# N336QS: 2014 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: 50500201
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: March 26, 2014
- Certificate issued: July 17, 2024
- Expires: July 31, 2031
- Mode S code: A3AD88
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=336QS
- Page: https://openairdocs.org/aircraft/N336QS

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 N336QS.

## FAA accident and incident reports

None matched to N336QS.

## Service difficulty reports (8)

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 DXTA2026081709286](https://openairdocs.org/sdr/DXTA2026081709286), Aug 14, 2026: DOWNLOCK SENSOR. DAMAGED. GEAR SELECTED UP AFTER T/O. LG LEVER DISAG. NLG INDICATED RED DASHED BOX. SELECTED GEAR DOWN PER QRH AND HEARD A SHORT GRINDING NOISE IN NLG. LANDED NORMALLY. R
- [SDR DXTA2023120410227](https://openairdocs.org/sdr/DXTA2023120410227), Dec 3, 2023: BATTERY. INOPERATIVE. DURING FLIGHT, EMERGENCY LIGHTS OVER THE DOORS AND THREE CENTER AISLE OVERHEAD LIGHTS BEGAN FLICKERING WITH THE SWITCH IN THE ARM POSITION. REMOVED FORWARD EMER
- [SDR DXTA2023040583730](https://openairdocs.org/sdr/DXTA2023040583730), Apr 5, 2023: UNKNOWN. UNKNOWN. MLG BRAKE PRESSURE: HAVING TO APPLY ASYMMETRICAL BRAKING ON LANDING. LEFT SIDE LOWER THAN RIGHT DURING BRAKING. MX TEAM COMPLETED THE SERVICING OF HYDRAULIC RES
- [SDR 2020FA0000426](https://openairdocs.org/sdr/2020FA0000426), Sep 25, 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 JGVR20200129001](https://openairdocs.org/sdr/JGVR20200129001), Jan 29, 2020: BALANCE WEIGHT. CORRODED. DURING COMPLIANCE OF SERVICE BULLETIN 505-55-A004 REV 5 MASS BALANCE AND ATTACHMENT PARTS - (INSPECTION, CORROSION FOUND ON ALL BALANCE WEIGHTS. WEIGHTS WERE CL
- [SDR DXTA2019121983222](https://openairdocs.org/sdr/DXTA2019121983222), Dec 18, 2019: WARNING MESSAGE. FALSE INDICATION. FOLLOWING CAS MSGS ILLUMINATED IN FLIGHT: SWPS FAULT AMS CTRL FAIL AP FAIL YD FAIL GSD2 FAIL SWPS ICE SPEED HSDB FAULT//SIGNOFF// PERFORMED GSD 2 OPERATIONAL CH
- [SDR DXTA2018012500512](https://openairdocs.org/sdr/DXTA2018012500512), Jan 25, 2018: UNKNOWN. ODOR. COCKPIT ODOR DURING CLIMB OUT. PERFORMED VISUAL INSPECTION FOR ANY WET INSULATION BLANKETS AND SURROUNDING AREA AROUND LAV, NO DEFECTS NOTED. RAN ENGINES FOR 1 
- [SDR DXTA2015061606032](https://openairdocs.org/sdr/DXTA2015061606032), Jun 14, 2015: BRAKE. FIRE. AFTER LANDING, DURING SPEED & NORMAL BRAKING, WHEN SETTING PARKING BRAKE AT TERMINAL, GND PERSONNEL REPORTED RT FRONT BRAKE ON FIRE. BEFORE FIRE BOTTLE ARRIVED 

## Service difficulty reports on N336QS not matched to an aircraft (21)

They name N336QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2010020103963](https://openairdocs.org/sdr/DXTA2010020103963), Jan 29, 2010: PEDAL. BINDING. ON LANDING WHILE APPLYING BRAKES, PEDALS SEEMED SOLID INITIALLY, THEN THERE WAS ADDITIONAL TRAVEL TO MAINTAIN THE SAME BRAKING. WHEN THE BRAKE PEDALS WERE RELEA
- [SDR DXTA2009120103876](https://openairdocs.org/sdr/DXTA2009120103876), Nov 30, 2009: CONTROL VALVE. OVERHEATED. WINDSHIELD O'HEAT ANNUNCIATOR CAME ON IN FLIGHT WHILE WINDSHIELD HEAT WAS ON, -20ºC RAT. ANNUNCIATOR DID NOT EXTINGUISH AUTOMATICALLY AND WAS ACCOMPANIED BY BUR
- [SDR DXTA2009092803799](https://openairdocs.org/sdr/DXTA2009092803799), Sep 24, 2009: BRAKE ASSY. MALFUNCTIONED. BRAKES SPONGY AT HIGH SPEED ROLL OUT AND PULL LEFT AS YOU INCREASE PRESSURE. WHEN AC REACHES 30 KTS & SLOWER BRAKES GRAB AS IF ANTI-SKID IS WORKING. BLED BRAKES
- [SDR DXTA2009051403649](https://openairdocs.org/sdr/DXTA2009051403649), May 12, 2009: THROTTLE. OUT OF RIG. DURING SPEED BRAKE TEST WITH ENGINES RUNNING, RT THROTTLE WAS MOVED FWD AND THEN BACK TO IDLE. AT THE IDLE STOP, RT ENGINE SHUTDOWN. INSPECTED NR 2 ENGINE S/N P
- [SDR DXTA200810043294](https://openairdocs.org/sdr/DXTA200810043294), Oct 4, 2008: RELAY. INOPERATIVE. BOTH BRAKES ON BOTH SIDES FAILED ON LANDING. BRAKE RESERVOIR IS FULL. ACCUMULATOR PRESSURE GAUGE READS RESIDUAL PRESSURE ONLY. CIRCUT BREAKER WAS CHECKED IN. NO
- [SDR DXTA200803294](https://openairdocs.org/sdr/DXTA200803294), Oct 4, 2008: BRAKE SYS. FAILED. BOTH BRAKES ON BOTH SIDES FAILED ON LANDING. (K)
- [SDR DXTA200807213189](https://openairdocs.org/sdr/DXTA200807213189), Jul 19, 2008: CONTROL HANDLE. WORN. AFTER TAKEOFF, THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO RETRACT. THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO EXTEND FLAPS EITHER. FLAPS ARE STUCK AT 7 DEGREES.
- [SDR DXTA200803189](https://openairdocs.org/sdr/DXTA200803189), Jul 19, 2008: FLAP SYSTEM. MALFUNCTIONED. AFTER TAKEOFF, THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO RETRACT. THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO EXTEND FLAPS EITHER. FLAPS ARE STUCK AT 7 DEGREES.
- [SDR DXTA200702583](https://openairdocs.org/sdr/DXTA200702583), Oct 30, 2007: FITTING. LOOSE. 1ST OFFICERS BRAKES ARE MUSHY AND REQUIRE A COUPLE OF PUMPS AFTER INTITAL PRESSURE TO FIRM UP. INSPECTED BRAKE SYSTEM, FOUND PILOTS LT MASTER CYLINDER FITTINGS 
- [SDR DXTA200702546](https://openairdocs.org/sdr/DXTA200702546), Oct 15, 2007: ANTI-SKID SYS. STICKING. BRAKE RELEASE, GRAB WITH THE ANTISKID ON. BLED BRAKES IAW CE560 MM 32-42-00.
- [SDR DXTA200702400](https://openairdocs.org/sdr/DXTA200702400), Aug 13, 2007: WIRE HARNESS. WORN. AFTER APPLYING BRAKE PRESSURE THE BRAKES GRAB AND THEN QUICKLY RELEASE. THET THEN GRAB AGAIN IN A JERKY FASHION. BLED A/C BRAKES. REMOVED AND REPLACED THE LEFT 
- [SDR DXTA200702348](https://openairdocs.org/sdr/DXTA200702348), Jul 18, 2007: IGNITION LEAD. MISINSTALLED. NR1 ENGINE (LT) WOULD NOT MAKE TAKEOFF POWER. AIRPORT, 318 FT ELEV,TEMP 18C, TARGET T/O PWR 97.8 PERCENT. COULD ONLY GET 87.2 PERCENT AT 580 ITT. POWER LEVEL FU
- [SDR DXTA200702249](https://openairdocs.org/sdr/DXTA200702249), Jun 7, 2007: BRAKE ASSY. WEAK. BOTH PILOTS + COPILOTS LEFT BRAKE SOFT. BOTH PILOTS & COPILOTS RIGHT BRAKE EXTREMLY SOFT PEDAL HAS TO BE PUSHED ALL THE WAY FORWARD TO GET ANY BRAKING ACTION ON
- [SDR DXTA200701917](https://openairdocs.org/sdr/DXTA200701917), Feb 6, 2007: ENGINE. MALFUNCTIONED. LT ENGINE SHUTDOWN DURING SPEED BRAKE RETRACTION TEST. N2 WAS 11 PERCENT. N1 WAS 7 PERCENT AND ITT STARTED TO RISE TO 550.
- [SDR DXTA200601748](https://openairdocs.org/sdr/DXTA200601748), Nov 21, 2006: CONTROL CABLE. BINDING. RT ENGINE SHUTDOWN WHEN THROTTLE WAS BROUGHT TO IDLE DETENT ON THE GROUND WITH IDLE SWITCH IN HIGH IDLE. THROTTLES FEEL NOTCHY NEAR THE LOW STOP. REMOVED RT ENG
- [SDR DXTA200500765](https://openairdocs.org/sdr/DXTA200500765), Jun 11, 2005: INDICATOR. FAILED. DURING TAKEOFF ROLL, STANDBY AIRSPEED INDICATOR STAYED AT 0 KTS. BOTH PFD AIRSPEED INDICATIONS WERE ACCELERATING THROUGH 60 KTS. ITEM IS UNDER INVESTIGATION.
- [SDR CWQ2004F00007](https://openairdocs.org/sdr/CWQ2004F00007), Jun 30, 2004: WIRE. MISINSTALLED. WHEN COMPLYING WITH SB ON AC, THE RT WING FUEL BOOST PUMP WIRING WAS FOUND TO BE UNACCEPTABLE IAW SB OUTER JACKET, WIRE BRAID AND WIRE INSULATION CHAFED THRU, A
- [SDR DXTA200300063](https://openairdocs.org/sdr/DXTA200300063), Jul 7, 2003: WIRE. BROKEN. BRAKES FAILED UPON TOUCHDOWN DEPLOYED EMERGENCY BRAKING SYSTEM. BLED BRAKE SYSTEM, TROUBLESHOT TO BROKEN WIRES ON THE ANTI-SKID TRANSDUCER. REPAIRED WIRING, PER
- [SDR 97ZZZX32](https://openairdocs.org/sdr/97ZZZX32), Nov 14, 1996: INVERTER. MALFUNCTION. ALTITUDE AND HEADING FAIL ON PILOT AND COPILOT PFD DISPLAYS. FOUND NR 1 INVERTER MALFUNCTIONING.
- [SDR 97ZZZX34](https://openairdocs.org/sdr/97ZZZX34), Nov 7, 1996: GYRO. MALFUNCTION. AUTOPILOT INOPERATIVE. RATE GYRO CIRCUIT BREAKER POPPED. FOUND RATE GYRO MALFUNCTIONING.
- [SDR 96ZZZX3390](https://openairdocs.org/sdr/96ZZZX3390), Jun 7, 1996: TUBE. MISADJUSTED. CABIN ENTRY DOOR FAILED TO OPEN UPON ARRIVAL. CREW HAD TO EGRESS THROUGH ESCAPE HATCH. FOUND LOWER FORWARD 3 PINS FAILING TO RETRACT FULLY. SUBMITTER STATED CAU

## 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

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