENERS AND BLENDED CORRODED AREA OF THE LT AFT WING SPAR LOWER CLIP LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL. PERFORMED NDT AND
- [SDR DXTA200802854](https://openairdocs.org/sdr/DXTA200802854), Feb 8, 2008: BRAKE ASSY. WEAK. CO PILOTS RT BRAKE PEDAL SOFT, PRESSURE DROPS DURING BRAKING. PERFORMED ANTI-SKID BRAKE SYS BLEED PROCEDURE. BRAKES CHECK GOOD AT THIS TIME. NO PRESSURE DROP NO
- [SDR DXTA200802805](https://openairdocs.org/sdr/DXTA200802805), Jan 28, 2008: HOSE. LEAKING. F/O'S BRAKE PEDALS ARE SOFT. INSPECTED SYS AND FOUND UPPER (SUPPLY) HOSE OF CO-PILOTS RT MASTER CYLINDER BRAIDING BROKEN AND FRAYED. ALSO FOUND SWIVEL FITTING F

## 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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