# N316QS: 2013 Embraer S A EMB-505

- Status: Valid registration
- Airframe: [Embraer S A EMB-505](https://openairdocs.org/model/embraer-s-a-emb-505) (registry code 326040C, 9 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: 50500161
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: September 16, 2013
- Certificate issued: May 18, 2022
- Expires: May 31, 2029
- Mode S code: A35E8A
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=316QS
- Page: https://openairdocs.org/aircraft/N316QS

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 S A 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 N316QS.

## 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 20240722008749I](https://openairdocs.org/incident/20240722008749I), Jul 22, 2024: Embraer EMB-505 (N316QS), Charlestown, SC, Minor damage. During landing rollout, the aircraft struck a deer at approximately 70 - 80 KIAS. The aircraft sustained damage to the underside of the fuselage aft of the…

## 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 DXTA2025110305492](https://openairdocs.org/sdr/DXTA2025110305492), Oct 29, 2025: BATTERY PACK. MALFUNCTIONED. TAXIING FOR TAKEOFF, ALL EMERGENCY LIGHTS STARTED FLICKERING. WHEN EMERGENCY SWITCH IN THE OFF POSITION, EMERGENCY LIGHTS SOMETIMES ON & SOMETIMES OFF. REMOVED 
- [SDR DXTA2025051103452](https://openairdocs.org/sdr/DXTA2025051103452), May 11, 2025: ELEC CONNECTOR. LOOSE. CABIN EMERG LIGHT: DURING POST-FLIGHT, THE OVERHEAD EMERGENCY LIGHT LOCATED BETWEEN SEAT 3 AND SEAT 4 IS INOPERATIVE. CORRECTIVE ACTION: FOUND THE CONNECTOR TO 
- [SDR DXTA2025022502456](https://openairdocs.org/sdr/DXTA2025022502456), Feb 21, 2025: DOOR. FAULTED. MAIN ENTRY DOOR NEEDS TO BE EVALUATED; DOOR TENDS TO DROP/SLAM WITHOUT GUIDANCE. REMOVED FOD. OPS CHECK GOOD. IAW EMB-505 AMM CH 52-14-00.
- [SDR DXTA2025012102010](https://openairdocs.org/sdr/DXTA2025012102010), Jan 17, 2025: STRUT. DEFECTIVE. LG LEVER DISAG RED CAS: REPEAT WRITE UP. ON TAKEOFF, RECIEVED RED "LG LEVER DISAG" CAS WHEN LG LEVER SELECTED UP. CYCLED LG PER QRH AND CONDITION RETURNED. RECI
- [SDR DXTA2024022010940](https://openairdocs.org/sdr/DXTA2024022010940), Feb 17, 2024: BATTERY. UNKNOWN. AC GENERATION AND CONTROL: AFTER TAKEOFF, WE GOT CAS EMER LIGHT NOT ARMED AND THE EMER LIGHTS WERE PHYSICALLY ON (THIS SEEMED TO SUPPORT WHAT WE LATER DISCOVERE
- [SDR DXTA2024010510519](https://openairdocs.org/sdr/DXTA2024010510519), Jan 4, 2024: SHUTOFF VALVE. DEFECTIVE. CABIN PRESSURIZATION CONTROL: DURING CLIMB OUT ~12000-14000' WE HAD AN ECS VALVE 2 FAILURE - PULLED UP THE ECS PAGE AND CONFIRMED IT. APPROXIMATELY 17000' IT CL
- [SDR DXTA2023101097610](https://openairdocs.org/sdr/DXTA2023101097610), Oct 10, 2023: UNKNOWN. UNKNOWN. WITH THE CABIN DOOR, OPEN, TOP RIGHT BOLT CAME OUT. WASHER FELL INTO THE DOOR COWLING. THIS HAPPENED DURING PASSENGER BOARDING. GAINED ACCESS TO MED INTERIOR AN
- [SDR DXTA2023060187500](https://openairdocs.org/sdr/DXTA2023060187500), Jun 1, 2023: UNKNOWN. UNKNOWN. MAIN ENTRANCE DOOR HANDLE BROKE OFF AT THE BASE WHILE A HUB SERVICE TECH WAS CLOSING THE DOOR. PERFORMED AN OPS CHECK AND TROUBLESHOOTING PLUS VISUAL INSPECTION
- [SDR DXTA2022080867530](https://openairdocs.org/sdr/DXTA2022080867530), Aug 7, 2022: NONE. NONE. CABIN EMERG LIGHT: EMERGENCY LIGHTS FLICKERING ON/OFF IN FLIGHT.
- [SDR DXTA2022072566700](https://openairdocs.org/sdr/DXTA2022072566700), Jul 24, 2022: BATTERY. DEFECTIVE. CABIN EMERGENCY LIGHTS FLASHING IN ARM POSITION. // SIGNOFF// GAINED ACCESS TO FWD EMERGENCY BATTERY BY REMOVING FLOOR PANEL 223CLF. REMOVED INOP EMERGENCY BATT
- [SDR 2020FA0000535](https://openairdocs.org/sdr/2020FA0000535), Dec 13, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEV
- [SDR DXTA2014091505881](https://openairdocs.org/sdr/DXTA2014091505881), Sep 11, 2014: TRANSDUCER. INOPERATIVE. WHEEL BRAKES PULSE & GRAB UNEVENLY DURING LANDING ROLLOUT, CAUSING SIGNIFICANT DIRECTIONAL CONTROL DIFFICULTY DURING BRAKING. THEREAFTER THE BRAKES PULSE DURING
- [SDR DXTA2013121205595](https://openairdocs.org/sdr/DXTA2013121205595), Dec 11, 2013: ACTUATOR. FAULTY. WHEN THE GEAR IS SELECTED TO THE DOWN POSITION THE NOSE GEAR REMAINS IN THE UP & LOCKED POSITION UNTIL THE MAIN GEAR IS DOWN & LOCKED THEN THE NOSE GEAR EXTENDS

## Service difficulty reports on N316QS not matched to an aircraft (15)

They name N316QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2011032104516](https://openairdocs.org/sdr/DXTA2011032104516), Mar 20, 2011: PRESSURE SWITCH. FAILED. NORMAL BRAKE FAILED ON LANDING ROLL. ON SHORT FINAL (100 FT AGL) "POWER BRAKE LOW PRESS" AND "ANTI SKID INOP" ANNUNCIATORS ILLUMINATED, ON LANDING NORMAL BRAKES
- [SDR DXTA2011010304385](https://openairdocs.org/sdr/DXTA2011010304385), Jan 2, 2011: LINE. LEAKING. OUT OF 4000 FT THE LT ENG FIRE LIGHT CAME ON, PULLED POWER TO IDLE AND LIGHT WENT OUT. LANDED WITH NO OTHER LIGHTS. REMOVED COWLING AND INSPECTED ENGINE FOR HOT
- [SDR DXTA2010081604191](https://openairdocs.org/sdr/DXTA2010081604191), Aug 13, 2010: MOTOR. SMOKE. SMOKE SEEN COMING FROM HELLHOLE, AC NOW INOP, NO SIGN OF CHARRING OR ANY OTHER SIGN OF DAMAGE. ODOR COMING FROM INSIDE MOTOR. REMOVED FREON FROM SYS. REMOVED AC
- [SDR DXTA2010043004081](https://openairdocs.org/sdr/DXTA2010043004081), Apr 29, 2010: BRAKE ASSY. WEAK. CO-PILOT'S BRAKE PEDALS SEEM TO BE SOFTER THAN NORMAL, ADDITIONALLY THE RT BRAKE PEDAL GOES FARTHER DOWN THAN THE LT WHEN PRESSURE IS APPLIED. COMPLIED WITH BLE
- [SDR DXTA2009072303738](https://openairdocs.org/sdr/DXTA2009072303738), Jul 22, 2009: TRIM SYSTEM. MALFUNCTIONED. WITH PITCH TRIM INDICATOR IN T/O POSITION, UPON ROTATION, ACFT OVER ROTATED AND IT TOOK BOTH HANDS TO CONTROL. NORMAL FLIGHT CONTROL FORCES WITH TRIM INDICATOR 
- [SDR DXTA200702585](https://openairdocs.org/sdr/DXTA200702585), Oct 30, 2007: MASTER CYLINDER. BYPASSING. PILOTS RT BRAKE PEDAL GOES SOFT AFTER 15-20 SEC OF INITIAL BRAKE APPLICATION. (LOSSED APPX 2-3 INCHES OF PEDAL TRAVEL). INSTALLED 1EA NEW PILOTS RH BRAKE MASTER
- [SDR DXTA200702573](https://openairdocs.org/sdr/DXTA200702573), Oct 25, 2007: BRAKE ASSY. WEAK. PILOTS RT BRAKE PEDAL GOES SOFT AFTER INITIAL APPLICATION. THE RT PEDAL TRAVELS SIGNIFICANTLY FURTHER THAN THE LT BRAKE PEDAL. BLED LT AND RT BRAKES IAW MM 32-4
- [SDR DXTA200702565](https://openairdocs.org/sdr/DXTA200702565), Oct 23, 2007: BRAKE. WEAK. RT BRAKE ON CAPTAIN'S SIDE DEPRESSES FURTHER THAN LT SIDE AND IS SOFT. CO-PILOTS SIDE HAS SIMILAR PROBLEM. REMOVED AND REPLACED RT MAIN BRAKE IAW CE-560 MAINTEN
- [SDR DXTA200702544](https://openairdocs.org/sdr/DXTA200702544), Oct 15, 2007: BRAKE. MALFUNCTIONED. WHEN TAXIING AND MAINTAINING LIGHT BRAKE PRESSURE ON BOTH BRAKE PEDALS, RT PEDAL PRESSURE DROPS AND PEDAL DEPRESSES ALL THE WAY TO STOP. BLED BOTH LT AND RT BRA
- [SDR DXTA200702422](https://openairdocs.org/sdr/DXTA200702422), Jul 27, 2007: BRAKE. MALFUNCTIONED. LT BRAKE PEDAL PRESSURE ON F/O SIDE IS LOW. NEEDS TO BE PUMPED UP MANUALLY. PREFORMED BRAKE BLEEDING PROCEDURE IAW CESSNA 560 MM 32-42-00. OPS AND LEAK CHECK GO
- [SDR DXTA200601307](https://openairdocs.org/sdr/DXTA200601307), Mar 18, 2006: HYDRAULIC LINE. LEAKING. POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHTS FAILED TO EXTINGUISH WHEN GEAR WERE EXTENDED. POST FLIGHT REVEALS NO FLUID SEEN THROUGH SITE GAUGES. FOUND LT BR
- [SDR DXTA200500943](https://openairdocs.org/sdr/DXTA200500943), Aug 30, 2005: MASTER CYLINDER. LEAKING. RIGHT PILOT'S BRAKE PEDAL SOFT. REMOVED AND REPLACED CO-PILOT'S LT & RT BRAKE MASTER CYLINDERS AND BLED BRAKE SYSTEM IAW 560 ULTRA MM 32-42, OPS CHECK GOOD.
- [SDR DXTA200400402](https://openairdocs.org/sdr/DXTA200400402), Sep 20, 2004: ODOR. DETECTED. DURING CLIMB BETWEEN FL180-FL190, NOTICED A STRONG FUEL SMELL IN THE COCKPIT AND AT THE REFRESHMENT CENTER, DURING DECENT AND LANDING THE SMELL FADED AWAY. ITEM
- [SDR DXTA200400395](https://openairdocs.org/sdr/DXTA200400395), Sep 16, 2004: CHECK VALVE. LEAKING. A STRONG FUEL SMELL WAS NOTED IN THE CABIN WHILE AT CRUISE. FOUND PRE-CHECK VALVE LEAKING, INSTALLED NEW VALVE WITH NEW PACKINGS IAW MM CHAPTER 28-22-00. OPS CH
- [SDR CWQ2003F00006](https://openairdocs.org/sdr/CWQ2003F00006), Mar 3, 2003: DUCT. CRACKED. DURING ROUTINE INSP LOCKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE PN 6512072-12 CRACKED 1.50 INCH IN A CIRCLE PATTERN AND READY TO BREAK OFF. FOUND

## 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 S A 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 S A EMB-505 aircraft: https://openairdocs.org/model/embraer-s-a-emb-505/aircraft.md
- The Pratt & Whitney Canada PW535E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535e.md

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