# N398QS: 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: 50500371
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: September 14, 2016
- Certificate issued: May 27, 2025
- Expires: May 31, 2032
- Mode S code: A4A1F0
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=398QS
- Page: https://openairdocs.org/aircraft/N398QS

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 N398QS.

## FAA accident and incident reports

None matched to N398QS.

## 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 DXTA2025122606272](https://openairdocs.org/sdr/DXTA2025122606272), Dec 23, 2025: BATTERY. FAULTY. UPON DESCENT INTO KILM THE EMERGENCY LIGHTS STARTED TO FLICKER. AFTER LANDING, SHUT THE BATTERIES OFF, AND UNPLUGGED THE MAIN BATTERY TO POSSIBLY DO A RESET. AF
- [SDR DXTA2025070304112](https://openairdocs.org/sdr/DXTA2025070304112), Jul 2, 2025: BATTERY PACK. INOPERATIVE. ON DEPARTURE CABIN EMER LIGHTS BEGAN FLASHING. UPON ARRIVAL INTO DAL, WHEN EMER LIGHTS SELECTED TO ARM, LIGHTS IN CABIN WERE ON CONTINUOSLY. REPLACED #2 EMERGEN
- [SDR DXTA2024080600098](https://openairdocs.org/sdr/DXTA2024080600098), Aug 4, 2024: LANDING GEAR. FAILED. DURING INITIAL CLIMB OUT FROM KBFI, NLG FAILED TO RETRACT. QRH PROCEDURE WAS RUN AND UNSUCCESSFUL AT RETRACTING NLG. PRECAUTIONARY LANDING WAS COMPLETED BACK TO
- [SDR DXTA2024012310704](https://openairdocs.org/sdr/DXTA2024012310704), Jan 22, 2024: UNKNOWN. ODOR. IMMEDIATELY AFTER TAKEOFF HEAVY, BURNING PLASTIC, SMELL IN COCKPIT AND CABIN FOR APPROXIMATELY 15 MINUTES SOMETIMES LONGER. BELIEVE THIS IS ASSOCIATED WITH ENGI
- [SDR DXTA2023112010082](https://openairdocs.org/sdr/DXTA2023112010082), Nov 18, 2023: CONTROL PANEL. DEFECTIVE. EMERGENCY LIGHTING: AFTER SHUTDOWN FLOW, INTERIOR AND EXTERIOR EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE OFF POSITION. //SIGNOFF// REMOVED FAULTY LIGH
- [SDR DXTA2023102498660](https://openairdocs.org/sdr/DXTA2023102498660), Oct 23, 2023: BATTERY. INOPERATIVE. CABIN EMERG LIGHT: AT CRUISE THE EMER LIGHTS STARTER FLASHING WITH THE SWITCH IN THE ARM POSITION. REMOVED INOP #1 EMERGENCY BATTERY PN 7450LS-00 SN 006774 INST
- [SDR DXTA2023091195130](https://openairdocs.org/sdr/DXTA2023091195130), Sep 10, 2023: UNKNOWN. UNKNOWN. MAIN EXIT SIGN/LIGHT: LOWER EXIT LIGHT NEAR MAIN CABIN DOOR INOP. FOUND EXIT SIGN LIGHT ELECTRICAL CONNECTION DISENGAGED. CONNECTED EXIT SIGN LIGHT IAW EMB PHEN
- [SDR DXTA2023060187520](https://openairdocs.org/sdr/DXTA2023060187520), Jun 1, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: DURING FLIGHT WITH THE EMER LT SWITCH SET TO ARM, CABIN EMERGENCY LIGHTS WERE ILLUMINATED AND FLASHING INTERMITTENTLY DURING INITIAL CLIMB UN
- [SDR DXTA2023030882190](https://openairdocs.org/sdr/DXTA2023030882190), Mar 7, 2023: NONE. DEFECTIVE. SHORTLY AFTER LEVELING OFF AT FL410, PASSENGERS NOTICED A BURNT SMELL IN THE BACK. THE SMELL DISSIPATED WITHIN FIVE MINUTES, AND NO SMOKE WAS OBSERVED. SHORTLY 
- [SDR DXTA2022062964940](https://openairdocs.org/sdr/DXTA2022062964940), Jun 28, 2022: BALANCE WEIGHT. OUT OF ADJUST. MAIN DOOR: WHEN DOOR IS OPENED IT DOES NOT SELF BRAKE . DOOR FALLS STRAIGHT TO STOPPING POINT AND BOUNCES TO REST // SIGNOFF//REMOVED MAIN DOOR LINING AND REMOV
- [SDR DXTA2022051962060](https://openairdocs.org/sdr/DXTA2022051962060), May 18, 2022: NONE. NONE. MAIN DOOR HANDLE: MAIN DOOR HANDLE BROKE OFF COMPLETELY. CAN NOT SHUT DOOR OR LOCK DOOR FROM OUTSIDE.
- [SDR DXTA2022041860520](https://openairdocs.org/sdr/DXTA2022041860520), Apr 16, 2022: NONE. DEFECTIVE. SPEED BRAKE INDICATION: ON APPROACH WHEN ATTEMPTING TO DEPLOY SPEED BRAKE, SPOILER FAULT CASS ILLUMINATED, FOLLOWED BY GROUND SPOILER FAIL YELLOW CASS. SPEED BR
- [SDR 2020FA0000421](https://openairdocs.org/sdr/2020FA0000421), Sep 22, 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 LT ELEVATOR: ADJUSTABL
- [SDR DXTA2017111200001](https://openairdocs.org/sdr/DXTA2017111200001), Nov 16, 2017: UNKNOWN. ODOR. DURING DEPARTURE, CREW DETECTED FUMES IN COCKPIT THAT SMELLED LIKE AN IRON BURNING THROUGH CLOTH. FUMES SUBSIDED ENROUTE AFTER THROTTLE REDUCTION BUT WAS INTERM

## Service difficulty reports on N398QS not matched to an aircraft (27)

They name N398QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010070704146](https://openairdocs.org/sdr/DXTA2010070704146), Jul 2, 2010: INDICATOR. INOPERATIVE. RT SIDE FUEL GAUGE INDICATING 400-500 LBS LESS THAN LT SIDE. THE RT SIDE APPEARED TO DROP AS WE LEVELED AT CRUISE ALTITUDE OF FL400. IMBALANCE REMAINED ALL THE 
- [SDR DXTA2009052803670](https://openairdocs.org/sdr/DXTA2009052803670), May 28, 2009: COALESCER BAG. DIRTY. RAN EACH ENGINE SEPEREATELY FOR TROUBLESHOOTING AND COULD NOT GET ANY FAULTS. REMOVED, INSPECTED AND CLEANED THE WATER SOCK. RAN ENGINES AGAIN WITHOUT FAULT. AL
- [SDR DXTA200905283670](https://openairdocs.org/sdr/DXTA200905283670), May 28, 2009: UNKNOWN. ODOR. AFTER ENGINES WERE STARTED AND RUNNING STRONG FUMES (SIMILAR TO CAR EXHAUST FUMES) WAS COMING OUT OF ALL WEMAC OUTLETS. THERE WERE NO OTHER A/C'S ON RAMP WITH E
- [SDR DXTA2009041303595](https://openairdocs.org/sdr/DXTA2009041303595), Apr 11, 2009: ANTI-ICE SYSTEM. MALFUNCTIONED. ANTI-SKID APPEARS TO RELEASE BRAKE PRESSURE DURING LANDING TAXI ROLL. TIGHTENED THE DRIVE CLIPS ON WHEEL COVERS OPS CHECKS GOOD IAW MM 32-42-00 OPS CHECK GOOD. 
- [SDR DXTA2008120403386](https://openairdocs.org/sdr/DXTA2008120403386), Dec 4, 2008: ROD END. STRIPPED. RT ENGINE QUIT WHEN THROTTLE WAS BROUGHT TO IDLE. REMOVED AND REPLACED RT ENGINE FLOW DIVIDER ROD END AND RIGGED IAW MM 71-01-03. GROUND RUN OPS NORMAL IAW MM 7
- [SDR DXTA2008120503386](https://openairdocs.org/sdr/DXTA2008120503386), Dec 4, 2008: ENGINE. STOPPED. RT ENGINE QUIT WHEN THROTTLE WAS BROUGHT TO IDLE.
- [SDR DXTA200809243287](https://openairdocs.org/sdr/DXTA200809243287), Sep 24, 2008: WIRE HARNESS. SHORTED. UPON LANDING ROLLOUT, BRAKES VERY WEAK, FEELS LIKE ANTI-SKID KICKING IN, TAKES EXCESSIVE DISTANCE TO STOP ON TAXI-IN. PERFORMED TAXI CHECK OF ACFT AND FOUND BRA
- [SDR DXTA20080924](https://openairdocs.org/sdr/DXTA20080924), Sep 24, 2008: WIRE HARNESS. SHORTED. UPON LANDING ROLLOUT, BRAKES VERY WEAK, FEELS LIKE ANTI-SKID KICKING IN, TAKES EXCESSIVE DISTANCE TO STOP ON TAXI-IN. PERFORMED TAXI CHECK OF ACFT AND FOUND BRA
- [SDR DXTA200803287](https://openairdocs.org/sdr/DXTA200803287), Sep 24, 2008: BRAKE. WEAK. UPON LANDING ROLLOUT, BRAKES VERY WEAK.
- [SDR DXTA200803251](https://openairdocs.org/sdr/DXTA200803251), Aug 27, 2008: WIRE HARNESS. MISREPAIRED. BRAKING UPON TOUCHDOWN WAS NON-EXISTANT FOR APPROX 2-3 SECONDS FOLLOWING TOUCHDOWN. INSPECTED LT WHEEL WELL HARNESS FOUND ANTISKID WIRING AT CONN PL008 REPAIRED
- [SDR DXT2008F00002](https://openairdocs.org/sdr/DXT2008F00002), Aug 27, 2008: BRAKE SYS. INOPERATIVE. BRAKING UPON TOUCHDOWN WAS NONEXISTENT FOR APPROX 2-3 SECONDS FOLLOWING TOUCHDOWN.
- [SDR DXTA200808263248](https://openairdocs.org/sdr/DXTA200808263248), Aug 26, 2008: RELAY. MALFUNCTIONED. REPEAT WRITE UP INITIAL BRAKE CHECK ON F/O SIDE UPON LEAVING CHOCKS IS SATISFACTORY. HOWEVER, AFTER FLIGHT THE F/O BRAKES ARE COMPLETELY INEFFECTIVE (BOTH SOFT 
- [SDR DXT2008F00001](https://openairdocs.org/sdr/DXT2008F00001), Aug 26, 2008: BRAKE SYS. DEFECTIVE. INITIAL BRAKE CHECK ON F/O SIDE UPON LEAVING CHOCKS IS SATISFACTORY. HOWEVER, AFTER FLIGHT THE F/O BRAKES ARE COMPLETELY INEFFECTIVE.
- [SDR DXTA200808153230](https://openairdocs.org/sdr/DXTA200808153230), Aug 16, 2008: BRAKE. WEAK. F/O RT PEDAL, GOES TO THE FWD STOP WHEN INITIALLY DEPRESSED; WHEN BRAKE IS PUMPED, LIMITED BRAKING RETURNS; F/O LT BRAKE PEDAL IS "SPONGY", REQUIRING GREATER TH
- [SDR DXTA200803230](https://openairdocs.org/sdr/DXTA200803230), Aug 16, 2008: BRAKE. WEAK. FIRST OFFICER`S RIGHT PEDAL GOES TO THE FORWARD STOP WHEN INITIALLY DEPRESSED. WHEN BRAKE IS PUMPED, LIMITED BRAKING RETURNS. FIRST OFFICER`S LT BRAKE PEDAL IS 
- [SDR DXTA200808/033214](https://openairdocs.org/sdr/DXTA200808%2F033214), Aug 3, 2008: BRAKE ASSY. WEAK. CO-PILOT'S BRAKES ARE VERY SQUISHY. TAKE MUCH MORE THEN NORMAL PRESSURE WHEN APPLYING BRAKES. VISUALLY INSPECTED RUDDER PEDAL MOUNT WEBBING FOR CRACKS AND FOUND
- [SDR DXTA200803214](https://openairdocs.org/sdr/DXTA200803214), Aug 3, 2008: BRAKE SYS. MALFUNCTIONED. CO-PILOT`S BRAKES ARE VERY SQUISHY. TAKES MUCH MORE THAN NORMAL PRESSURE WHEN APPLYING BRAKES. (S)
- [SDR DXTA200803154](https://openairdocs.org/sdr/DXTA200803154), Jun 29, 2008: BRAKE SYS. MALFUNCTIONED. CO PILOTS SIDE BRAKES-VERY LITTLE PRESSURE ON LANDING (PEDALS COMPRESS FULLY), THEY WORK BETTER DURING TAXI. CAPTAINS SIDE BREAKS NORMAL. BLED BRAKES IAW ENGINE
- [SDR DXTA200802972](https://openairdocs.org/sdr/DXTA200802972), Mar 30, 2008: ACTUATOR. VIBRATION. VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF). REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW THE CHAP 32-21-03. LEAK AND OPERATIONAL C
- [SDR DXTA20082972](https://openairdocs.org/sdr/DXTA20082972), Mar 30, 2008: WHEEL. VIBRATION. VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF).
- [SDR DXTA200702590](https://openairdocs.org/sdr/DXTA200702590), Nov 3, 2007: RESERVOIR. LOW. CO-PILOT'S RT BRAKE IS SPONGY, WILL PUMP UP AFTER SEVERAL APPLICATIONS. INSPECTED RESERVOIR, PUMP/MOTOR, ACCUMULATOR, ANTISKID VALVES FITTINGS, (4) MASTER CYLIN
- [SDR DXTA200702578](https://openairdocs.org/sdr/DXTA200702578), Oct 28, 2007: MASTER CYLINDER. LEAKING. DURING TAXI OUT, CO-PILOTS RT BRAKE IS SPONGY CAUSING A/C TO VEER LT. FOUND CO-PILOTS RT MASTER CYLINDER LEAKING. REMOVED AND REPLACED MASTER CYLINDER WITH NEW 
- [SDR DXTA200702490](https://openairdocs.org/sdr/DXTA200702490), Sep 20, 2007: BRAKE. WEAK. CO-PILOTS RT BRAKE GOES SOFT. CAN BE PUMPED UP BUT GOES SOFT AGAIN. 09-28-07 BLED RT BRAKE. OPS CHECKS GOOD. WORK DONE IAW CITATION 560 M/M 32-42-00.
- [SDR DXTA200702442](https://openairdocs.org/sdr/DXTA200702442), Sep 2, 2007: BRAKE ASSY. WEAK. COPILOTS RT BRAKE PEDAL IS SOFT.
- [SDR DXTA200601326](https://openairdocs.org/sdr/DXTA200601326), Mar 31, 2006: TRANSDUCER. INOPERATIVE. DURING LANDING, BRAKES GRAB THEN FADE MULTIPLE TIMES, BRAKE PRESSURE REMAINS GOOD. REPLACED LEFT MAIN WHEEL TRANSDUCER. INSTALLED AN OVERHAULED UNIT BY HYDRO-AI
- [SDR DXTA200500651](https://openairdocs.org/sdr/DXTA200500651), Mar 30, 2005: BRAKE. MALFUNCTIONED. CO-PILOT LEFT BRAKE PEDAL EXCESSIVE TRAVEL & SPONGY. CHECKED BRAKE ASSEMBLIES, ALL VISIBLE BRAKE LINES, MASTER CYLINDERS, & RESERVOIR FOR LEAKS, NONE FOUND. CHE
- [SDR DXTA200300105](https://openairdocs.org/sdr/DXTA200300105), Aug 27, 2003: BRAKE ASSY. INTERMITTENT. BRAKE PEDALS FEEL SOFT DURING USE, BRAKES GRAB AND RELEASE INTERMITTENTLY DURING LANDING DECELERATION. JACKED A/C INSPECTED BRAKES AND ENGAGEMENT OF ANTI-SKID, 

## 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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