# N360QS: 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: 50500254
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: February 23, 2015
- Certificate issued: August 17, 2026
- Expires: August 31, 2033
- Mode S code: A40DBB
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=360QS
- Page: https://openairdocs.org/aircraft/N360QS

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 N360QS.

## FAA accident and incident reports

None matched to N360QS.

## Service difficulty reports (17)

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 DXTA2026042107697](https://openairdocs.org/sdr/DXTA2026042107697), Apr 19, 2026: PIN. DISENGAGED. AFTER 1ST NR 2 ENGINE START, PAX DOOR OPEN CAS MSG ILLUMINATED. ATTEMPTED NUMEROUS TRYS OPENING & CLOSING THE DOOR. NO VISIBLE OBSTRUCTIONS. FROM INSIDE, IT APP
- [SDR DXTA2025110305485](https://openairdocs.org/sdr/DXTA2025110305485), Oct 28, 2025: BATTERY PACK. INOPERATIVE. CABIN EMERGENCY LIGHTS WERE FLASHING IN FLIGHT IN THE ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES IAW AMM 33-52-01. OPS TEST CHECKED GOOD
- [SDR DXTA2025032402766](https://openairdocs.org/sdr/DXTA2025032402766), Mar 20, 2025: DRAIN. DEFECTIVE. FUSELAGE DRAIN: BETWEEN 12000 AND 16000, WE EXPERIENCED A SUDDEN ONSET VIBRATION SEEMINGLY ORIGINATING FROM THE FLOOR AREA NEAR THE COCKPIT. WE COULD HEAR A LOU
- [SDR DXTA2024111501120](https://openairdocs.org/sdr/DXTA2024111501120), Nov 11, 2024: SEAL. SEPARATED. ABOVE FL 180, IN LEVEL FLIGHT, 300KTS OR ABOVE INDICATED, LOUD ACOUSTIC HUM FROM MID CABIN, RIGHT SIDE. ALSO A SLIGHT VIBRATION CAN BE FELT THERE TOO, ABOVE FL 
- [SDR DXTA2024092600650](https://openairdocs.org/sdr/DXTA2024092600650), Sep 23, 2024: BATTERY. MALFUNCTIONED. ABOUT 15 MINUTES PRIOR TO LANDING ALL THE EMERGENCY LIGHTS IN THE CABIN BEGAN TO FLICKER AND CONTINUED ALL THE WAY THROUGH SHUT DOWN. WE CHECKED AGAIN ON THE GR
- [SDR DXTA2023122610433](https://openairdocs.org/sdr/DXTA2023122610433), Dec 24, 2023: UNKNOWN. UNKNOWN. DURING TAKEOFF, CREW NOTICED A LOUD SQUEAL COMING FROM THE AREA NEAR THE EMERGENCY OVER WING EXIT. TECHS SET UP FOR ENG RUN. AFTER ENGINES ARE STARTED, WE PRESS
- [SDR DXTA2023032783260](https://openairdocs.org/sdr/DXTA2023032783260), Mar 27, 2023: UNKNOWN. UNKNOWN. CLIMBING THRU 29,000 FT, RECEIVED BLD 1 LEAK CAS IND. FOLLOWED QRH, REDUCE POWER NR 1 ENG & WAITED 3 MINS FOR MESGE TO EXTING. 3 MINS, MESGE EXTINGUISH. RETURNE
- [SDR DXTA2023031682700](https://openairdocs.org/sdr/DXTA2023031682700), Mar 15, 2023: ROD. DAMAGED. MAIN DOOR TELESCOPING ROD: TELESCOPING ROD MOUNT BROKEN. COMPLIED WITH THE ETD2022-P300-04650764 AND INSTALLED NEW TELESCOPIC ROD FITTING P/N 500-09754-001 S/N 
- [SDR DXTA2022121976400](https://openairdocs.org/sdr/DXTA2022121976400), Dec 16, 2022: DOOR LATCH. BROKEN. MAIN DOOR HANDLE: TEFLON SLIDER BEHIND MAIN ENTRY HANDLE FALL OFF // SIGNOFF// REMOVED FAULTY MAIN DOOR EXTERNAL HANDLE PN: UKN. INSTALLED NEW MAIN DOOR EXTERIO
- [SDR DXTA2022112274190](https://openairdocs.org/sdr/DXTA2022112274190), Nov 21, 2022: WIRE HARNESS. MISROUTED. BEFORE ENGINE START, AFTER CLOSING MAIN CABIN DOOR, RED PASSENGER DOOR WARNING REMAINED ILLUMINATED. DOOR LOCK FLAGS (2) ARE NOT VISIBLE ON MAIN CABIN DOOR. FOU
- [SDR DXTA2022071866110](https://openairdocs.org/sdr/DXTA2022071866110), Jul 15, 2022: LENS. MISSING. MAIN DOOR VISUAL INDICATOR: LOCK INDICATOR LENS MISSING, WHEN VIEWED WITH DOOR OPEN, LOCATED FORWARD AND MIDWAY ON DOOR. *** CORRECTIVE ACTION *** FOUND DOOR IN
- [SDR DXTA2022033059250](https://openairdocs.org/sdr/DXTA2022033059250), Mar 30, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR: MAIN ENTRY DOOR "HANGS UP" ABOUT THE HALFWAY OPEN POINT. DOOR IS DIFFICULT TO OPEN THE REMAINDER OF THE WAY WITH THE RED HANDLE. STANDING ON THE TOP 
- [SDR DXTA2022013155970](https://openairdocs.org/sdr/DXTA2022013155970), Jan 30, 2022: ROD. DEFECTIVE. MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN OR CLOSE PROPERLY. DOOR GETS STUCK HALFWAY THROUGH ITS TRAVEL GOING UP OR DOWN. // SIGNOFF // REPLACED AFT PASSENGER DO
- [SDR DXTA2021013104658](https://openairdocs.org/sdr/DXTA2021013104658), Jan 31, 2021: BATTERY PACK. DEPLETED. CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT WITH THE EMER LT SWITCH IN ARM. CORRECTIVE ACTION: REMOVED FWD EMER BATTERY P/N 6450LS-00, S/N 001098 AND AFT EMERGENC
- [SDR JGVR202011180001](https://openairdocs.org/sdr/JGVR202011180001), Nov 18, 2020: BALANCE WEIGHT. DAMAGED. WHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHT TO NOT MEET SB SPECIFICATIONS AND REQUIRING REPLACEMENT: ONE LT EL
- [SDR DXTA2018062000194](https://openairdocs.org/sdr/DXTA2018062000194), Jun 20, 2018: SUPPORT ROD. BROKEN. DURING THE TAIL CONE REMOVAL FOR ELEVATOR CONTROL CABLE INSPECTION FOUND THE LT ROD ASSY FOR THE RUDDER TORQUE TUBE DAMAGED. PN AFFECTED WAS 3836-2.
- [SDR DXTA2015102606113](https://openairdocs.org/sdr/DXTA2015102606113), Oct 25, 2015: UNKNOWN. ODOR. NOTED A STRONG ODOR FROM PRESSURIZATION SYS WHEN ENGS STARTED & VERY LOUD ROARING SOUND DURING TAKEOFF, CLIMB OUT, DESCENT & LANDING. PERFORMED ENG RUNS & PRESS

## Service difficulty reports on N360QS not matched to an aircraft (8)

They name N360QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010021703991](https://openairdocs.org/sdr/DXTA2010021703991), Feb 16, 2010: FLEX LINE. LEAKING. UPON LANDING, DEPRESSED BRAKES AND POWER BRAKE LOW PRESS LIGHT CAME ON AND ANTI SKID INOP LIGHT CAME ON. BRAKES WENT TO THE FLOOR. HAD TO USE THE EMERGENCY RED 
- [SDR DXTA2009052803667](https://openairdocs.org/sdr/DXTA2009052803667), May 27, 2009: STRUCTURE. DENTED. DURING POSTFLIGHT, DISCOVERED DENT IN LT ENGINE PYLON. EVALUATED DAMAGE. REMOVED PYLON LEADING EDGE. INSTALLED NEW LEADING EDGE WITH SEALANT AND RIVETS. PRIMED 
- [SDR DXTA2008121103397](https://openairdocs.org/sdr/DXTA2008121103397), Dec 11, 2008: GYRO. INOPERATIVE. DURING TAKEOFF ROLL AT 50 KIAS, RED "HDG" FLAGS APPEARED ON CAPTAIN PFD, MFD, AND SIMULTANEOUSLY ON STBY HSI. AFTER 15 SECONDS RED FLAGS DISAPPEARED AND HEADING
- [SDR DXTA2008121203397](https://openairdocs.org/sdr/DXTA2008121203397), Dec 11, 2008: INDICATOR. MALFUNCTIONED. DURING TAKEOFF ROLL AT 50 KIAS, RED "HDG" FLAGS APPEARED ON CAPTAIN PFD, MFD, AND SIMULTANEOUSLY ON STBY HSI.
- [SDR DXTA200702211](https://openairdocs.org/sdr/DXTA200702211), May 22, 2007: CONTROL SYSTEM. OUT OF RIG. AT FL 280 AND 275 KTS RECEIVED AMBER ANNUNCIATOR (AP PITCH MIS-TRIM) AND (TRIM DN), MANUALLY DISCONNECTED AUTOPILOT AND ATTEMPTED TO TRIM DOWN MANUALLY AND ELEC
- [SDR DXTA200601583](https://openairdocs.org/sdr/DXTA200601583), Aug 30, 2006: LINE. LEAKING. PILOT'S LEFT BRAKE HAS TENDENCY TO GRAB WHILE TAXING WITH MINIMAL PEDAL PRESSURE. CO-PILOT BRAKES MUST BE DEPRESSED 2 - 3 INCHES BEFORE ANY PRESSURE IS FELT. BL
- [SDR DXTA200601362](https://openairdocs.org/sdr/DXTA200601362), Apr 25, 2006: HOOK. OUT OF POSITION. AFTER RAISING GEAR RED GEAR UNLOCKED LIGHT AND AMBER HYDRAULIC PRESS ON REMAINED ILLUMINATED. PERFORMED RESISTANCE CHECKS ON LT AND RT UPLOCK SWITCHES. BOTH CHE
- [SDR DXTA200500964](https://openairdocs.org/sdr/DXTA200500964), Sep 12, 2005: RUDDER PEDAL. ERRATIC. REPEAT WRITE UP. ON DESCENT INTO TEB, RUDDER PEDALS WOULD JERK RIGHT AND LEFT. SEEMS TO BE HAPPENING WHEN AFIS SENDS AND RECEIVES.

## 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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