# N352QS: 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: 50500244
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: December 18, 2014
- Certificate issued: January 17, 2025
- Expires: January 31, 2032
- Mode S code: A3EDAA
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=352QS
- Page: https://openairdocs.org/aircraft/N352QS

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 N352QS.

## 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 20251110016109I](https://openairdocs.org/incident/20251110016109I), Nov 10, 2025: Embraer Executive Aircraft Inc EMB-505 (N352QS), Atlanta, GA, Minor damage. On takeoff ingested a bird into the left engine. Maintenance removeed and replace the fan assembly.

## Service difficulty reports (11)

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 DXTA2026062308534](https://openairdocs.org/sdr/DXTA2026062308534), Jun 21, 2026: SHROUD. UNSECURE. AIRCRAFT HAS A MUSTY ODOR WHILE THE VCS OPERATES. ARRIVED TO ACFT AND RAN VCS SYSTEM. MUSTY ODOR COMING OUT OF COCKPIT VENTS. GAINED ACCESS AS NECESSARY TO COCK
- [SDR DXTA2026010706443](https://openairdocs.org/sdr/DXTA2026010706443), Jan 5, 2026: BATTERY. FAULTY. DURING EXTERIOR PREFLIGHT LIGHT CHECK PUT THE EMERGENCY LIGHTS IN THE ON POSITION AND OBSERVED THE EMERGENCY LIGHTS FLASHING. SHUT POWER OFF TO AIRCRAFT AND TUR
- [SDR DXTA2024011910658](https://openairdocs.org/sdr/DXTA2024011910658), Jan 17, 2024: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS STAY ON IN THE ARM POSITION AFTER BOTH ENGINES ARE RUNNING. RESOLUTION: REMOVED EMERGENCY BATTERY I PN 7450LS-00 SN 006361 A
- [SDR DXTA2024010910560](https://openairdocs.org/sdr/DXTA2024010910560), Jan 8, 2024: UNKNOWN. UNKNOWN. EMERG LIGHTS CAME ON DURING FLIGHT IN THE ARM POSITION. LIGHTS STARTED FLICKERING UPON DESCENDING (ABOUT 15 MIN LATER). POWERED UP AIRCRAFT AND DUPLICATED SQUAW
- [SDR DXTA2023050585420](https://openairdocs.org/sdr/DXTA2023050585420), May 3, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS ARE ACTIVATED CONTINUOUSLY WHEN SWITCH IS IN THE ARMED POSITION. STARTED TO FLICKER AS WELL. REMOVED BATTERY NR 1 AND INSTALLED TESTED BATTERY 
- [SDR DXTA2023010377540](https://openairdocs.org/sdr/DXTA2023010377540), Dec 30, 2022: STARTER GEN. DAMAGED. NR 2 GENERATOR FAILED IN FLIGHT CAUSING NR 2 ENGINE TO VIBRATE AND MAKE NOISE, PER THE CHECKLIST WE SHUTDOWN NR 2 ENGINE IN FLIGHT. REMOVED AND INSTALLED OVERHA
- [SDR DXTA2022062764800](https://openairdocs.org/sdr/DXTA2022062764800), Jun 27, 2022: SHROUD. ABNORMAL. MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN. WE CAN ROTATE RED HANDLE OUTSIDE WHICH FEELS NORMAL AND PRESSURE RELIEF FLAP OPENS. THE DOOR WILL THEN ONLY MOVE OUT A
- [SDR DXTA2022052662740](https://openairdocs.org/sdr/DXTA2022052662740), May 25, 2022: BATTERY. DISCHARGED. CABIN EMERG LIGHT: EMERGENCY LIGHTS ON CABIN ARE ALL ONE WHEN THE SWITCH IS IN THE ARMED POSITION. EMERGENCY BATTERIES ARE MOST LIKELY LOW. /// CORRECTIVE ACTIO
- [SDR 2021FA0000265](https://openairdocs.org/sdr/2021FA0000265), Sep 23, 2021: FUSE. FAILED. AFT LIGHT ON THE MAIN DOOR AIRSTAIRS FAILED TO OPERATE DURING THE EMERGENCY LIGHTS OPERATIONAL TEST PER PHENOM 300 AMM 33-52-00. TROUBLESHOT TO OPEN FUSE F0047.
- [SDR EBVR20191014001](https://openairdocs.org/sdr/EBVR20191014001), Oct 14, 2020: BALANCE WEIGHT. CORRODED. RUDDER AND AILERON WEIGHTS FOUND SURFACE CORROSION AND DETERIORATION OF MASS BALANCE WEIGHTS. COMPLIED WITH EMBRAER SB505-55-0004 REV 01. ACCOMPLISHED PART II A
- [SDR DXTA2017012006358](https://openairdocs.org/sdr/DXTA2017012006358), Jan 20, 2017: BRAKE ASSY. MALFUNCTIONED. AFTER LANDING THE BRAKES WERE VERY INEFFECTIVE INITIALLY FROM COPILOT SIDE. THE BRAKES THEN GRABBED VERY AGGRESSIVELY AND THE AIRCRAFT PULLED HARD TO THE LEFT. 

## Service difficulty reports on N352QS not matched to an aircraft (16)

They name N352QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2011020404449](https://openairdocs.org/sdr/DXTA2011020404449), Feb 3, 2011: LANDING GEAR. ICED. MLG UNSAFE LIGHT AFTER RETRACTION, DUE TO ICE AND SLUSH ON TAXI OUT, LT MLG EXTENDED TO 400 FT AGL. UPON SELECTING GEAR UP ACFT YAWED GENTLY TO THE LEFT, RED GE
- [SDR DXTA200802978](https://openairdocs.org/sdr/DXTA200802978), Apr 2, 2008: INDICATOR. FAILED. ABOVE 40 KTS, LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR. INSPECTED GPWS SYSTEM PERFORMED GPWS SELF TEST NO FAULTS FOUND CHECK
- [SDR DXTA20082978](https://openairdocs.org/sdr/DXTA20082978), Apr 2, 2008: INDICATOR. FAILED. ABOVE 40 KTS LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR.
- [SDR DXTA20082891](https://openairdocs.org/sdr/DXTA20082891), Feb 20, 2008: BRAKE ASSY. MALFUNCTIONED. COPILOTS SIDE BRAKES REQUIRE MORE THAN NORMAL PRESSURE TO GET ANY BRAKING. RAN AC WITH ANTI-SKID ON AND OFF CONDUCTING HIGH SPEED STOPS AND MANY MANUVERING TURN
- [SDR DXTA200702505](https://openairdocs.org/sdr/DXTA200702505), Sep 27, 2007: BULB. BURNED OUT. NO GREEN LIGHT ON LT MAIN GEAR DURING GEAR EXTENTION, RAN THE EMERGENCY EXTENTION CHECKLIST. BLOWED GEAR DOWN FOR POSITIVE DOWN AND LOCKED. CREW VERIFIED GREEN 
- [SDR DXTA200702256](https://openairdocs.org/sdr/DXTA200702256), Jun 11, 2007: CONTROL BOX. FAULTED. THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE SAME AMOUNT OF PRESSURE. REMOVED FAULTY A
- [SDR DXTA200702251](https://openairdocs.org/sdr/DXTA200702251), Jun 10, 2007: BRAKE. SEIZED. THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE SAME AMOUNT OF PRESSURE. BLED LT AND RT B
- [SDR DXTA200702163](https://openairdocs.org/sdr/DXTA200702163), Apr 27, 2007: BRAKE ASSY. MALFUNCTIONED. BRAKES NOT WORKING WELL AT SPEEDS ABOVE 5 KNOTS. WITH ANTI SKID OFF BRAKES WORK FINE. [SUP 05-16-07] INSPECTED ANTI SKID WIRING FOUND BAD GROUND FROM P1007 LT W
- [SDR DXTA200601545](https://openairdocs.org/sdr/DXTA200601545), Aug 8, 2006: ELEC CONNECTOR. BROKEN. DURING TAXI OUT OF GSO, CO PILOT SIDE BRAKES BECAME INOP AT APPROX 15 KNOTS FOR ABOUT 5 SECONDS. BRAKES RESPONDED NORMAL AFTER INITIAL LOSS. CHECKED ANTI-SKID B
- [SDR DXTA200601542](https://openairdocs.org/sdr/DXTA200601542), Aug 7, 2006: LINE. LEAKING. ON TAXI OUT OF RAMP. CO-PILOT SIDE BRAKES FAILED. REPEAT WRITE UP. BOTH PEDALS WERE FULLY DEPRESSED TO THE FLOOR WITH NO BRAKING ACTION. INSPECTED ALL MASTER CY
- [SDR DXTA200601509](https://openairdocs.org/sdr/DXTA200601509), Jul 18, 2006: LINE. CONTAMINATED. DURING LANDING (SPEED ,40 KTS) RT BRAKE STOPPED FUNCTIONING. WHEN PUMPED, STARTED FUNCTIONING AGAIN. PROCESS CONFIRMED BY USING BRAKES PEDALS ON RT SIDE. BRAKES
- [SDR DXTA200500567](https://openairdocs.org/sdr/DXTA200500567), Jan 30, 2005: POWER CABLE. OUT OF RIG. ON LANDING THE POWER LEVERS WERE BROUGHT TO IDLE AND LEFT ENGINE FAILED (AT IDLE). ADJUSTED FLOW DIVIDER TO FUEL CONTROL INTERCONNECT ROD FOR PROPER IDLE DETENT
- [SDR DXTA200500540](https://openairdocs.org/sdr/DXTA200500540), Jan 17, 2005: TAB. BENT. APPARENT PARTIAL THRUST REVERSER DEPLOYMENT AT CRUISE FLIGHT 30,000 FT. RIGHT UNLOCK LIGHT WAS ON, DEPLOY LIGHT DID NOT LIGHT. RUMBLING AND DECELERATION WAS FEL
- [SDR DXTA200400288](https://openairdocs.org/sdr/DXTA200400288), Apr 4, 2004: CONTROL CABLE. OUT OF RIG. LEFT ENGINE FLAMED OUT AFTER DOING PREFLIGHT WING SPOILER CHECK. INSPECTED LEFT ENGINE CONTROLS AT FUEL CONTROL UNIT AND ACCOMPLISHED ENGINE POWER CONTROLS CHEC
- [SDR CWQ2004F00004](https://openairdocs.org/sdr/CWQ2004F00004), Aug 28, 2003: LINE. MISMANUFACTURED. DURING ROUTINE MAINT, A FUEL LEAK WAS BEING WORKED IN RT WING AREA FORWARD OF MLG. DURING INSTALLATION OF PLUMBING WHICH WAS REMOVED FOR ACCESS A LINE WAS DAMAG
- [SDR DXTA200300038](https://openairdocs.org/sdr/DXTA200300038), Jun 1, 2003: LAMP. INOPERATIVE. DID NOT GET 3 GREEN LIGHTS UPON GEAR EXTENSION. RAN CHECKLIST AND CONFIRMED DOWN AND LOCKED. BLEW EMERGENCY BOTTLE TO COMPLETE CHECKLIST. RT MAIN GEAR DID NOT I

## 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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