# N314QS: 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: 50500158 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: August 20, 2013 - Certificate issued: August 29, 2023 - Expires: August 31, 2030 - Mode S code: A3571C - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314QS - Page: https://openairdocs.org/aircraft/N314QS 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 N314QS. ## NTSB investigations on N314QS not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ATL00IA035](https://openairdocs.org/ntsb/ATL00IA035), Mar 5, 2000: Cessna CE-560 (N314QS), Key Largo, FL, incident, minor damage. Probable cause: The malfunction of the nose gear locking mechanism for undetermined reason. ## FAA accident and incident reports None matched to N314QS. ## Reports on N314QS not matched to an aircraft (2) They name N314QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20020401008479I](https://openairdocs.org/incident/20020401008479I), Apr 1, 2002: Cessna 560CESSNA (N314QS), Lincoln, NE. (-23) Executive jet aviation flight 314, Cessna citation 560, was enroute at 41,000 feet from aspen, Colorado to columbus Ohio. Forty miles west of Lincoln, NE… - [Incident 20000305003389I](https://openairdocs.org/incident/20000305003389I), Mar 5, 2000: Gulstm 560 (N314QS), Key Largo, FL, Minor damage. Upon landing on runway 04 at the Ocean Reef Club Airport (X09) the nose gear collapsed. There were no indications of a hard landig and the aircraft received… ## Service difficulty reports (18) 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 DXTA2025051503463](https://openairdocs.org/sdr/DXTA2025051503463), May 12, 2025: CARTRIDGE. DEFECTIVE. FUEL PUMP 1 FAIL YELLOW CAS: AT 400 FEET AGL ON DEPARTURE GOT A FUEL LO PRES CAS, WHICH QUICKLY WENT AWAY AND REPLACED BY A FUEL PUMP 1 FAIL YELLOW CAS AND A FU - [SDR DXTA2025051203463](https://openairdocs.org/sdr/DXTA2025051203463), May 12, 2025: WARNING MESSAGE. ILLUMINATED. FUEL PUMP 1 FAIL YELLOW CAS: AT 400 FEET AGL ON DEPARTURE GOT A FUEL LO PRES CAS, WHICH QUICKLY WENT AWAY AND REPLACED BY A FUEL PUMP 1 FAIL YELLOW CAS AND A FU - [SDR DXTA2025031402646](https://openairdocs.org/sdr/DXTA2025031402646), Mar 11, 2025: BRAKE. NO DISCREPANCY. BRAKE CHECK UPON INTIAL TAXI ROLL CAUSED A CHATTER AND BOUNCING EFFECT UPON BRAKE APPLICATION. HARD TO TELL IF LEFT BRAKE, RIGHT BRAKE OR BOTH. SERVICED HYDRAUL - [SDR DXTA2025013002122](https://openairdocs.org/sdr/DXTA2025013002122), Jan 26, 2025: CONTROL LEVER. FAILED. NLG LANDING GEAR RETRACTION: ON DEPARTURE GEAR FAILED TO RETRACT AFTER GEAR UP SELECTED. RED INDICATION ON ALL 3 GEAR WITH VIBRATION . COMPLETED QRH AND HAD THR - [SDR DXTA2025012302036](https://openairdocs.org/sdr/DXTA2025012302036), Jan 19, 2025: CONTROL LEVER. DEFECTIVE. LG LEVER DISAG RED CAS: ON RETRACTING THE GEAR AFTER TAKEOFF, LG LEVER DISAG DISPLAYED WITH THREE RED DN INDICATIONS. AN UNUSUALLY LOUD RUMBLING SOUND DURING RE - [SDR DXTA2024121601523](https://openairdocs.org/sdr/DXTA2024121601523), Dec 13, 2024: AHRS. DEFECTIVE. VENTRAL RUD FAIL WHITE CAS: REPEAT WRITE UP. CAS ILLUMINATED IN FLIGHT, STARTED WITH YELLOW HDG FLAG FOLLOWED BY AP/YD/SWPS FAIL CAS MESSAGE. ALSO RECEIVED AHRS - [SDR DXTA2024121301495](https://openairdocs.org/sdr/DXTA2024121301495), Dec 12, 2024: DOOR. FROZEN. DOOR HANDLE PLACED IN THE OPEN POSITION, BUT LOCKING PINS WILL NOT RELEASE. DOOR CAN NOT BE OPENED. UNLOCKED CABIN DOOR AND OPENED AS NORMAL. NOTED WATER AROUND - [SDR DXTA2024120401379](https://openairdocs.org/sdr/DXTA2024120401379), Dec 2, 2024: WARNING MESSAGE. FALSE ACTIVATION. RECEIVED IN CONJUNCTION WITH AMBER AHRS 2 FAIL, AP FAIL, & YD FAIL. CORRECTIVE ACTION; POWERED UP AIRCRAFT AND ALLOWED FOR FULL BOOT UP, NO CAS MESSAGES POSTED. - [SDR DXTA2024082600331](https://openairdocs.org/sdr/DXTA2024082600331), Aug 25, 2024: SWITCH PANEL. DEFECTIVE. EMER LT NOT ARM YELLOW CAS: EMER LT NOT ARM YELLOW CAS IN FLIGHT. SWITCH IN THE ARM POSITION. INTERIOR EMER LIGHTS ILLUMINATED. CORRECTIVE ACTION: REMOVED INOP - [SDR DXTA2024032211272](https://openairdocs.org/sdr/DXTA2024032211272), Mar 22, 2024: SWITCH. MALFUNCTIONED. EMERGENCY LIGHTS STAY ON WHEN THE SWITCH IS IN THE ARM POSITION. REMOVED DEFECTIVE EMERGENCY LIGHT BATTERY 1 P/N:7450LS-00 S/N:005253 AND REPLACED WITH CUSTOMER - [SDR DXTA2024032011241](https://openairdocs.org/sdr/DXTA2024032011241), Mar 18, 2024: BATTERY. DISCHARGED. EMERGENCY LIGHTING: UPON LANDING OWNERS INFORMED US THE EMERGENCY LIGHTS HAD BEEN FLASHING FOR APPROXIMATLEY 45 MINUTES. I PLACED THE EMER LT SWITCH TO ALL 3 PO - [SDR DXTA2023101898250](https://openairdocs.org/sdr/DXTA2023101898250), Oct 17, 2023: BATTERY. MALFUNCTIONED. CABIN EMERG LIGHT: AT 43,000 ABOUT HOUR INTO FLIGHT CABIN EMERLIGHTING FLICKERING. LOOK AT VIDEO ATTACHMENT. REMOVED AND REPLACED #1 EMERGENCY BATTERY. REMOVED - [SDR DXTA2021122754180](https://openairdocs.org/sdr/DXTA2021122754180), Dec 26, 2021: NONE. DEFECTIVE. EMERG LIGHT SWITCH: EMER LIGHTS REMAIN ILLUMINATED WHEN IN THE ARM POSITION. // SIGNOFF// REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERY IN REF WITH PHENOM - [SDR 2021FA0000154](https://openairdocs.org/sdr/2021FA0000154), May 19, 2021: RECEPTACLE. BURNED. GROUND POWER UNIT (GPU) POWERED ON GROUND AND GPU EXTERNAL POWER RECEPTACLE STARTED BURNING AT CONNECTION ON AIRCRAFT AND AIRCRAFT EXTERNAL POWER RECEPTACLE ALS - [SDR 2020FA0000435](https://openairdocs.org/sdr/2020FA0000435), Oct 2, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTA - [SDR DXTA2019062002541](https://openairdocs.org/sdr/DXTA2019062002541), Jun 20, 2019: MODULE. BURNED. DURING MX EVENT FOUND COMPRESSOR DRIVE MODULE POWER TERMINAL AND ASSOCIATED CONNECTOR HEAT DAMAGED // SIGNOFF // REMOVED AND REPLACED COMPRESSOR DRIVE MODULE, P - [SDR DXTA2018011500479](https://openairdocs.org/sdr/DXTA2018011500479), Jan 15, 2018: FLAP SYSTEM. MALFUNCTIONED. ON DEPARTURE AND UPON RETRACTING THE FLAPS FROM FLAPS 1, RECEIVED A FLAPS FAIL CAS MESSAGE. THE FLAP INDICATOR WAS SHOWING AN X. QRH WAS PERFORMED. MOVING THE F - [SDR DXTA2015123006148](https://openairdocs.org/sdr/DXTA2015123006148), Dec 29, 2015: CONTROL UNIT. MALFUNCTIONED. BRAKE FAIL CAS MSG ON LANDING ROLL OUT, STILL HAD RT BRAKE WITH NO ANTI-SKID. ODOR NOTICED IN COCKPIT OF PLANE. ACFT WAS TOWED FROM TAXIWAY. TROUBLE SHOT BRAKE ## Service difficulty reports on N314QS not matched to an aircraft (17) They name N314QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2012101505146](https://openairdocs.org/sdr/DXTA2012101505146), Oct 14, 2012: UNKNOWN. ODOR. AFTER TAKEOFF, NOTICED A CHEMICAL ODOR. NO SMOKE IN CABIN. WENT ON OXYGEN AND RETURNED TO DEPARTURE. ON GROUND, RAN ENGINES INDEPENDENTLY AND NO ODOR DETECTED. - [SDR DXTA2010011103937](https://openairdocs.org/sdr/DXTA2010011103937), Jan 9, 2010: RMU. SHORTED. WHEN AVIONICS POWER WAS BROUGHT ON, ARCING SOUNDS WERE HEARD ALONG WITH THE ODOR OF BURNED ELECTRONICS. NO C/B POPPED. RMU 1 SCREEN FLICKERING RAPIDLY. REMOVED - [SDR DXTA2009050103627](https://openairdocs.org/sdr/DXTA2009050103627), Apr 30, 2009: BULB. INOPERATIVE. LEFT MLG INDICATOR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS PUT DOWN. ROTARY TEST: LIGHT OUT, UNLOCK LIGHT EXTINGUISHED. WITH FLAPS DOWN, THROTTLES IDLE, SPEED BE - [SDR DXTA200811083345](https://openairdocs.org/sdr/DXTA200811083345), Nov 8, 2008: PITOT TUBE. OBSTRUCTED. LT PITOT TUBE WAS OBSTRUCTED BY SOME FOREIGN DEBRIS DURING TAKEOFF ROLL, HAD TO ABORT. NO AIRSPEED ON CAPTAIN PFD. ABORTED AT 75 KTS. REMOVED FWD LT NOSE BAGGAG - [SDR DXTA2008111003345](https://openairdocs.org/sdr/DXTA2008111003345), Nov 8, 2008: UNKNOWN. MALFUNCTIONED. NO AIRSPEED ON CAPTAIN PFD. ABORTED AT 75 KTS. - [SDR DXTA200803035](https://openairdocs.org/sdr/DXTA200803035), Apr 30, 2008: BRAKE. WEAK. RT SEAT BRAKES ARE SPONGY. PERFORMED BRAKE BLEED ON BOTH BRAKES, NO LEAKS NOTED & BRAKES ARE GOOD REF CE560E 32-42-00. - [SDR DXTA200802765](https://openairdocs.org/sdr/DXTA200802765), Jan 13, 2008: WIRE HARNESS. SHORTED. AT APPROXIMATELY 70 KNOTS THE ANTI-SKID INOP LIGHT CAME ON. ABORTED THE TAKEOFF. REMOVED THE LT ANTI-SKID TRANSDUCER WIRE BUNDLE FROM LEFT GEN TO WHEEL WELL CON - [SDR DXTA200701991](https://openairdocs.org/sdr/DXTA200701991), Mar 2, 2007: STATIC INVERTER. DISCONNECTED. RT PFD FAILURE ATTITUDE AND HEADING FLASH RAPIDLY ATT ANNUNCIATOR ON LT PFD FLASHES. HAPPENS INTERMITTENTLY. AUTOPILOT DISCONNECTS FREQUENTLY WHEN COUPLED TO RT - [SDR DXTA200701936](https://openairdocs.org/sdr/DXTA200701936), Feb 13, 2007: BULB. BURNED OUT. LEFT GEAR LIGHT DID NOT ILLUMINATE WITH THE GEAR DOWN CONFIRMED LIGHT INOP WITH ROTARY TEST. CYCLED GEAR 3 TIMES WITH NO CHANGE. VISUALLY CONFIRMED GEAR EXTENDE - [SDR DXTA200701890](https://openairdocs.org/sdr/DXTA200701890), Jan 29, 2007: TIRE. SMOKE. UPON TAXI IN THE LINE PERSONNEL ADVISED US THAT THE RT MAIN GEAR WAS SMOKING. THERE APPEARS TO BE A FILM OF OIL OR GREASE ON THE OUTSIDE AND PORTIONS OF THE INS - [SDR DXTA200501167](https://openairdocs.org/sdr/DXTA200501167), Dec 21, 2005: WIRE. BROKEN. WHILE AIRCRAFT WAS STOPPED AND RT SIDE BRAKE PRESSED POWER LO PRESSURE AND ANTI-SKID ANNUNCIATORS ILLUMINATED. INITIALLY HAD SOME BRAKE PRESSURE. TAXIED CLEAR O - [SDR DXTA200500775](https://openairdocs.org/sdr/DXTA200500775), Jun 14, 2005: PUMP. LEAKING. ON SHORT FINAL, ANTI-SKID INOP AND POWER BRAKE LOW PRESS LIGHTS ILLUMINATED. NO BRAKES ON LANDING. LARGE HYD FLUID LEAK NOTICED ON POST FLIGHT. FLUID ON NOSE GE - [SDR DXTA200400467](https://openairdocs.org/sdr/DXTA200400467), Dec 5, 2004: CLIP. DAMAGED. ON LANDING PILOT APPLIED BRAKES WITH NO RESPONSE (HARD PEDAL) COPILOT APPLIED BRAKES WITH SAME RESULT. SEVERAL APPLICATIONS WERE MADE. AT 70KIAS BRAKES LOCKED M - [SDR DXTA200400401](https://openairdocs.org/sdr/DXTA200400401), Sep 20, 2004: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF, RT MAIN GEAR WOULD NOT RETRACT, FLYING AT APPROX. 200 KTS. THE RT MAIN GEAR LIGHT WAS ON ALONG WITH THE GEAR UNSAFE LIGHT, THE HYDRAULIC LIGHT DI - [SDR DXTA200400256](https://openairdocs.org/sdr/DXTA200400256), Mar 8, 2004: BRAKE ASSY. INTERMITTENT. ON LANDING BRAKES FELT WEAK, DURING TAXI BRAKES FUNCTIONED INTERMITTENTLY UNTIL BRAKES FAILED COMPLETELY, USED EMERGENCY BRAKES TO STOP AIRCRAFT. ITEM IS UNDER - [SDR CJ62002F00000](https://openairdocs.org/sdr/CJ62002F00000), Jul 1, 2002: LINE. CHAFED. NOTICED HYDRAULIC FLUID LEAKING ON NOSE STRUT. FOUND NOSE GEAR EXTEND HYDRAULIC LINE SEVERELY CHAFED AND LEAKING FLUID. LINE WAS POSITIONED SUCH THAT EVERY TIME - [SDR 98ZZZX984](https://openairdocs.org/sdr/98ZZZX984), Feb 10, 1998: CONNECTOR. MISMARKED. CONNECTOR FOR OIL TEMPERATURE AT ENGINE MISLABELED, P.93. PER MANUFACTURER, CONNECTOR SHOULD BE LABELED P.87. ## 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 --- 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.