# N343QS: 2014 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: 50500194
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: May 14, 2014
- Certificate issued: May 16, 2022
- Expires: May 31, 2029
- Mode S code: A3C9E2
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=343QS
- Page: https://openairdocs.org/aircraft/N343QS

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 N343QS.

## 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 20260129000379I](https://openairdocs.org/incident/20260129000379I), Jan 29, 2026: Embraer Executive Aircraft Inc EMB-505 (N343QS), Cincinnati, OH, Minor damage. Bird strike at 400 feet on landing, flock of geese. One hit the windshield; no damage to windscreen noted. Another dented the left starter/generator inlet duct…

## Service difficulty reports (22)

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 DXTA2026062208522](https://openairdocs.org/sdr/DXTA2026062208522), Jun 20, 2026: WARNING MESSAGE. ILLUMINATED. DURING THE APPROACH WHILE SELECTING FLAPS FROM 2 TO FULL WE RECEIVED A YELLOW FLAP FAIL CAS MESSAGE. WE ACCOMPLISHED THE RESPECTIVE QRC AND TRIED CYCLING THE FL
- [SDR DXTA2026061508426](https://openairdocs.org/sdr/DXTA2026061508426), Jun 13, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI OUT WE RECEIVED A VENTRAL RUDDER FAIL CAS FOLLOWED BY AP FAIL AND YD FAIL. WHEN WE STOPPED TAXIING, ALL MESSAGES DISAPPEARED. WHEN WE STARTED TO TAX
- [SDR DXTA2026042707778](https://openairdocs.org/sdr/DXTA2026042707778), Apr 24, 2026: LATCH. INOPERATIVE. MAIN PAX DOOR DOWN LOCK LATCH MECHANISM IS IN-OP. INSPECTED MAIN PAX DOOR AND CHECKED LENGTH OF HOIST ROD. ADJUSTED THE MAIN DOOR HOISTING ROD TO 8.5 INCHES PER
- [SDR DXTA2026022306958](https://openairdocs.org/sdr/DXTA2026022306958), Feb 19, 2026: PRESSURE SWITCH. FAULTED. DURING CRUISE WE HAD A FUEL 1 FEED FAULT CAS MESSAGE. FUEL SYNOPTIC SHOWS YELLOW X OVER PUMP. QRH PROCEDURE SHOWS CREW AWARENESS. CORRECTIVE ACTION: REMOVED THE
- [SDR DXTA2025111105645](https://openairdocs.org/sdr/DXTA2025111105645), Nov 10, 2025: CONTACTOR. FAULTED. REPEAT WRITE UP ON APPROACH TO LANDING IN KYIP WE RECEIVED GEN 1 OFF BUS YELLOW CAS ACCOMPANIED BY SHED BUS OFF. PLACED GEN 1 SWITCH IN OFF POSITION PER QRH DUE
- [SDR DXTA2025011601957](https://openairdocs.org/sdr/DXTA2025011601957), Jan 13, 2025: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: EMERGENCY LIGHTS FLASH CONTINUOUSLY UPON LANDING AND TAXI. CORRECTIVE ACTION: REPLACED FWD & AFT EMERGENCY BATTERIES. OPS CHECK GOOD. ORIGIN
- [SDR DXTA2024070312242](https://openairdocs.org/sdr/DXTA2024070312242), Jul 2, 2024: PIN. FAILED. AT FL400 PAX DOOR OPEN LIGHT CAME ON. REMAINED ON UNTIL DECENDING THROUGH FL370. REMOVED PIN, P/N: 43031-0009 NSN AND INSTALLED CUSTOMER SUPPLIED NEW PIN, P/N: 
- [SDR DXTA2024062612179](https://openairdocs.org/sdr/DXTA2024062612179), Jun 26, 2024: WIRE HARNESS. MISLOCATED. WHEN EMER LIGHTS ARE ON, THE MIDDLE, CEILING FLOOD LIGHT DOES NOT ILLUMINATE; WHEN TURNING ON THE SEAT BELT SIGN, MIDDLE CEILING FLOOD LIGHT DOES ILLUMINATE. FO
- [SDR DXTA2023121810364](https://openairdocs.org/sdr/DXTA2023121810364), Dec 17, 2023: ENGINE. FAULTED. RIGHT ENGINE ENGINE OIL PRESSURE INDICATION: WITHIN A MINUTE OF EXPERIENCING SEVERVE TURBULENCE A SMELL WAS NOTICED AND THEN SMOKE IN THE CABIN WAS OBSERVED. OI
- [SDR DXTA2023103199410](https://openairdocs.org/sdr/DXTA2023103199410), Oct 30, 2023: UNKNOWN. UNKNOWN. DURING LEVEL FLIGHT AT 32000 WE HAD THE FOLLOWING AMBER CAS MSGS SWPS FAULT,FLAP FAIL,PTRIM BKP FAIL ALSO AMBER X ON FLAP SYNOPTIC FLAP POSITION ,FLAP INDICATIO
- [SDR DXTA2023102398420](https://openairdocs.org/sdr/DXTA2023102398420), Oct 20, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: EBATT CABIN LIGHTS FLICKERING WHEN ON. //SIGNOFF// FOUND CABIN OVERHEAD LIGHTING PULSING WITH GPU ON. STARTED ENGINE IAW PHENOM 300 AMM 71-00
- [SDR DXTA2023060587870](https://openairdocs.org/sdr/DXTA2023060587870), Jun 5, 2023: UNKNOWN. UNKNOWN. DOOR PAX OPEN CAS ILLUMINATED IN FLIGHT. FIRST INTERMITTENT, THEN CONTINUOUS AT 37000FT. DIVERTED. BELOW 10000FT, THE MESSAGE WENT OUT.//CORRECTIVE ACTION//PRIN
- [SDR DXTA2023053087240](https://openairdocs.org/sdr/DXTA2023053087240), May 30, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: OF THE THREE CENTER EMERGENCY CEILING LIGHTS THE MIDDLE LIGHT DOES NOT ILLUMINATE WHEN THE EMER LT SWITCH IS PLACED TO ON//CORRECTIVEACTION//
- [SDR DXTA2023050185080](https://openairdocs.org/sdr/DXTA2023050185080), May 1, 2023: UNKNOWN. UNKNOWN. MLG BRAKE PRESSURE: ON TAXI OUT BOTH BRAKES WERE SHUDDERING WHEN APPLIED. AND WOULD RATTLE THE WHOLE AIRCRAFT. THIS HAPPENED WHEN APPLYING BOTH BRAKES OR EACH B
- [SDR DXTA2023042184630](https://openairdocs.org/sdr/DXTA2023042184630), Apr 20, 2023: UNKNOWN. UNKNOWN. DURING CLIMB OUT, PASSING 13,000', FELT & HEARD A VIBRATION IN AIRFRAME. LEVELED OFF AT 16,000' & RAN ENG ABNORMAL VIBRATION CHKLST NAP1-15. AFTER REDUCING POWE
- [SDR DXTA2023030280760](https://openairdocs.org/sdr/DXTA2023030280760), Feb 19, 2023: STOWAGE BOX. LEAKING. BOTH OXYGEN MASKS WERE STOWED AND STARTED FLOWING OXYGEN. YOU COULD HEAR THE SOUND. WHEN DONNED, WE RECEIVED CONTINUOUS FLOW AND WAS UNABLE TO SHUT OFF. LANDED 
- [SDR DXTA2023011978850](https://openairdocs.org/sdr/DXTA2023011978850), Jan 19, 2023: BATTERY PACK. FAULTED. EMERGENCY LIGHTS NOT ARM YELLOW CAS: ON START UP LIGHTS WOULD FLICKER THEN THE YELLOW CASS MSG. LIGHTS WOULD GO OUT AFTER ENGINE START THEN COME BACK ON IN THE 
- [SDR DXTA2022090970040](https://openairdocs.org/sdr/DXTA2022090970040), Sep 8, 2022: NONE. NONE. NONE OF THE 3 EMER LIGHTS HOUSED IN EACH OF THE 3 MAIN ENTRY DOOR STEPS OPERATE WHEN THE EMER LIGHT SWITCH IS TURNED ON. IF PRESSURE IS APPLIED BY WALKING DOWN 
- [SDR DXTA2022070565140](https://openairdocs.org/sdr/DXTA2022070565140), Jul 1, 2022: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTING FLICKERING ON/OFF WITH SWITCH IN ARM. "CORRECTIVE ACTION" REMOVED AND REPLACED AFT EMERGENCY LIGHTS BATTERY, OPERATI
- [SDR DXTA2022040159460](https://openairdocs.org/sdr/DXTA2022040159460), Apr 1, 2022: NONE. NONE. EMERGENCY LIGHTS BATTERY: IMMEDIATELY AFTER ENGINE START THE EMERGENCY LIGHTS STARTED CYCLING ON/OFF. WE TURNED THE EMER LT SWITCH TO ATM THEN OFF, BUT THE EMER
- [SDR DXTA2018020500549](https://openairdocs.org/sdr/DXTA2018020500549), Feb 4, 2018: CONTROL HANDLE. FAILED. ON GEAR RETRACTION THE MLG LEVER WAS PLACED IN THE UP POSITION. RECEIVED A RED CAS MESSAGE FOR LG LEVER DISAGREE. HAD THREE RED DOWN INDICATORS. RAN THE MLG LEV
- [SDR DXTA2015062206033](https://openairdocs.org/sdr/DXTA2015062206033), Jun 18, 2015: CONTROL UNIT. FAILED. FLYING AT 40,000 FT, NOTICED YELLOW X THROUGH BOTH PITCH & SPOILER INDICATORS. NO OTHER INDICATIONS OR CAS MSGS DISPLAYED. ACFT SEEMED FINE BUT SHORTLY THEREAFT

## Service difficulty reports on N343QS not matched to an aircraft (12)

They name N343QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2009122103905](https://openairdocs.org/sdr/DXTA2009122103905), Dec 19, 2009: ROD END. WORN. AFTER NORMAL GEAR RETRACTION UNUSUAL NOISE AND VIBRATIONS NOTED FROM NOSE AREA. AFTER RETURN TO AIRPORT, NOSE GEAR DOORS STILL OPEN. INSPECTED NLG FOUND NOSE GE
- [SDR DXTA2009011703468](https://openairdocs.org/sdr/DXTA2009011703468), Jan 17, 2009: MOTOR. INOPERATIVE. BRAKE LOW PRESSURE CAUTION ADVISORY LIGHT ILLUMINATED ON TAXI; PEDALS WENT TO FLOOR. LIGHT WENT OFF AND PRESSURE RETURNED AFTER 10 MINUTES. REMOVED AND REPLACED
- [SDR DXTA2009011903468](https://openairdocs.org/sdr/DXTA2009011903468), Jan 17, 2009: WARNING LIGHT. ILLUMINATED. BRAKE LOW PRESSURE CAUTION ADVISORY LIGHT ILLUMINATED ON TAXI; PEDALS WENT TO FLOOR.
- [SDR DXTA2008121903410](https://openairdocs.org/sdr/DXTA2008121903410), Dec 19, 2008: MASTER CYLINDER. LEAKING. LT BRAKE PEDAL ON PILOT'S SIDE WILL NOT HOLD PRESSURE WITH STEADY SLOW PRESSURE APPLIED, THE PEDAL GOES TO THE FLOOR. TS SYS REMOVED PILOTS LT WHEEL BRAKE MASTE
- [SDR DXTA2008122203410](https://openairdocs.org/sdr/DXTA2008122203410), Dec 19, 2008: BRAKE. WEAK. LEFT BRAKE PEDAL ON PILOT'S SIDE WILL NOT HOLD PRESSURE. WITH STEADY SLOW PRESSURE APPLIED, THE PEDAL GOES TO THE FLOOR.
- [SDR DXTA200802982](https://openairdocs.org/sdr/DXTA200802982), Apr 6, 2008: ENGINE. BIRD INGESTION. DURING CLIMB OUT AT APPROX 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABI
- [SDR DXTA20082982](https://openairdocs.org/sdr/DXTA20082982), Apr 6, 2008: ENGINE. BIRD INGESTION. DURING CLIMB OUT AT 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABIN.
- [SDR DXTA200702215](https://openairdocs.org/sdr/DXTA200702215), May 24, 2007: WARNING LIGHT. FALSE ACTIVATION. LT ENGINE N2 OVER SPEED LIGHT (RED) COMES ON DURING TAKEOFF ROLL. N1 WAS SET AT 96.7 AND N2 DIGITS INDICATE 94-95 PERCENT. (M2B) UPON ARRIVAL RAN ACFT TO TAKEOF
- [SDR DXTA200601588](https://openairdocs.org/sdr/DXTA200601588), Sep 1, 2006: ANTI-SKID SYS. MALFUNCTIONED. DURING TAXI-OUT FOR DEPARTURE, THE INITIAL BRAKE CHECK WAS GOOD. DURING ADDITIONAL BRAKING (ABOVE 12 KTS), THE BRAKES WOULD INITIALLY HOLD, THEN RELEASE & GRAB 
- [SDR DXTA200501127](https://openairdocs.org/sdr/DXTA200501127), Dec 4, 2005: PEDAL. LEAKING. LEFT BRAKE PEDAL ON LEFT SIDE INTERMITTANTLY LOSES HYDRAULIC PRESSURE. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200300087](https://openairdocs.org/sdr/DXTA200300087), Aug 17, 2003: BULB. BURNED OUT. RT MAIN LANDING GEAR LIGHT NOT ILLUMINATED WHEN GEAR CONTROL SELECTED DOWN ON APPROACH TO PHX, EMERGENCY GEAR EXTENSION SYSTEM ACTIVATED. TROUBLESHOT SYSTEM FOU
- [SDR 99ZZZX9](https://openairdocs.org/sdr/99ZZZX9), Feb 19, 1998: ACTUATOR. MISINSTALLED. DURING INSPECTION ATTEMPT TO LUBRICATE THE LEFT ELEVATOR TRIM ACTUATOR, DETERMINED THE PART NUMBER AND GREASE ZERT LOCATION WAS THAT OF THE RIGHT SIDE PART.

## 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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