# N436QS: 2019 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: 50500525
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: August 14, 2019
- Certificate issued: June 30, 2026
- Expires: June 30, 2033
- Mode S code: A53AD7
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=436QS
- Page: https://openairdocs.org/aircraft/N436QS

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 N436QS.

## FAA accident and incident reports

None matched to N436QS.

## Service difficulty reports (9)

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 DXTA2024101100796](https://openairdocs.org/sdr/DXTA2024101100796), Oct 8, 2024: CONTROL UNIT. FAILED. MLG BRAKE PRESSURE: UPON TAXI OUT I APPLIED BRAKE PRESSURE TO MAKE THE INITIAL TURN OUT OF ATLANTIC AVIATION. I NOTICED THE BRAKES IMMEDIATELY FELT "MUSHY" AND 
- [SDR DXTA2024082600324](https://openairdocs.org/sdr/DXTA2024082600324), Aug 24, 2024: INDICATOR. OBSTRUCTED. MAIN DOOR VISUAL INDICATOR: MAIN CABIN DOOR LOWER RIGHT LOCKING INDICATOR GREEN FLAG IS EITHER OBSCURED OR NOT SHOWING IN THE VIEW WINDOW. CORRECTIVE ACTION: RE
- [SDR DXTA2024081900219](https://openairdocs.org/sdr/DXTA2024081900219), Aug 15, 2024: BLOWER. FAILED. AIR DISTRIBUTION: WHILE CRUISING AT FL 400 WE SMELLED SMOKE/ FUMES IN THE COCKPIT. WE COULD NOT LOCATE THE SOURCE OF IT. THE SMELL/ FUME GOT STRONGER AS TIME PR
- [SDR DXTA2023112910174](https://openairdocs.org/sdr/DXTA2023112910174), Nov 28, 2023: BATTERY. FAULTED. CABIN EMERGENCY LIGHTS FLASHING INFLIGHT. REMOVED FAILED FWD BATTERY PACK & INSTALLED REPAIRED UNIT IAW AMM 33-52-01. REMOVED FAILED AFT BATTERY PACK & INSTALLE
- [SDR DXTA2023061288430](https://openairdocs.org/sdr/DXTA2023061288430), Jun 12, 2023: UNKNOWN. UNKNOWN. NLG LANDING GEAR RETRACTION: ON DEPARTURE AFTER GEAR RETRACTION THE LG LEVER DISAG CAS CAME ON. QRH COMPLETED BUT DID NOT FIX PROBLEM. NOSE GEAR DID NOT RETRACT
- [SDR DXTA2023062287720](https://openairdocs.org/sdr/DXTA2023062287720), Jun 3, 2023: BRAKE. DEFECTIVE. RIGHT MLG BRAKE: WHILE TAXIING TO RUNWAY THE RIGHT BRAKE STARTED LOCKING UP WHEN DEPRESSING THE BRAKE PEDAL, NO MATTER HOW GENTLY. IT SENT EXTREME SHUDDERS THRO
- [SDR DXTA2022122977370](https://openairdocs.org/sdr/DXTA2022122977370), Dec 28, 2022: BRAKE SYS. INOPERATIVE. UPON POWERING UP THE ENGINES FOR TAKEOFF WITH THE BREAKS HELD FOR A STATIC TAKEOFF, YELLOW BRK FAIL CAS MESSAGE CAME ON AND THE BREAKS NO LONGER WORKED AT ALL. 
- [SDR DXTA2022091570390](https://openairdocs.org/sdr/DXTA2022091570390), Sep 14, 2022: NONE. DEFECTIVE. CABIN EMERG LIGHT: ALL EMERGENCY LIGHTS CONTINUOUSLY FLICKER WITH SWITCH SELECTED TO ARMED AND ON POSITIONS. VIDEO ATTACHED. POWERD UP AIRCRAFT AND FOUND LIGHTS
- [SDR DXTA2020102504269](https://openairdocs.org/sdr/DXTA2020102504269), Oct 25, 2020: BATTERY PACK. INOPERATIVE. THE EMERGENCY LIGHTS BEGAN BLINKING WHILE IN THE ARM AND ON POSITIONS. CORRECTIVE ACTION: INSTALLED REPAIRED FWD EMERGENCY BATTERY AND MODIFIED AFT EMERGENCY BA

## Service difficulty reports on N436QS not matched to an aircraft (27)

They name N436QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR G02R20170802004](https://openairdocs.org/sdr/G02R20170802004), May 25, 2017: FLOORBOARD. PUNCTURED. FLOORBOARD PUNCTURED IN THE TOP SKIN OF FLOOR.
- [SDR G02R20170724011](https://openairdocs.org/sdr/G02R20170724011), May 22, 2017: FITTING. CORRODED. LEFT AND RIGHT HORIZ STAB PIVOT BUSHINGS AND LUGS CORRODED.
- [SDR G02R20170724010](https://openairdocs.org/sdr/G02R20170724010), May 22, 2017: HINGE FITTING. CORRODED. VERTICAL FIN, RUDDER HINGE, UPPER FITTING IS CORRODED.
- [SDR G02R20170724009](https://openairdocs.org/sdr/G02R20170724009), May 22, 2017: HINGE FITTING. CORRODED. VERTICAL FIN, RUDDER HINGE, CENTER FITTING IS PITTED
- [SDR G02R20170724008](https://openairdocs.org/sdr/G02R20170724008), May 22, 2017: HINGE FITTING. CORRODED. VERTICAL FIN, RUDDER HINGE, LOWER FITTING IS PITTED.
- [SDR G02R2017080100003](https://openairdocs.org/sdr/G02R2017080100003), May 18, 2017: TORQUE TUBE. CORRODED. RUDDER TORQUE TUBE IS PITTED BEYOND THE ALLOWABLE DAMAGE LIMITS
- [SDR G02R08012017002](https://openairdocs.org/sdr/G02R08012017002), May 18, 2017: HINGE FITTING. CORRODED. RIGHT NR 4 ELEVATOR HINGE HAS PITTED CORROSION, TOP AND BOTTON CONTACT SURFACES.
- [SDR G02R08012017001](https://openairdocs.org/sdr/G02R08012017001), May 18, 2017: HINGE FITTING. CORRODED. RIGHT ELEVATOR HINGE LINE NR 1 ON HORIZONTAL STAB HAS PITTED CORROSION AND ELONGATION IN BOTTOM FITTING.
- [SDR G02R07242017007](https://openairdocs.org/sdr/G02R07242017007), May 18, 2017: HINGE FITTING. CORRODED. RT ELEVATOR HINGE LINE NR 4 CORRODED.
- [SDR G02R20170724006](https://openairdocs.org/sdr/G02R20170724006), May 18, 2017: HINGE. CORRODED. LEFT ELEVATOR HINGE CORRODED.
- [SDR G02R20170724005](https://openairdocs.org/sdr/G02R20170724005), May 18, 2017: HINGE FITTING. CORRODED. LT ELEVATOR HINGE LINE NR 4 CORRODED.
- [SDR G02R20170724004](https://openairdocs.org/sdr/G02R20170724004), May 18, 2017: HINGE FITTING. CORRODED. RIGHT ELEVATOR HINGE LINE NR 3 CORRODED.
- [SDR G02R20170724003](https://openairdocs.org/sdr/G02R20170724003), May 18, 2017: HINGE FITTING. CORRODED. LEFT ELEVATOR HINGE LINE NR 3 CORRODED.
- [SDR G02R20170724002](https://openairdocs.org/sdr/G02R20170724002), May 18, 2017: HINGE FITTING. CORRODED. RIGHT ELEVATOR HINGE LINE NR 2 HAS CORROSION.
- [SDR G02R20170724001](https://openairdocs.org/sdr/G02R20170724001), May 18, 2017: HINGE FITTING. CORRODED. LEFT ELEVATOR HINGE LINE NR 2 ON HORIZONTAL STAB HAS CORROSION BOTH FITTINGS.
- [SDR GR4220160913001](https://openairdocs.org/sdr/GR4220160913001), Sep 7, 2016: FITTING. GOUGED. LEFT ENGINE AFT MOUNT FITTING HAS GOUGES AND SCRATCHES ON THE AFT VIBRATION ISOLATOR FITTING ON THE FORWARD FACE IN SEVERAL LOCATIONS.
- [SDR DXTA2013110705560](https://openairdocs.org/sdr/DXTA2013110705560), Nov 6, 2013: APU. ODOR. AIR CONDITIONING SYSTEM PRODUCED A DIRTY SOCK ODOR. REMOVED LEFT AND RIGHT WATER SEPARATOR COALESCER BAG AND INSTALLED NEW. COMPLIED WITH CMP 215005 AIR CONDITI
- [SDR DXTA2012110505166](https://openairdocs.org/sdr/DXTA2012110505166), Nov 2, 2012: COALESCER BAG. ODOR. DURING CLIMB, NOTICED A VERY STRONG EXHAUST ODOR THROUGHOUT THE ENTIRE CABIN. THE ODOR TEMPORARILY FADED BUT REAPPEARED ABOUT 10 MINUTES INTO THE FLIGHT AND REM
- [SDR DXTA2011012704434](https://openairdocs.org/sdr/DXTA2011012704434), Jan 24, 2011: COALESCER BAG. ODOR. STRONG EXHAUST & FUEL ODOR PREVALENT IN CABIN UPON DESCENT. ODOR WAS VERY STRONG AND WAS FIRST NOTICED ON DESCENT THROUGHOUT APPROXIMATELY 10,000FT. R & R WATER
- [SDR N93A07232010](https://openairdocs.org/sdr/N93A07232010), Jul 23, 2010: OVEN. ODOR. ABOUT 30 MINUTES INTO FLIGHT, THE F/A TURNED THE OVEN ON TO WARM SOME BREAD. WITHIN A FEW MINUTES SHE NOTICED THE AREA HAD AN ELECTRICAL BURNING ODOR AND AN ODO
- [SDR N93A04062010](https://openairdocs.org/sdr/N93A04062010), Apr 6, 2010: SAFETY VALVE. MALFUNCTIONED. DURING CLIMB, CABIN PRESURIZATION BECAME ERRATIC AND UNCONTROLABLE. CREW DESCENDED IMEDIATELY. CABIN LOW WARNING ILLUMINATED. OPEN.
- [SDR N93A03222010](https://openairdocs.org/sdr/N93A03222010), Mar 22, 2010: THROTTLE CABLE. BROKEN. CREW REPORTED LT THROTTLE IS LOOSE AND INOPERATIVE. MX FOUND LT THROTTLE CABLE BROKEN UNDER FLOOR IN AFT LAV JUST FWD OF WHERE CABLE TURNS UPWARD AT AFT LAV AFT
- [SDR 143612282005](https://openairdocs.org/sdr/143612282005), Dec 28, 2005: WIRE HARNESS. FAILED. STEER BY WIRE FAILURE ON LANDING ROLLOUT.
- [SDR 14361216052](https://openairdocs.org/sdr/14361216052), Dec 16, 2005: SERVO VALVE. FAILED. NOSE STEERING FAILED ON LANDING.
- [SDR 1436121605](https://openairdocs.org/sdr/1436121605), Dec 16, 2005: MANIFOLD. FAILED. STEER BY WIRE FAILED ON LANDING.
- [SDR 1436120405](https://openairdocs.org/sdr/1436120405), Dec 4, 2005: STEERING SYS. OUT OF ADJUST. STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW GIV MM 32-05-00.
- [SDR 143612042005](https://openairdocs.org/sdr/143612042005), Dec 4, 2005: STEERING SYS. MALFUNCTIONED. STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW MM 32-05-00.

## 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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