# N328QS: 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: 50500175 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, commuter - Airworthiness date: November 22, 2013 - Certificate issued: August 20, 2026 - Expires: August 31, 2033 - Mode S code: A38D77 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=328QS - Page: https://openairdocs.org/aircraft/N328QS 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 N328QS. ## FAA accident and incident reports None matched to N328QS. ## 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 DXTA2026092109742](https://openairdocs.org/sdr/DXTA2026092109742), Sep 16, 2026: RELIEF VALVE. DEFECTIVE. DURING CRUISE RECEIVED AN EMER BRK LOW PRESSURE CAS. PRESSURE WAS APPROXIMATLEY 150PSI AND CONTINUED TO DROP. SOMETIME BETWEEN TOUCHDOWN AND ENGINE SHUTDOWN PRE - [SDR DXTA2025092405053](https://openairdocs.org/sdr/DXTA2025092405053), Sep 22, 2025: BATTERY. FAULTED. DURING FLIGHT ALL INTERIOR EMER LIGHTS ILLUMINATED. EMER LIGHT SWITCH IN ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY LIGHT BATTERIES WITH CUSTOMER - [SDR DXTA2024090900454](https://openairdocs.org/sdr/DXTA2024090900454), Sep 6, 2024: LIGHT. DETACHED. CABIN EMERG LIGHT: EMER AISLE LIGHT BETWEEN SEATS 1 AND 2 IS NOT MOUNTED PROPERLY CORRECTIVE ACTION: REINSTALLED EMERGENCY AISLE LIGHT BETWEEN SEATS 1 AND 2. OP - [SDR DXTA2023080492240](https://openairdocs.org/sdr/DXTA2023080492240), Aug 4, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: DURING BEFORE START FLOW AFTER ARMING EMG LIGHTS THEY REMAINED EMG LT NOT ARM. TRIED CHARGING THEM FOR 20MINS WITH GPU BUT DID NOT HELP. PERF - [SDR DXTA2023062689470](https://openairdocs.org/sdr/DXTA2023062689470), Jun 26, 2023: BATTERY PACK. DEFECTIVE. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLASH WHILE IN FLIGHT. TURNING SWITCH TO OFF TURNS THEM OFF BUT WHENEVET THE SWITCH IS IN THE ARM POSITION THEY FLASH. - [SDR DXTA2023062689550](https://openairdocs.org/sdr/DXTA2023062689550), Jun 26, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS FLASH WHILE IN FLT. TURNING SWITCH TO OFF TURNS THEM OFF BUT WHEN EVER THE SWITCH IS IN THE ARM POSITION THEY FLASH. REMOVED FAULTY #1 EMERGENC - [SDR DXTA2023020980180](https://openairdocs.org/sdr/DXTA2023020980180), Feb 9, 2023: PRESSURE SWITCH. DEFECTIVE. BRK FAIL YELLOW CAS: WHITE HYD SYS FAULT ADVISORY POSTED DURING CLIMB APPROXIMATELY 12000', FOLLOWED BY BRK FAIL YELLOW CAS APPROXIMATELY 15 MINUTES LATER. COMP - [SDR DXTA2021081646890](https://openairdocs.org/sdr/DXTA2021081646890), Aug 13, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: IN FLIGHT EMER LT NOT ARM YELLOW CAS MESSAGE CAME ON INTERMITTANTLY. EMERGENCY LIGHTING CAME AND STAYED ON WITH THE SWITCH IN ARM. // SIGNOFF - [SDR 2021F00025](https://openairdocs.org/sdr/2021F00025), Feb 7, 2021: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEV - [SDR 2021F00020](https://openairdocs.org/sdr/2021F00020), Feb 5, 2021: BATTERY PACK. NO TEST. THE COCKPIT LOCATION EMERGENCY LIGHTS BATTERY FAILED SCHEDULED FUNCTIONAL TEST. BATTERY ASSEMBLY WAS REPLACED WITH A REPAIRED BATTERY AND NO FURTHER DEFECTS WER - [SDR DXTA2019091102836](https://openairdocs.org/sdr/DXTA2019091102836), Sep 10, 2019: WARNING SYSTEM. FALSE ACTIVATION. FLAP FAIL YELLOW CAS ILLUMINATED - IN CRUISE AT FL410 CREW RECEIVED THE FOLLOWING CAS MESSAGES (ALL CONSISTENT WITH FCE 1 FAIL): YELLOW SWPS FAULT, FLAP FAIL, A - [SDR DXTA2015092206089](https://openairdocs.org/sdr/DXTA2015092206089), Sep 21, 2015: ENGINE. ODOR. RETURNING TO THE GATE, ODOR IN CABIN DURING TAXI. R & R THE NR 1 ENGINE IAW AMM 71-00-00-400-801-A & 71-00-00-400-802-A. PERFORMED 5 POINT CALIBRATION RUN ON TH - [SDR DXTA2014043005749](https://openairdocs.org/sdr/DXTA2014043005749), Apr 29, 2014: UNKNOWN. ODOR. FROM INITIAL APPLICATION OF TAKEOFF POWER TO 20,000 FT THERE WAS A STRONG ODOR LIKE HOT OIL OR JET FUEL IN THE CABIN. PERFORMED GROUND RUN TO DUPLICATE FAULT, N - [SDR DXTA2014042905746](https://openairdocs.org/sdr/DXTA2014042905746), Apr 25, 2014: UNKNOWN. ODOR. DURING INITIAL CLIMB, NOTICED A STRONG ODOR LIKE HOT DUCT THAT DID NOT DIMINISH DURING THE CLIMB OUT. SELECTING ECS 1, THEN ECS 2 DID NOT CHANGE THE ODOR. RETAR ## Service difficulty reports on N328QS not matched to an aircraft (14) They name N328QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2010102804278](https://openairdocs.org/sdr/DXTA2010102804278), Oct 27, 2010: POWER SUPPLY. INOPERATIVE. AFTER ROTATION, SEC FLT DISPLAY C/B POPPED, WITH ASSOCIATED STANDBY GYRO AMBER LIGHT ILLUMINATION. R & R STANDBY GYRO POWER SUPPLY IAW MM 34-21-14. OPS CHECKED - [SDR DXTA2010050604086](https://openairdocs.org/sdr/DXTA2010050604086), May 5, 2010: BRAKE ASSY. MALFUNCTIONED. WHEN EQUAL BRAKE PRESSURE IS APPLIED TO BOTH BRAKES, AIRCRAFT JERKS TO THE LT. LT BRAKE IS GRABBY AND SENSITIVE. RT BRAKE FEELS LESS EFFECTIVE. R & R RT MAIN BR - [SDR DXTA2010031004024](https://openairdocs.org/sdr/DXTA2010031004024), Mar 9, 2010: BRAKE SYS. SENSITIVITY. LT BRAKE PEDAL VERY SENSITIVE. RT BRAKE PEDAL ALMOST TO FLOOR TO ACHIEVE SAME BRAKING ACTION. THIS HAPPENS FROM BOTH SIDES. BLED THE BRAKES IAW MM 32-42-00. OPS - [SDR DXTA200702535](https://openairdocs.org/sdr/DXTA200702535), Oct 11, 2007: LANDING GEAR. MALFUNCTIONED. LT MAIN GEAR DID NOT INITALLY RETRACT AFTER TAKEOFF OTHER GEAR RETRACTED NORMALLY. REMOVED LEFT MAIN GEAR UPLOCK SWITCH DUE TO HIGH RESISTANCE. INSTALLED NEW SW - [SDR DXTA200702213](https://openairdocs.org/sdr/DXTA200702213), May 22, 2007: INDICATION SYS. OUT OF RIG. RUDDER TRIM OUT OF RIG. WILL TRIM FULL LT AND BACK TO CENTER, WILL NOT TRIM FULL RT. TROUBLESHOT SYSTEM, FOUND INDICATOR OUT OF RIG AND CONTACTING PEDESTAL, RIG - [SDR DXTA200702195](https://openairdocs.org/sdr/DXTA200702195), May 14, 2007: UNKNOWN. UNKNOWN. ON LANDING ROLLOUT, AT ABOUT 40 KTS, THE BRAKES STOPPED BRAKING. RELEASED THE BRAKES AND REAPPLIED FIRMLY AND THEY RE-ENGAGED. ON POST FLIGHT, FOUND BRAKE FLUID - [SDR DXTA200701955](https://openairdocs.org/sdr/DXTA200701955), Feb 18, 2007: ELBOW. LEAKING. AFTER TAKEOFF AND CLIMBING THRU 6000 FT RT ENGINE FIRE LIGHT CAME ON. REDUCED POWER ON RT ENGINE AND LIGHT WENT OUT. RAN THE POWER UP SLIGHTLY AND NOTICED OIL T - [SDR DXTA200701860](https://openairdocs.org/sdr/DXTA200701860), Jan 17, 2007: LINKAGE. OBSTRUCTED. ON TAKEOFF, LEFT ENGINE WOULD NOT GO ABOVE 90% N1 TAKEOFF ABORTED.TROUBLESHOOTING DETERMINED THE THROTTLE LINKAGE WAS STRIKING THE INBOARD IGNITER LEAD. REPOSIT - [SDR DXTA200601702](https://openairdocs.org/sdr/DXTA200601702), Oct 31, 2006: LINE. CONTAMINATED. BRAKES PULSATE ON ROLL OUT AT 60 KIAS AND BELOW UNTIL LOW SPEED TAXI. PERFORMED BRAKE BLEED AND ANTI-SKID FUNCTIONAL TEST IAW MM 32-42-00. REF. SQUAWK 1.5 FOR O - [SDR DXTA200601672](https://openairdocs.org/sdr/DXTA200601672), Oct 19, 2006: BRAKE. MALFUNCTIONED. ON 2 SEPARATE OCCASIONS, BRAKING QUIT AT ABOUT 10 KNOTS, AS THOUGH ANTI-SKID HAD QUIT MOMENTARILY. BLED BRAKES AND PERFORMED ANTISKID FUNCTIONAL CHECK. OPS CHEC - [SDR DXTA200601491](https://openairdocs.org/sdr/DXTA200601491), Jul 11, 2006: RELAY. FAILED. AT APPROXIMATELY 200 FEET ABOVE GROUND IN APPROACH TO LANDING, ANTI-SKID ILLUMINATED. AT 50 FT LOWER, POWER BRAKE LO PRESS ILLUMINATED. DURING TOUCHDOWN, HAD SU - [SDR DXTA200601384](https://openairdocs.org/sdr/DXTA200601384), May 8, 2006: LINE. FAILED. BRAKES (ON RIGHT SEAT) LOOSE EFFECTIVENESS, BUT MAINTAIN PRESSURE. BLEED BRAKES AS REQUIRED UNTIL FREE FLOW OF HYD FLUID WITH NO AIR PRESENT. SERVICED BRAKE RES - [SDR DXTA200501062](https://openairdocs.org/sdr/DXTA200501062), Nov 5, 2005: CASE. CRACKED. BRAKE PRESS LOW AND ANTI-SKID INOP LIGHTS ON BEFORE LANDING, BRAKES INOP. PEDALS TO FLOOR ON LANDING, USED BOTTLE TO STOP. BRAKE FLUID COMING OUT ALL OVER NOSE - [SDR DXTA200300075](https://openairdocs.org/sdr/DXTA200300075), Jul 29, 2003: MOTOR. BURNED. GROUND CREW OBSERVED SMOKE FROM BATTERY COMPARTMENT. GPU CONNECTED WITH AIR CONDITIONER RUNNING, STRONG SMOKE ODOR IN BATTERY COMPARTMENT. FOUND A/C MOTOR HAD I ## 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.