# N363QS: 2015 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: 50500256
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: March 13, 2015
- Certificate issued: January 9, 2026
- Expires: January 31, 2033
- Mode S code: A418E0
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=363QS
- Page: https://openairdocs.org/aircraft/N363QS

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 N363QS.

## FAA accident and incident reports

None matched to N363QS.

## 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 DXTA2026012306625](https://openairdocs.org/sdr/DXTA2026012306625), Jan 21, 2026: BATTERY. FAULTED. UPON TAXI DEPARTING MMU FBO WE NOTICED THAT THE EMERGENCY LIGHTS WERE STILL ON AS THE EMER LT SWITCH WAS PLACED IN ARM. WHEN REACHING THE RUN-UP PAD AT MMU THE 
- [SDR DXTA2023120410209](https://openairdocs.org/sdr/DXTA2023120410209), Dec 1, 2023: UNKNOWN. UNKNOWN. DOOR PAX OPEN ANNUNCIATOR ILLUM DURING CLIMB, THRU 21,000 FT. AFTER LEVEL OFF & BEGINNING DESCENT, ANNUNCIATOR EXTINGUISHED. QRH PROCEDURE FOLLOWED, CABIN WAS D
- [SDR DXTA2023081192750](https://openairdocs.org/sdr/DXTA2023081192750), Aug 11, 2023: LIGHT. DEFECTIVE. FLOOR EMERGENCY LIGHT BETWEEN SEATS 1 & 3 LENS BROKEN, FOUND ON FLOOR, LAMP NOT VISIBLE. LENS IN CABIN CUP HOLDER AT SEAT 3. FOUND LIGHT PUSHED INSIDE FISHED LI
- [SDR EBVR202208180001](https://openairdocs.org/sdr/EBVR202208180001), Aug 18, 2022: MOUNT. CRACKED. A CRACK WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE UNDER THE FWD SUPPORT ROD MOUNT, THE CRACK WAS REPAIRED IAW AQRD ERO-106779 REV IR DATED: AUG 18, 2022. FAA A
- [SDR DXTA2022070565290](https://openairdocs.org/sdr/DXTA2022070565290), Jul 4, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS ARE ON WITH THE SWITCH IN THE ARMED POSITION // SIGNOFF// CONFIRMED WRITE UP,T/S PER FIM AND HAD BATTERY'S FAIL, 2 BATTERY'S
- [SDR DXTA2022030757970](https://openairdocs.org/sdr/DXTA2022030757970), Mar 6, 2022: DRAIN VALVE. DAMAGED. FOUL ODOR EMANATES FROM COCKPIT VENTS WITH AIR CONDITIONING ON. SMELLS LIKE RODENT URINE. NO NOTICEABLE ODOR IN CABIN. CABIN AIR PURGED WITH OZONE/PURIFIER. INS
- [SDR DXTA2022020256030](https://openairdocs.org/sdr/DXTA2022020256030), Feb 1, 2022: CONTROL UNIT. DEFECTIVE. BRK FAIL YELLOW CAS: REPEAT WRITE UP. YELLOW BRK FAIL CAS MESSAGE DISPLAYED AFTER TAKEOFF. DIVERTED TO KLNK. CW QRH. NO NORMAL BRAKES. STOPPED WITH EMERGENCY BR
- [SDR DXTA2022012155520](https://openairdocs.org/sdr/DXTA2022012155520), Jan 21, 2022: MODULE. DEFECTIVE. BRK FAIL YELLOW CAS: BRAKE CAS FAIL MESSAGE CAME ON AT ABOUT 6000 FEET. WE CLIMBED TO 16000 FEET. RAN QRH FOR MESSAGE THEN LANDED. USED LITTLE PARKING BRAKE TO 
- [SDR 2022FA0000009](https://openairdocs.org/sdr/2022FA0000009), Jan 9, 2022: LIGHT. INOPERATIVE. DURING SCHEDULED MAINTENANCE, THE OVER-WING EMERGENCY EXIT LIGHT HAD SEVERAL LED SEGMENTS INOPERATIVE. LIGHT ASSEMBLY WAS REPLACED WITH NEW AND OPERATIONAL TEST
- [SDR DXTA2021121653650](https://openairdocs.org/sdr/DXTA2021121653650), Dec 15, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMER LIGHT CAME ON DURING FLIGHT WITHOUT BEING SELECTED. // SIGNOFF// REMOVED AND REPLACED #2 EMERGENCY BATTERY. IAW EMB-605 AMM 33-52-01 OPS
- [SDR DXTA2021120653100](https://openairdocs.org/sdr/DXTA2021120653100), Dec 5, 2021: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: ALL EMERGENCY EXIT LIGHTS FLICHERING DURING FLIGHT. LIGHTS FLICKER WITH SWITCH IN ON AND ARMED POSITIONS. // SIGNOFF // TROUBLESHOT SYSTEM I
- [SDR DXTA2021042141070](https://openairdocs.org/sdr/DXTA2021042141070), Apr 21, 2021: CABIN PRESSURE. MALFUNCTIONED. PRESN AUTO FAIL YELLOW CAS: AT FL400 CRUISE THE FOLLOWING CAS MESSAGES ILLUMINATED: PRESN AUTO FAIL, SWPS FAULT, AP FAIL, AMS CTRL FAIL, YD FAIL, STBY BARO FAIL
- [SDR DXTA2019041822155](https://openairdocs.org/sdr/DXTA2019041822155), Apr 12, 2019: PRIORITY VALVE. MALFUNCTIONED. NLG LANDING GEAR EXTENSION DELAY - DURING GEAR EXTENSION, A THUD WAS HEARD AND FELT FROM THE RIGHR MAIN GEAR FOLLOWED BY ABOUT A 10 SECOND DELAY OF THE NOSE GEA
- [SDR 2018FA0000408](https://openairdocs.org/sdr/2018FA0000408), Oct 8, 2018: SUPPORT TUBE. SWOLLEN. DURING SCHEDULED INSPECTION IT WAS FOUND THAT THE LOWER RUDDER LT SUPPORT TUBE WAS SWELLING. WHILE NO CRACKS WERE FOUND ON THIS ONE IT'S BEEN KNOWN TO HAVE CRAC

## Service difficulty reports on N363QS not matched to an aircraft (28)

They name N363QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2011060704607](https://openairdocs.org/sdr/DXTA2011060704607), Jun 6, 2011: MASTER CYLINDER. LEAKING. CO-PILOT SIDE RT BRAKE IS FREE MOVING HALF WAY THROUGH THE BRAKES. WHEN APPLIED IT CAUSES UNEVEN BRAKING. R & R LT & RT CO-PILOTS BRAKE MASTER CYLINDER. PERFORM
- [SDR DXTA2011060604605](https://openairdocs.org/sdr/DXTA2011060604605), Jun 4, 2011: BRAKE SYS. WEAK. COPILOTS LT AND RT BRAKE PEDALS ARE SPONGY. RT SIDE PEDAL GOES ALMOST TO THE FLOOR ON BRAKE APPLICATION. PERFORMED BLEED PROCEDURE ON RT BRAKE SYS. PERFORMED TA
- [SDR DXTA2011052004585](https://openairdocs.org/sdr/DXTA2011052004585), May 20, 2011: BRAKE. UNKNOWN. AIRPLANE PULLS HARD TO THE LEFT WHEN BRAKING FROM PILOTS AND COPILOTS SIDE. COMPLIED WITH BRAKE SYS BLEED IAW MM 32-42-00. LEAK AND TAXI CHECKED GOOD.
- [SDR CWQR201102](https://openairdocs.org/sdr/CWQR201102), Jan 20, 2011: ANGLE. CRACKED. DURING A SCHEDULED PHASE INSP, FOUND MINOR CORRISION ON THE RT ENGINE BOX BEAM. THE ENGINE WAS REMOVED AND WHEN THE CLOSE OUT PANEL WAS REMOVED FOR CORRISION IN
- [SDR CWQR201101](https://openairdocs.org/sdr/CWQR201101), Jan 20, 2011: CHANNEL. DAMAGED. DURING A SCHEDULED PHASE INS, THE TECH FOUND MINOR CORROISION ON THE RT ENGINE BOX BEAM. THE ENGINE WAS REMOVED AND WHEN THE CLOSE OUT PANEL WAS REMOVED FOR COR
- [SDR 2008FA0000832](https://openairdocs.org/sdr/2008FA0000832), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000831](https://openairdocs.org/sdr/2008FA0000831), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000830](https://openairdocs.org/sdr/2008FA0000830), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000829](https://openairdocs.org/sdr/2008FA0000829), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000828](https://openairdocs.org/sdr/2008FA0000828), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000827](https://openairdocs.org/sdr/2008FA0000827), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000826](https://openairdocs.org/sdr/2008FA0000826), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000825](https://openairdocs.org/sdr/2008FA0000825), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000824](https://openairdocs.org/sdr/2008FA0000824), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000823](https://openairdocs.org/sdr/2008FA0000823), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000822](https://openairdocs.org/sdr/2008FA0000822), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000821](https://openairdocs.org/sdr/2008FA0000821), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000820](https://openairdocs.org/sdr/2008FA0000820), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000819](https://openairdocs.org/sdr/2008FA0000819), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000818](https://openairdocs.org/sdr/2008FA0000818), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000817](https://openairdocs.org/sdr/2008FA0000817), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000816](https://openairdocs.org/sdr/2008FA0000816), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000815](https://openairdocs.org/sdr/2008FA0000815), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000814](https://openairdocs.org/sdr/2008FA0000814), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000813](https://openairdocs.org/sdr/2008FA0000813), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR 2008FA0000812](https://openairdocs.org/sdr/2008FA0000812), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB
- [SDR DXTA200702079](https://openairdocs.org/sdr/DXTA200702079), Apr 4, 2007: BRAKE ASSY. FAULTED. F/O BRAKES LITTLE TO NO EFFECT DURING FIRST 80 PERCENT OF TRAVEL WORKED DURING LAST PART BUT SOFT. NEEDED TO BE PUMPED AT LEAST TWICE TO GET RESISTANCE BUT FADE
- [SDR CWQ2003F00001](https://openairdocs.org/sdr/CWQ2003F00001), Feb 12, 2003: DUCT. CRACKED. DURING ROUTINE INSPECTION, LOOKED INTO DORSAL NACA SCOOPS AND SAW THE LOWER AIR VANE WITH A 3 IN CRACK STARTING FROM CENTER OF (V) CUT TO OUTBOARD EDGE. GAINED 

## 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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