# N302QS: 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: 50500123
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: April 26, 2013
- Certificate issued: April 8, 2026
- Expires: April 30, 2033
- Mode S code: A3282F
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=302QS
- Page: https://openairdocs.org/aircraft/N302QS

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 N302QS.

## FAA accident and incident reports

None matched to N302QS.

## Reports on N302QS not matched to an aircraft (1)

They name N302QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20050603019289I](https://openairdocs.org/incident/20050603019289I), Jun 3, 2005: Cessna 560CESSNA (N302QS), Buffalo, NY. (-23) On June 3, 2005, at 1040 EDT, a Cessna CE-560, N302QS, operated by dxta enroute from mdw to lwm with two passengers at FL410 declared an emergency…

## Service difficulty reports (14)

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 DXTA2026030307060](https://openairdocs.org/sdr/DXTA2026030307060), Feb 28, 2026: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTS ILLUMINATED WHILE IN ARM POSITION. REMOVED PILOT AND COPILOT SEATS. PULLED UP COCKPIT CENTER FLOOR MATTING. REMOVED CENTER COCKPIT FLOOR PANEL.
- [SDR DXTA2026020606783](https://openairdocs.org/sdr/DXTA2026020606783), Feb 4, 2026: BATTERY PACK. DEFECTIVE. UPON STARTUP INTERIOR EMER LIGHTS CONTINUOUSLY FLASHING. REMOVED EMERGENCY BATTERY NO.1 AND REPLACED IT WITH A REPAIRED UNIT. REMOVED EMERGENCY BATTERY NO.2 AND
- [SDR JGVR20251209003](https://openairdocs.org/sdr/JGVR20251209003), Dec 9, 2025: SKIN. SCRATCHED. BLENDED SCRATCHES ON THE LT & RT LEADING EDGES, PERFORMED NDT AND PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. VERIFIED NO BLENDS EXCEEDED THICKNESS MATER
- [SDR DXTA2025091604975](https://openairdocs.org/sdr/DXTA2025091604975), Sep 14, 2025: BATTERY PACK. FAULTED. FORWARD CABIN EMERGENCY LIGHTS COME ON FOR A FEW MINUTES THEN GO OUT FOR AWHILE AND THEN COME BACK ON FOR A FEW MINUTES, REPEATEDLY. REMOVED BOTH EMERGENCY BATT
- [SDR DXTA2024032611310](https://openairdocs.org/sdr/DXTA2024032611310), Mar 25, 2024: SWITCH. FAULTED. EMERGENCY SWITCH WAS IN THE ARMED POSITION. EMERGENCY FLOOR LIGHTS ELUMINATED WITH NO CAUSE. WE LEFT THEM ON AND THEY BEGAN BLINKING. WE SWITCHED THEM TO OFF AN
- [SDR DXTA2023120800217](https://openairdocs.org/sdr/DXTA2023120800217), Dec 7, 2023: GDS. FAULTY. REMOVED FAILED GDS 1 AND INSTALLED A REPAIRED GSD 41, WORK DONE IAW AMM 31-41-01. PERFORMED GSD 1 SOFTWARE/CONFIGURATION UPLOADING IAW AMM 31-41-01. PERFORMED O
- [SDR DXTA2023112110114](https://openairdocs.org/sdr/DXTA2023112110114), Nov 21, 2023: BATTERY. DEFECTIVE. IN FLIGHT, THE CABIN EMERGENCY LIGHTS WERE CONTINUING TO PULSE. REMOVED AND REPLACED EMERGENCY BATTERY. IAW TASK 33-52-01-400-801-A
- [SDR DXTA2023053087370](https://openairdocs.org/sdr/DXTA2023053087370), May 30, 2023: LIGHT. DEFECTIVE. CABIN EMERG LIGHT: FORWARD CEILING EMERGENCY LIGHT BY MAIN CABIN DOOR DOES NOT ILLUMINATE WHEN EMER LT SWITCH SELECTED TO ON. BOTH THE MIDDLE AND AFT ILLUMINATE
- [SDR DXTA2021101550300](https://openairdocs.org/sdr/DXTA2021101550300), Oct 14, 2021: NONE. NONE. CABIN EMERG LIGHT: IN FLIGHT WITH EMER LIGHT ARMED, EMERGENCY LIGHTS IN CABIN WERE FLASHING.///SIGN-OFF///PREFORMED TROUBLESHOOTING IAW EMBRAER SERVICE LETTER N
- [SDR 2020FA0000512](https://openairdocs.org/sdr/2020FA0000512), Nov 21, 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 2020FA0000371](https://openairdocs.org/sdr/2020FA0000371), Aug 11, 2020: BATTERY PACK. FAILED. DISCREPANCY: AIRCRAFT CREW REPORTED "ON GROUND JUST BEFORE ENGINE START, GROUND POWER UNIT CONNECTED AND ON WITH EMERGENCY LIGHT SWITCH IN "ARM" POSITION", THE 
- [SDR DXTA2019112103103](https://openairdocs.org/sdr/DXTA2019112103103), Nov 20, 2019: SENSOR. FAILED. DURING CLIMBOUT CRUISE AND DESCENT EXPERIENCED WHITE SHED BUS 1&2 OFF INTERMITTENTLY AND AN BLEED 1 FX THAT WENT AWAY VIA THE CHECKLIST. BELOW 10,000 FT. AMBER 
- [SDR DXTA2014032805701](https://openairdocs.org/sdr/DXTA2014032805701), Mar 27, 2014: CONTROL UNIT. FAILED. SHORTLY AFTER LEVELING AT FL430, SWPS FAULT AMBER CAS CAME ON ALONG WITH THE WHITE, SPOILER FAULT MESSAGE. THERE WERE YELLOW X'S IN THE FLAP INDICATOR, PITCH TR
- [SDR DXTA2013060505412](https://openairdocs.org/sdr/DXTA2013060505412), Jun 5, 2013: DISPLAY. FAILED. AFTER DEPARTURE, PFD 1 FAILED AND REVERTED. MFD FAILED AND REVERTED. COMM 1 FAILED. TXPDR 1 FAILED. SPLIT SCREEN JEPP CHARTS ON PFD FAILED. APPROX A DOZEN CAS M

## Service difficulty reports on N302QS not matched to an aircraft (20)

They name N302QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010061704124](https://openairdocs.org/sdr/DXTA2010061704124), Jun 15, 2010: SEAL. FAILED. AT FLT LEVEL 390, A SUDDEN, EXTREMELY LOUD SQUEALING NOISE FILLED CABIN, NO SECONDARY INDICATIONS OF A PRESSURE ISSUE AT THE TIME. STARTED A RAPID DESCENT AS A 
- [SDR DXTA2010022504003](https://openairdocs.org/sdr/DXTA2010022504003), Feb 24, 2010: UNKNOWN. ODOR. NOTED FAINT ELECT/ BURNED INSULATION TYPE ODOR IN FLIGHT. NO SMOKE. COULD NOT IDENTIFY THE SOURCE. PRECAUTIONARY LANDING MADE. INSPECTED ACFT AND PERFORMED NUME
- [SDR DXTA200811123352](https://openairdocs.org/sdr/DXTA200811123352), Nov 12, 2008: FLOW DIVIDER. MISRIGGED. RT ENGINE QUIT ON LANDING ROLL OUT. ENGINE QUIT WHEN RT THROTTLE WAS BROUGHT TO IDLE. RT THROTTLE SEEMS TO HAVE AN EXCESSIVE AMOUNT OF SLOP WHEN BROUGHT BACK TO
- [SDR DXTA2008111303352](https://openairdocs.org/sdr/DXTA2008111303352), Nov 12, 2008: ENGINE. MALFUNCTIONED. RIGHT ENGINE QUIT ON LANDING ROLL OUT.
- [SDR DXTA200811113349](https://openairdocs.org/sdr/DXTA200811113349), Nov 11, 2008: ENGINE. UNKNOWN. RT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES IDLE. REMOVED LT/RT ENG LWR COWLS FOR ACCESS. RE-RIGGED RT FDV TO FUEL CONTROL RD. ADJUSTED RT THROTT
- [SDR DXTA2008111203349](https://openairdocs.org/sdr/DXTA2008111203349), Nov 11, 2008: ENGINE. SHUTDOWN. RIGHT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES AT IDLE.
- [SDR DXTA200809283290](https://openairdocs.org/sdr/DXTA200809283290), Sep 28, 2008: RETAINER. MISSING. RT SEAT BRAKES NOT OPERATING PROPERLY. DURING TAXI, YOU MUST GO VERY FAR ON THE BRAKES TO GET ANY RESISTANCE. NORMAL BRAKING ON LT SEAT SIDE. NO FLUID NOTED UND
- [SDR DXTA200803257](https://openairdocs.org/sdr/DXTA200803257), Aug 31, 2008: BRAKE SYS. CONTAMINATED. COPILOT RT BRAKE PEDAL IS LESS EFFECTIVE THEN THE LT PEDAL. MORE TRAVEL IS NEEDED TO PRODUCE BRAKE PRESSURE. PERFORMED VISUAL INSP, CHECKING BRAKE LINES IN COCK
- [SDR DXTA200803202](https://openairdocs.org/sdr/DXTA200803202), Jul 28, 2008: STARTER GEN. MALFUNCTIONED. STARTER DISENGAGE PROBLEM - ABORTED LT ENG START WHEN N2 AT 25% AND NO N1. ENG APPEARED TO SHUTDOWN NORMALLY. F/O CHECKED, ENG WAS STILL RUNNING AND SMOKE WAS C
- [SDR DXTA200803103](https://openairdocs.org/sdr/DXTA200803103), Jun 7, 2008: BRAKE SYS. WEAK. CAPTAIN AND COPILOT RIGHT BRAKE PEDALS ARE LESS EFFECTIVE THEN THE LEFT PEDAL, MORE TRAVEL IS NEEDED TO PRODUCE BRAKE PRESSURE. ACCOMPLISHED TASK CARD TC-560-32
- [SDR DXTA200803064](https://openairdocs.org/sdr/DXTA200803064), May 17, 2008: BRAKE SYS. MALFUNCTIONED. ON TAXI OUT BOTH PILOT AND CO-PILOT BRAKES WERE VERY HARD DURING APPLICATION, WHEN BRAKES WERE APPLIED (CO-PILOT OR PILOT), AIRCRAFT WOULD NOT SLOW UNTIL A GREA
- [SDR DXTA200803003](https://openairdocs.org/sdr/DXTA200803003), Apr 18, 2008: FLOW DIVIDER. OUT OF ADJUST. DURING SPEED BRAKE TEST, LT ENGINE SHUTDOWN AND RT ENGINE SHUTDOWN. ADJUSTED TENSION ON BALL PLUNGER ON THE FUEL FLOW DIVIDER, PERFORMED OPS CHECK WITH NO DEFEC
- [SDR DXTA200702581](https://openairdocs.org/sdr/DXTA200702581), Oct 29, 2007: SQUAT SWITCH. READS HIGH. LOST CABIN PRESSURIZATION AT FL290. CABIN PRESSURE ROSE TO 13500 PA AND STABILIZED. ON DESCENT, CABIIN PRESSURE DESCENDED WITH THE AIRCRAFT ALTITUDE. FOUND LT S
- [SDR DXTA200500944](https://openairdocs.org/sdr/DXTA200500944), Aug 31, 2005: BRAKE. FAILED. ON TAXI OUT DURING BRAKE CHECK CAPTAINS LEFT BRAKE WENT ALL THE WAY TO THE FLOOR. UPON ACTIVATION OF THE CO-PILOTS LEFT BRAKE, BOTH BECAME SPONGY. RESET BRAKE S
- [SDR DXTA200500774](https://openairdocs.org/sdr/DXTA200500774), Jun 14, 2005: ENGINE. MALFUNCTIONED. ABORTED TAKEOFF, RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER (97.2) ONLY ACHIEVED 95.3 PERCENT. RAN RIGHT ENGINE TO TAKEOFF POWER [97.2], ALL PARAMETERS WERE WITH
- [SDR DXTA200400275](https://openairdocs.org/sdr/DXTA200400275), Mar 25, 2004: RELAY. FAILED. 400 FT ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED, AND BRAKES BECME 
- [SDR DXTA200400273](https://openairdocs.org/sdr/DXTA200400273), Mar 22, 2004: CONNECTOR. CONTAMINATED. 400 FEET ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED. - BLED AIRCRAFT
- [SDR DXTA200400268](https://openairdocs.org/sdr/DXTA200400268), Mar 18, 2004: CIRCUIT BREAKER. TRIPPED. APPROX 100 FT ABOVE TOUCHDOWN THE "POWER BRAKE LOW PRESS." AND "ANTISKID INOP." ANNUNCIATOR LIGHTS ILLUMINATED AND THE ANTI SKID CIRCUIT BREAKER POPPED. LANDING
- [SDR DXTA200400261](https://openairdocs.org/sdr/DXTA200400261), Mar 12, 2004: WARNING LIGHT. ILLUMINATED. ON APPROACH POWER BRAKE LOW PRESS AND ANTI-SKID INOP, ANNUNCIATORS ILLUMINATED. EMERGENCY CHECKLIST PROCEDURE WAS COMPLIED WITH AND ANNUNCIATOR REMAINED ILLUMIN
- [SDR DXTA200300062](https://openairdocs.org/sdr/DXTA200300062), Jul 5, 2003: WIRE. BROKEN. LEFT THRUST REVERSER UNLOCK LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. BLED BRAKE SYSTEM, TROUBLESHOT TO BROKEN WIRES ON THE ANTI-SKID TRANSDUCER. REPA

## 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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