# N393QS: 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: 50500356
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: June 28, 2016
- Certificate issued: March 23, 2026
- Expires: March 31, 2033
- Mode S code: A48F5D
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=393QS
- Page: https://openairdocs.org/aircraft/N393QS

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 N393QS.

## FAA accident and incident reports

None matched to N393QS.

## Service difficulty reports (12)

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 DXTA2025122606275](https://openairdocs.org/sdr/DXTA2025122606275), Dec 23, 2025: BRAKE ASSY. WEAK. WHILE AT TAXI SPEED BRAKES BECOME SPONGY AND REQUIRES A LOT MORE PRESSURE TO STOP. BRAKES ACT NORMALLY DURING LANDING. PERFORMED BRAKE BLEED, PERFORMED TAXI RUN
- [SDR DXTA2025012202059](https://openairdocs.org/sdr/DXTA2025012202059), Jan 20, 2025: HANDLE. DEFECTIVE. WHILE CLOSING MAIN DOOR, OUTSIDE DOOR HANDLE BROKE OFF. CORRECTIVE ACTION: REPLACED DOOR HANDLE. OPS CHECK GOOD. IAW EMB-505 AMM 52-11-24
- [SDR DXTA2024121101427](https://openairdocs.org/sdr/DXTA2024121101427), Dec 7, 2024: BATTERY. FAULTED. AFTER DEPARTURE ENROUTE WE SHUT OFF THE CABIN LIGHTS AND NOTICED THAT THE EMERGENCY LIGHTS STAYED ON. IF WE SELECT THE EMER LIGHTS TO OFF THEY WILL GO OUT BUT C
- [SDR DXTA2024071612361](https://openairdocs.org/sdr/DXTA2024071612361), Jul 15, 2024: CONTROL UNIT. DEFECTIVE. BRAKES PULSATING ON LANDING &TAXI. PER CRC RECOMMENDATION, PERFORMED A VISUAL INSP OF BRAKE SYS & NO FAULTS. BLED HYD SYS. CHECKED & FOUND HYD SYS PROPERLY SERV
- [SDR DXTA2024052311844](https://openairdocs.org/sdr/DXTA2024052311844), May 22, 2024: SHUTOFF VALVE. FAULTED. RECEIVED ECS VALVE FAIL MESSAGES, FOLLOWED THE QRC, AND DURING DESCENT RECEIVED CAB ALTITUDE HI MESSAGE, WHICH RESULTED IN 1 SET OF PAX MASKS DROPPING IN THE CA
- [SDR DXTA2023080892520](https://openairdocs.org/sdr/DXTA2023080892520), Aug 7, 2023: UNKNOWN. UNKNOWN. ON ROTATION CAPTAINS YOKE MADE A CLUNK AND IS LOOSE. FOUND PILOT'S YOKE SUPPORT LOOSE. REMOVED AND REPLACED PILOT'S VOICE SUPPORT NUT AND WASHERS. REF AMM 27-01
- [SDR DXTA2023052286860](https://openairdocs.org/sdr/DXTA2023052286860), May 21, 2023: CONTROL MODULE. DEFECTIVE. RIGHT MLG BRAKE: REPEAT WRITE-UP. ON LANDING AND TAXI IN, A NOTICEABLE BRAKE PULSE OR OSCILLATION. MOST NOTABLE FROM 80 KTS DOWN TO ABOUT 20 KTS. NOT SURE IF IT
- [SDR DXTA2022060963560](https://openairdocs.org/sdr/DXTA2022060963560), Jun 8, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: AFTER LANDING AND SHUT DOWN THE EMERGENCY LIGHTS STAYED ON. TRIED TURNING THE BATTERYS ON AND RECYLED THE THE SWITCH AND BEFORE WE TRYED THE 
- [SDR DXTA2021122754100](https://openairdocs.org/sdr/DXTA2021122754100), Dec 24, 2021: NONE. DEFECTIVE. EMERGENCY LIGHTING: ALL OF THE EMERGENCY LIGHTS ILLUMINATE IN BOTH THE ARM AND ON POSITION WITH AIRCRAFT POWER AVAILABLE. THE LIGHTS WILL SHUT OFF IF THE EMER L
- [SDR DXTA2021021204724](https://openairdocs.org/sdr/DXTA2021021204724), Feb 11, 2021: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTS BATTERY: EMERGENCY EXIT LIGHTS BEGAN FLASHING IN FLIGHT. FLASHED ON/OFF FOR THE LAST 10 MINUTES OF FLIGHT. LIGHT SWITCH WAS IN ARM POSITION.///
- [SDR DXTA202101054560](https://openairdocs.org/sdr/DXTA202101054560), Jan 5, 2021: LIGHT. INOPERATIVE. EMERGENCY EXIT LOWER SIGN DOES NOT ILLUMINATE. REMOVED COVERS AND LAMP ASSEMBLY. CHECKED WIRING AND SWAPPED POSITIONS WITH THE FWD LAMP ASSEMBLY. BOTH LAMPS ARE
- [SDR DXTA2019011501913](https://openairdocs.org/sdr/DXTA2019011501913), Jan 15, 2019: WARNING SYSTEM. FALSE ACTIVATION. SWPS FAULT YELLOW CAS ILLUMINATED - DURING INITIAL DESCENT FROM CRUISE FLIGHT, WE HAD MULTIPLE CAS FAIL AND FAULTS LIGHTS INCLUDING PTRIM BKP FAIL, SWPS FAULT, 

## Service difficulty reports on N393QS not matched to an aircraft (19)

They name N393QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200811253373](https://openairdocs.org/sdr/DXTA200811253373), Nov 25, 2008: THROTTLE. OUT OF RIG. DURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUT DOWN. RIGGED THROTTLE LINKAGE AND RAN ACFT STILL SHO
- [SDR DXTA2008112603373](https://openairdocs.org/sdr/DXTA2008112603373), Nov 25, 2008: ENGINE. SHUTDOWN. DURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROUGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUTDOWN.
- [SDR DXTA2008111003343](https://openairdocs.org/sdr/DXTA2008111003343), Nov 7, 2008: BRAKE SYS. MALFUNCTIONED. AT END OF LANDING ROLL OUT RIGHT SEAT PILOT LOST BRAKE PRESSURE WITH PEDALS PRESSED 3/4 THROW. RELEASED BRAKES AND REAPPLIED WITH SAME RESULT (NO BRAKING). WHIL
- [SDR DXTA200802815](https://openairdocs.org/sdr/DXTA200802815), Jan 31, 2008: CONNECTOR. LOOSE. DURING T/O POWER APPLICATION HYD PRESS LIGHT CAME ON AT APPX 80 PERCENT N1. ABORTED T/O. GAINED ACCESS TO SPEED BRAKE SWITCHES. FOUND CONNECTOR FOR SWITCH WIRIN
- [SDR DXTA200702657](https://openairdocs.org/sdr/DXTA200702657), Dec 7, 2007: UNKNOWN. UNKNOWN. AFTER TAKEOFF, RED LANDING GEAR NOT LOCKED AND AMBER HYD SYS PRESS LIGHTS REMAINED ILLUMINATED FOR APPROXIMATELY 2 MINUTES. AT THAT TIME A THUMP WAS HEARD AND F
- [SDR DXTA200702273](https://openairdocs.org/sdr/DXTA200702273), Jun 17, 2007: BRAKE. FAILED. POWER BRAKE SYSTEM FAILURE (POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHT ON) LIGHT STAYS ON. [07-10-07] FOUND THE BRAKE PRESSURE RELIEF VALVE STUCK IN THE OPE
- [SDR DXTA200702110](https://openairdocs.org/sdr/DXTA200702110), Apr 15, 2007: BRAKE. WEAK. FO BRAKES VERY SOFT AND SPONGY. F/O BRAKE PEDALS TRAVELS TO THE STOP. CAPTAINS SIDE SOFT AS WELL. BLEED BRAKE PER CITATION 560 M/M 32-42-00. OPS AND LEAK CHECK 
- [SDR DXTA200702096](https://openairdocs.org/sdr/DXTA200702096), Apr 10, 2007: BRAKE ASSY. WEAK. CO-PILOT'S BRAKES ARE SPONGY.BLED BRAKES AS REQUIRED. NO DEFECTS NOTED. ALL WORK DONE IAW CESSNA 560 MAINTENANCE MANUAL 32-42-00.
- [SDR DXTA200601745](https://openairdocs.org/sdr/DXTA200601745), Nov 20, 2006: ACCUMULATOR. LOW. POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP LIGHTS STAYED ON MUCH LONGER THAN USUAL UPON LANDING GEAR EXTENSION (APPROX 10 SECONDS). FOUND POWER BRAKE ACCUMULAT
- [SDR DXTA200601651](https://openairdocs.org/sdr/DXTA200601651), Oct 12, 2006: THROTTLE. MISRIGGED. WITH ENGINES RUNNING IF EITHER THROTTLE IS BROUGHT BACK TO IDLE FIRMLY, THAT ENGINE SHUTDOWN. DURING START OF LT ENGINE, AN UNSUAL (CLICK) NOISE WAS HEARD WHEN 
- [SDR DXTA200601548](https://openairdocs.org/sdr/DXTA200601548), Aug 9, 2006: BYPASS VALVE. MALFUNCTIONED. HYD PRESS ON LIGHT CAME ON INFLIGHT. COMPLIED WITH PILOTS ABBRVT CHECKLIST (J2). LIGHT REMAINED ON UNTIL ON FINAL AND GEAR WAS EXTENDED. TROUBLESHOT SYSTEM AND 
- [SDR DXTA200601539](https://openairdocs.org/sdr/DXTA200601539), Aug 6, 2006: FCU. OUT OF RIG. RIGHT ENGINE SHUTDOWN AGAIN WHILE BRINGING THROTTLE TO IDLE ON THE POST START SPEED-BRAKE CHECK. FOUND RIGGING OUT OF SPEC AT FUEL CONTROL. RERIGGED AT FUEL CON
- [SDR DXTA200601537](https://openairdocs.org/sdr/DXTA200601537), Aug 5, 2006: LIMIT SWITCH. OUT OF ADJUST. RT ENGINE SHUTDOWN WHILE BRINGING THROTTLE TO IDLE ON SPEED BRAKE CHECK. ADJUSTED RT ENGINE THROTTLE CUTOFF SWITCH IAW CE560 MM CH 73-30-03. OPS CHECKED GOOD.
- [SDR DXTA200601499](https://openairdocs.org/sdr/DXTA200601499), Jul 14, 2006: BRAKE ASSY. CONTAMINATED. CO-PILOTS RIGHT BRAKE PEDAL HAS NO PRESSURE. PEDAL GOES TO THE STOP. BLED BRAKES PER CE 560 MM 32-42-00. OPS CHECKED NORMAL.
- [SDR DXTA200601311](https://openairdocs.org/sdr/DXTA200601311), Mar 22, 2006: BULB. BURNED OUT. RT GREEN GEAR LIGHT DID NOT ILLUMINATE AFTER SELECTING GEAR DOWN (NO UNSAFE LIGHT OR OTHER WARNINGS WERE NOTICED), EMERGENCY GEAR BOTTLE WAS USED TO BLOW DOWN G
- [SDR DXTA200300088](https://openairdocs.org/sdr/DXTA200300088), Aug 17, 2003: COALESCER BAG. CONTAMINATED. DIVERTED BACK INTO CMH WHEN EMERGENCY PRESSURIZATION LIGHT CAME ON AFTER TAKEOFF, EMERGENCY PRESSURIZATION CHECK LIST FOLLOWED. - FOUND WATER SEPARATOR COALESCE
- [SDR DXTA200300045](https://openairdocs.org/sdr/DXTA200300045), Jun 9, 2003: SENSOR. FAULTY. SHORTLY AFTER T/O EMER PRESS LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION ACTIVATED W/SYSTEM IN NORMAL POSITION. AIRCRAFT RETURNED AFTER TAKEOFF AND LANDED OV
- [SDR 99ZZZX603](https://openairdocs.org/sdr/99ZZZX603), Jan 8, 1998: CHANNEL. MISMANUFACTURED. CESSNA SB 560-54-03 COMPLETED 12-14-98. SB INCORPORATES VAPOR BARRIER/VIBRATION DAMPENING CHANNEL AROUND ENGINE INLET DUCT. FOUND CHANNELS MELTED AFTER 77.1 HOU
- [SDR 97ZZZX2581](https://openairdocs.org/sdr/97ZZZX2581), May 15, 1997: SKIN. CRACKED. FOUND 3 INCH CRACK ON RIGHT SIDE OF RUDDER ALONG AFT RIB - WL 158.00. CRACK IS THROUGH 3 EACH RIVETS. SUBMITTER STATED THIS IS THE 8TH OCCURRENCE ON FLEET.

## 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.