# N395QS: 2016 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: 50500365
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: August 22, 2016
- Certificate issued: July 6, 2026
- Expires: July 31, 2033
- Mode S code: A496CB
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=395QS
- Page: https://openairdocs.org/aircraft/N395QS

From the FAA registry file of October 29, 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 N395QS.

## FAA accident and incident reports

None matched to N395QS.

## Service difficulty reports (13)

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 DXTA2025111705702](https://openairdocs.org/sdr/DXTA2025111705702), Nov 15, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY EXIT SIGN OVER MAIN ENTRANCE DOOR IS NOT WORKING. REMOVED THE EMERGENCY EXIT SIGN OVER MED & FOUND THE ELECTRICAL CONNECTOR WAS JAMMED BETWEEN OVERHEA
- [SDR DXTA2025102005318](https://openairdocs.org/sdr/DXTA2025102005318), Oct 15, 2025: STRUT. FAULTY. REPEAT WRITEUP. HIGH PITCH NOISE FROM NOSE GEAR ON GROUND DURING HIGH SPEEDS. NO SHIMMY OR VIBRATION OR DIRECTIONAL CONTROL PROBLEMS NOTED. POST FLIGHT REVEALS 
- [SDR DXTA2025060903799](https://openairdocs.org/sdr/DXTA2025060903799), Jun 6, 2025: BRAKE ASSY. DEFECTIVE. THE AIRCRAFT IS PULLING VERY HARD TO THE RIGHT ON EACH LANDING AND CONTINUES TO PULL HARDER. REMOVED AND REPLACED RH BRAKE ASSEMBLY IAW PHENOM 300 AMM 32-40-00.
- [SDR DXTA2025012102048](https://openairdocs.org/sdr/DXTA2025012102048), Jan 20, 2025: LIGHT. INOPERATIVE. MAIN EXIT SIGN/LIGHT: THE EMERGENCY EXIT LIGHT OVER THE MAIN CABIN DOOR, ON THE INSIDE OF THE AIRCRAFT IS INOP AND NOT ILLUMINATING. PERFORMED EMERGENCY BATTERY
- [SDR DXTA2024050911713](https://openairdocs.org/sdr/DXTA2024050911713), May 8, 2024: BATTERY. FAULTED. EMERGENCY LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. THEY LATER STARTED FLICKERING. EMERGENCY LIGHTS TURN OFF WITH SWITCH IN OFF POSITION. REMOVED #1 EMERG
- [SDR DXTA2024030511075](https://openairdocs.org/sdr/DXTA2024030511075), Mar 2, 2024: FLAG. OBSTRUCTED. LOWER DOOR LOCK INDICATION FLAG IS NOT VISIBLE. LOOKS LIKE IT IS OBSTRUCTED BY SOMETHING BLUE IN COLOR. VERIFIED THAT THERE IS SOMETHING IN FONT OF FLAG IT LOOK
- [SDR DXTA2023092896710](https://openairdocs.org/sdr/DXTA2023092896710), Sep 28, 2023: BATTERY. FAILED. ON TAXI OUT WHILE IN "ARM" THE EMERGENCY LIGHTING SYSTEM STARTED TO FLASH. VERIFIED FAULT. WHEN SELECTED TO ARM LIGHTS CAME ON & STAYED ON. DISCHARGED UNTIL LIG
- [SDR DXTA2023081793360](https://openairdocs.org/sdr/DXTA2023081793360), Aug 17, 2023: BATTERY. DEFECTIVE. CABIN EMERGENCY LIGHTS ARE "ON" WITH THE SWITCH IN THE ARMED POSITION. GAINED ACCESS TO A/C AND WE ARE ABLE TO DUPLICATE DISCREPANCY. VISUAL INSPECTED (CIRCUIT 
- [SDR DXTA2023070390140](https://openairdocs.org/sdr/DXTA2023070390140), Jul 3, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: EMERGENCY EXIT LIGHTS IN CABIN BEGAN BLINKING IN FLIGHT AND THEN CAME ON STEADY. SWITCH WAS IN THE ARM POSITION THE ENTIRE TIME. REMOVED #2 E
- [SDR DXTA2021102550760](https://openairdocs.org/sdr/DXTA2021102550760), Oct 22, 2021: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: EMERGENCY LIGHTS TURN ON AND INTERMITTENTLY FLASH ON AND OFF WITH SWITCH IN "ARMED" POSITION. //SIGNOFF// REMOVED AND REPLACED THE FWD EMERG
- [SDR DXTA2018033000783](https://openairdocs.org/sdr/DXTA2018033000783), Mar 30, 2018: UNKNOWN. ODOR. UNFAMILIAR ODOR NOTICED ABOVE 10,000 FEET. WENT AWAY FOR A WHILE THEN IT CAME BACK WHEN ABOUT TO LEVEL OFF AT FLIGHT LEVEL 410. ODOR SMELLS LIKE BURNING OIL COM
- [SDR DXTA2018032400758](https://openairdocs.org/sdr/DXTA2018032400758), Mar 23, 2018: PRECOOLER. FAILED. BLEED 1 FAIL YELLOW CAS ILLUMINATED, CLIMBING THROUGH APPROXIMATELY 16,000 FT IN ICING CONDITIONS WITH WING AND ENGINE ANTI-ICE SWITCHES SELECTED ON. AFFECTED B
- [SDR DXTA2018031900726](https://openairdocs.org/sdr/DXTA2018031900726), Mar 16, 2018: INTERFACE UNIT. FAULTED. MULTIPLE AIRFRAME AND ENGINE CAS MESSAGES IN-FLIGHT INCLUDING, LG LEVER DISAG, E1 TTO HTR FAIL, PRESN AUTO FAIL, OXY LOW PRES, A-I E2 ON, A-I E1 ON, SWPS ICE SP

## Service difficulty reports on N395QS not matched to an aircraft (11)

They name N395QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010083004210](https://openairdocs.org/sdr/DXTA2010083004210), Aug 29, 2010: SQUAT SWITCH. FAILED. ANTI SKID LIGHT ILLUM INFLT AT 35000. LIGHT WENT OUT AFTER ABOUT A MIN. CAME BACK ON 5 MIN LATER & STAYED ON UNTIL SWITCH TURNED OFF. FOUND SQUAT SWITCH DISAGRE
- [SDR DXTA2010040504059](https://openairdocs.org/sdr/DXTA2010040504059), Apr 2, 2010: LANDING GEAR. MALFUNCTIONED. LT MAIN GEAR DID NOT RETRACT ON TAKEOFF (CONFIRMED BY INDICATOR LIGHTS, TOWER AND WIND NOISE). AFTER ABOUT 2 MIN RETRACTED BY ITSELF, WITHOUT US CYCLING THE GEA
- [SDR DXTA2010032304045](https://openairdocs.org/sdr/DXTA2010032304045), Mar 21, 2010: LANDING GEAR. MALFUNCTIONED. ON DEPARTURE WHEN GEAR HANDLE SELECTED TO UP, THERE WAS A SIGNIFICANT NOSE GEAR RETRACTION DELAY. THE NOSE GEAR GREEN DOWN INDICATOR REMAINED ILLUMINATED AND RE
- [SDR DXTA2009090803776](https://openairdocs.org/sdr/DXTA2009090803776), Sep 6, 2009: SWITCH. SHORTED. AT T/R DEPLOYMENT ON LANDING ROLL, A SPARK CAME FROM THE EMER\STOW SWITCH AREA. A SLIGHT ELECTRICAL ODOR WAS PRESENT. RT SIDE T/R EMER/STOW SWITCH. REMOVED AND 
- [SDR DXTA200803120](https://openairdocs.org/sdr/DXTA200803120), Jun 14, 2008: BULB. INOPERATIVE. LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE SELECTED DOWN ON LANDING. VERIFIED BULB INOP ON LT GEAR INDICATION REMOVED ALL GEAR INDICATING BULBS 
- [SDR DXTA200702028](https://openairdocs.org/sdr/DXTA200702028), Mar 16, 2007: BRAKE ASSY. WEAK. BRAKES ARE MUSHY THROUGH THE FIRST 75 PERCENT OF PRESSURE APPLICATION. DON'T START TO FEEL BRAKING UNTIL PAST THE 75 PERCENT MARK. IMPROVES SLIGHTLY IF YOU PUMP
- [SDR DXTA200601199](https://openairdocs.org/sdr/DXTA200601199), Jan 16, 2006: WIRE. BROKEN. AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. LANDING GEAR IN RETRACT POSITION. POSITIONED GEAR HANDLE TO AGREE WITH GEAR POSITION, VERIFIED GEAR DOWN WITH THRO
- [SDR DXTA200500978](https://openairdocs.org/sdr/DXTA200500978), Sep 19, 2005: ANTI-SKID SYS. MALFUNCTIONED. UPON LANDING, EXPERIENCED "HARD PEDALS" AND NO BRAKES FOR ABOUT 6 SECONDS. JUST BEFORE USING EMER BRAKING THE BRAKES SUDDENLY GRABBED VIOLENTLY. AFTER THAT THEY
- [SDR DXTA200500976](https://openairdocs.org/sdr/DXTA200500976), Sep 19, 2005: BRAKE. MALFUNCTIONED. UPON LANDING, EXPERIENCED "HARD PEDALS" AND NO BRAKES FOR ABOUT 6 SECONDS. JUST BEFORE USING EMER BRAKING THE BRAKES SUDDENLY GRABBED VIOLENTLY. AFTER THAT THEY
- [SDR DXTA200400244](https://openairdocs.org/sdr/DXTA200400244), Feb 16, 2004: LANDING GEAR. INOPERATIVE. AFTER TAKEOFF COULD NOT RETRACT LANDING GEAR, DIVERTED AIRCRAFT TO SUA. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200400236](https://openairdocs.org/sdr/DXTA200400236), Feb 2, 2004: BRAKE ASSY. MALFUNCTIONED. UPON TOUCH DOWN AND INITIAL APPLICATION OF BRAKES, CAPTAIN’S SIDE HAD POSITIVE BRAKE PRESSURE BUT AIRCRAFT WOULD NOT SLOW DOWN. AFTER APPLICATION OF EXCESSIVE B

## 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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