# N312QS: 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: 50500153
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: August 8, 2013
- Certificate issued: July 24, 2023
- Expires: July 31, 2030
- Mode S code: A34FAE
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=312QS
- Page: https://openairdocs.org/aircraft/N312QS

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 N312QS.

## FAA accident and incident reports

None matched to N312QS.

## Reports on N312QS not matched to an aircraft (1)

They name N312QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20080301832669I](https://openairdocs.org/incident/20080301832669I), Mar 1, 2008: Cessna 560CESSNA (N312QS), Cleveland, OH, No damage. (-23) During descent out of FL410 flt 312 (msp-pit) brought power back and the cabin went to a plus 6000FPM climb and the cabin greater than 10,000 ft…

## Service difficulty reports (15)

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 DXTA2025071404214](https://openairdocs.org/sdr/DXTA2025071404214), Jul 11, 2025: BATTERY PACK. FAULTED. DURING FLT, EMERGENCY LIGHTS REMAINED ILLUMINATED & DID NOT TURN OFF AS EXPECTED. VERIFIED SWITCH POSITION & CYCLED THE EMERGENCY LIGHT SWITCH. LIGHT REMAINED O
- [SDR DXTA2025032402758](https://openairdocs.org/sdr/DXTA2025032402758), Mar 20, 2025: WARNING MESSAGE. FALSE ACTIVATION. FUEL XFEED FAIL YELLOW CAS: FUEL XFEED FAIL YELLOW CAS DURING FLIGHT CORRECTIVE ACTION; PERFORMED OPERATIONAL CHECKS OF THE FUEL CROSSFEED AND COULD NOT DUPLICA
- [SDR DXTA2024031811203](https://openairdocs.org/sdr/DXTA2024031811203), Mar 14, 2024: BATTERY. DISCHARGED. DURING TAXI IN AND AFTER ENGINE SHUTDOWN, NOTICED EMERGENCY LIGHTING WAS ON. COMPLIED WITH TOP CHARGE OF EMERGENCY BATTERIES IAW AMM 33-52-01 AND NJA TC-505-33-
- [SDR DXTA2023112710154](https://openairdocs.org/sdr/DXTA2023112710154), Nov 26, 2023: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: DURING FLIGHT, WITH EMER LT SWITCH IN ARM POSITION, ALL EMER LIGHTS BEGAN FLASHING.///SIGN-OFF REMOVED AND REPLACE RH AFT EMERGENCY LIGHT BAT
- [SDR DXTA2023070590300](https://openairdocs.org/sdr/DXTA2023070590300), Jul 3, 2023: UNKNOWN. UNKNOWN. MAIN DOOR VISUAL INDICATOR: 3 OF THE 8 MAIN CABIN DOOR INDICATORS LOCATED AFT SECTION OF THE DOOR ARE OBSTRUCTED AND BARELY VISIBLE //SIGNOFF// INSPECTED ANO FO
- [SDR DXTA2023020379800](https://openairdocs.org/sdr/DXTA2023020379800), Feb 2, 2023: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: DURING CRUISE WITH EMER LIGHT SWITCH IN ARM POSITION, ALL CABIN EMER LIGHTS FLASHING. // SIGNOFF// GAINED ACCESS TO AND REMOVED AND REPLACED
- [SDR DXTA2022122777150](https://openairdocs.org/sdr/DXTA2022122777150), Dec 26, 2022: DISPLAY. DEFECTIVE. HIGHLIGHTED YELLOW GIA 1 FAIL. ASSOCIATED CAS MESSAGES: YELLOW TCAS FAIL, PTRIM NML FAIL, AP FAIL, YD FAIL, FLAP AND SPEED BRAKE YELLOW X'S, LG WOW SYS FAIL; WH
- [SDR DXTA2022090669790](https://openairdocs.org/sdr/DXTA2022090669790), Sep 6, 2022: HARNESS. DEFECTIVE. NLG LANDING GEAR EXTENSION: DURING LANDING APPROACH AT KDAL, AFTER SELECTING GEAR DOWN RECEIVED AN RED LANDING GEAR LEVER DISAGREEMENT CAS MESSAGE ACCOMPANIED B
- [SDR 2021FA0000000](https://openairdocs.org/sdr/2021FA0000000), Dec 27, 2020: 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 DXTA2020120804443](https://openairdocs.org/sdr/DXTA2020120804443), Dec 8, 2020: DISPLAY. DEFECTIVE. AT FLIGHT LEVEL 400 AP FAIL, YD FAIL, SWPS FAIL, BLEED 2 OFF, STBY BARO NOCOMP, GSD 1 FAIL, SWPS ICE SPEED, HSDB FAULT, LEFT MAIN GEAR WOULD NOT SHOW DOWN BUT S
- [SDR DXTA2020101304199](https://openairdocs.org/sdr/DXTA2020101304199), Oct 12, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY CABIN LIGHTS COME ON IN ARMED POSITION. BEGAN TROUBLE SHOOTING EMERGENCY CABIN LIGHTS, IAW FIM P-300 33-50-00 PAGE 3 BLOCK DIA 1 STEP 1 AND 2 FOUND EM
- [SDR JGVR20200115003](https://openairdocs.org/sdr/JGVR20200115003), Jan 15, 2020: BALANCE WEIGHT. UNDERSIZE. REPLACED LH ELEVATOR HORN MASS BALANCE WEIGHT P/N PE915109-L42 DUE TO BEING UNDER MINIMUM WEIGHT PER SB505-55-A004 REV 4
- [SDR DXTA2019112203105](https://openairdocs.org/sdr/DXTA2019112203105), Nov 21, 2019: STARTER GEN. DEFECTIVE. GEN 1 OFF BUS YELLOW CAS ILLUMINATED - YELLOW GEN 1 OFF BUS CAS ILLUMINATED IN FLIGHT ASSOCIATED WITH BAD ENGINE VIBRATION. AIRCRAFT WAS CLIMBING THROUGH 30,000
- [SDR DXTA2017010306355](https://openairdocs.org/sdr/DXTA2017010306355), Jan 3, 2017: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, WHEN THE LANDING GEAR LEVER MOVED TO THE DOWN POSITION, THE NOSE GEAR SHOWED A RED BOX AND LG LEVER DISAG CAS DISPLAYED. AFTER RECYCLING GEAR I
- [SDR DXTA2014073105840](https://openairdocs.org/sdr/DXTA2014073105840), Jul 30, 2014: BOLT. BROKEN. MAIN EXIT DOOR WILL NOT OPEN FROM INSIDE THE ACFT. RED HANDLE WILL ROTATE UP HALF WAY BEFORE IT BINDS. R & R BROKEN BOLT THAT CAME LOOSE & INSPECTED MAIN DOOR L

## Service difficulty reports on N312QS not matched to an aircraft (26)

They name N312QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200803002](https://openairdocs.org/sdr/DXTA200803002), Apr 16, 2008: PRESSURE SENSOR. INOPERATIVE. ON TAXI OUT TO RUNWAY, CAPTAIN PRESSED BRAKES AND BRAKES WENT TO STOPS WITH NO PRESSURE.TROUBLESHOT TO DEFECTIVE PRESSURE SWITCH. REMOVED AND INSTALLED NEW CUST
- [SDR DXTA20082906](https://openairdocs.org/sdr/DXTA20082906), Feb 29, 2008: RELAY. INOPERATIVE. CABIN CLIMBED AT MAX RATE, 10,000 FT, CABIN PRESSURE LIGHT CAME ON. THE PNUEMATIC RELAY WAS REMOVED AND REPLACED S/N OFF 15-2131. WORK PERFORMED IAW MM 21-31. S
- [SDR DXTA20082885](https://openairdocs.org/sdr/DXTA20082885), Feb 16, 2008: MASTER CYLINDER. BYPASSING. CO PILOTS LT BRAKE DEPRESSES ALL THE WAY TO THE FLOOR. PUMPING PEDAL TEMPORARILY RESTORES EFFECTIVNESS FOR A FEW SECONDS ONLY. REMOVED COMPLETE LT WHEEL BRAKE M
- [SDR DXTA20082871](https://openairdocs.org/sdr/DXTA20082871), Feb 13, 2008: BRAKE ASSY. MALFUNCTIONED. CO-PILOT'S LT BRAKE DEPRESSES TO FLOOR WITH NO RESULT. COMPLETED BRAKE BLEED PROCEDURE. BRAKES OPS CHK GOOD. AMM 32-42-00.
- [SDR DXTA200702328](https://openairdocs.org/sdr/DXTA200702328), Jul 10, 2007: NONE. NONE. DURING THE TAKEOFF ROLL AT APPROXIMATELY 65 KTS, WE HIT A FLOCK OF BIRDS AND ABORTED THE TAKEOFF. (M2B) COMPLIED WITH FOD INSPECTIONS IAW MM. CHAPTER 05-50 MM. 
- [SDR DXTA200601828](https://openairdocs.org/sdr/DXTA200601828), Dec 30, 2006: LAMP. SHORTED. SMOKE COMING FROM TAIL NAV LIGHT AREA. SMOKE SMELLED ELECTRICAL. REMOVED POWER FROM AIRCRAFT SMOKE STOPPED. PLATE UNDER THE LIGHT WAS HOT TO THE TOUCH. REPLACED
- [SDR DXTA20061690](https://openairdocs.org/sdr/DXTA20061690), Oct 27, 2006: ENGINE. LEAKING. SMOKE IN THE COCKPIT AFTER TAKEOFF. REMOVED S/N PCE-JC0296, INSTALLED REPAIRED UNIT IAW MM 71-01-02. OPS AND LEAK CHECK GOOD.
- [SDR DXTA200601605](https://openairdocs.org/sdr/DXTA200601605), Sep 17, 2006: ENGINE. SHUTDOWN. RIGHT ENGINE SHUT DOWN WHEN DOING THE SPEEDBRAKE CHECK. - PERFORMED ENGINE GROUND RUN, EXTENDED SPEED BRAKES SEVERAL TIMES WITH NO DEFECTS TO ENGINES. PERFORMED
- [SDR DXTA200601547](https://openairdocs.org/sdr/DXTA200601547), Aug 9, 2006: ENGINE. UNKNOWN. RT ENGINE STARTED FIRST THEN LEFT. RT ENGINE QUIT. RESTARTED RT ENGINE. FUEL FLOW INDICATOR READS ZERO. ADVANCE THRUST LEVER INDICATOR INCREASES. LEVER TO IDLE 
- [SDR DXTA200601314](https://openairdocs.org/sdr/DXTA200601314), Mar 23, 2006: SHAFT. SHEARED. BRAKE FAILURE ON TAXI OUT. BRAKE ACCUMULATOR IS OUT OF GREEN ARC WITH BATTERY ON. NO VISUAL LEAKS, FOUND ANTI-SKID POWER PACK MOTOR SPINS BUT NO PRESSURE BUILD 
- [SDR DXTA200601272](https://openairdocs.org/sdr/DXTA200601272), Feb 28, 2006: BRAKE ASSY. MALFUNCTIONED. ON LANDING ROLL FIRST OFFICER'S RIGHT BRAKE PEDAL WENT ALMOST TO THE FLOOR. CAPTAIN'S SIDE WORKS FINE. AFTER BRAKE PEDAL IS PUMPED UP IT WILL HOLD PRESSURE FOR 
- [SDR DXTA200601270](https://openairdocs.org/sdr/DXTA200601270), Feb 27, 2006: LINE. LEAKING. AFTER SELECTING GEAR DOWN POWER BRAKE LOW PRESS AND ANTI SKID INOP ANNUNCIATOR LIGHTS WOULD NOT EXTINGUISH. USED EMERGENCY BRAKING, BRAKE RESERVOIR IS EMPTY. FO
- [SDR DXTA200601747](https://openairdocs.org/sdr/DXTA200601747), Jan 21, 2006: ENGINE. UNKNOWN. DURING THE STOW CHECK OF THE SPEED BRAKES, THE ENGINE SHUTDOWN , UPON RETURNING THE THROTTLES TO IDLE. PERFORMED GROUND RUN OF RT AND LT ENGINES AT IDLE AND TAK
- [SDR DXTA200501134](https://openairdocs.org/sdr/DXTA200501134), Dec 8, 2005: BRAKE ASSY. MALFUNCTIONED. CO-PILOTS BRAKES DURING LANDING ARE SPONGY, GO ALMOST TO FLOOR AND WHEN BRAKES GRAB, THE AIRPLANE TURNS TO THE RIGHT. PERFORMED BRAKE BLEEDING PROCEDURES IAW CE
- [SDR DXTA200501133](https://openairdocs.org/sdr/DXTA200501133), Dec 7, 2005: BRAKE ASSY. MALFUNCTIONED. CO-PILOTS BRAKES GO TO THE FLOOR AND WHEN BRAKES DID GRAB, THE AIRPLANE TURNED 30 DEGREES HARD TO THE RIGHT. ON ARRIVAL OF ACFT INSPECTED BRAKES FOUND TO APPEAR
- [SDR DXTA200501121](https://openairdocs.org/sdr/DXTA200501121), Nov 28, 2005: BRAKE. MALFUNCTIONED. ON LANDING, LEFT BRAKE PEDAL ON CO-PILOT SIDE WENT TO FLOOR. RIGHT PEDAL WORKED NORMALLY. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200501112](https://openairdocs.org/sdr/DXTA200501112), Nov 25, 2005: LINE. LEAKING. CO-PILOT'S LEFT BRAKE FAILURE UPON LANDING. BRAKE WENT TO FLOOR, REQUIRED PUMPING TO RESTORE PRESSURE. VERIFFIED LT CO-PILOT PEDAL SOFT, REMOVED FWD BAGGAGE PAN
- [SDR DXTA200501091](https://openairdocs.org/sdr/DXTA200501091), Nov 18, 2005: BRAKE. STICKING. UPON LANDING AND TAXIING BRAKES WERE HARD, MORE THAN NORMAL BRAKING PRESSURE WAS REQUIRED. UNEVEN BRAKING AND JERKING DURING TAXI RESULTED. INSPECTED BRAKE SYST
- [SDR DXTA200501059](https://openairdocs.org/sdr/DXTA200501059), Nov 4, 2005: MASTER CYLINDER. FAILED. BRAKES ON CO-PILOT SIDE ARE SPONGY, AND WHEN TURNING OFF RUNWAY LEFT PEDAL WENT TO THE FLOOR. REPEAT WRITE-UP. REMOVED PILOT'S AND COPILOT'S LEFT AND RIGHT MAST
- [SDR DXTA200500816](https://openairdocs.org/sdr/DXTA200500816), Jul 3, 2005: BRAKE. MALFUNCTIONED. RIGHT SIDE FOOT BRAKES HAVE TO BE PUSHED TO THE FLOOR TO EFFECT BRAKING. FEELS LIKE AIR IN BRAKE LINE. BLED BRAKES IAW CESSNA 560 MM 32-42-00, OPS CHECK GOOD.
- [SDR DXTA200500744](https://openairdocs.org/sdr/DXTA200500744), May 29, 2005: BRAKE. MALFUNCTIONED. BRAKE PEDALS ON THE RIGHT SIDE FEEL MUSHY GO ALL THE WAY TO THE STOPS AND GRAB. LEFT SIDE IS NORMAL. BLED BRAKES PER CE560 M/M 32-42-00. OPS CHECKED GOOD.
- [SDR DXTA200400409](https://openairdocs.org/sdr/DXTA200400409), Sep 29, 2004: COMPUTER. FAULTY. BOTH CAPTAIN'S BRAKES INTERMITTENTLY REQUIRE UNEVEN APPLICATION CAUSING PLANE TO SLOW/STOP UNEVENLY OR GRAB. APPEARS LEFT BRAKE INTERMITTENTLY TRAVELS FURTHER B
- [SDR DXTA200400309](https://openairdocs.org/sdr/DXTA200400309), May 11, 2004: SENSOR. MALFUNCTIONED. BATTERY TEMP INDICATOR IN FLIGHT INDICATED 180ºF VARIED SLOWLY TO 160ºF, EMEGENCY DECLARED. INDICATION DURING 2 PREVIOUS LEGS WAS 120ºF PREFLIGHT COCKPIT ROTARY
- [SDR DXTA200300115](https://openairdocs.org/sdr/DXTA200300115), Sep 10, 2003: AUTOPILOT SYS. MALFUNCTIONED. AIRCRAFT EXPERIENCED UNCOMMANDED RIGHT RUDDER INPUT DURING CRUISE WITH AUTOPILOT ON, ALSO DEVELOPED NOTICEABLE PITCH ROLL WITH AUTO PILOT ON. PERFORMED NJA OPER
- [SDR 96ZZZX2094](https://openairdocs.org/sdr/96ZZZX2094), Apr 9, 1996: ACTUATOR. MALFUNCTIONED. ON TAKEOFF, THE RIGHT ENGINE RPM ROLLED BACK 10 PERCENT AND THE I.T.T. INCREASED TO 700 DEGREES. AIRCRAFT RETURNED AND ENGINE WAS INSPECTED. NO PROBLEM WAS FOUN
- [SDR 96ZZZX2093](https://openairdocs.org/sdr/96ZZZX2093), Apr 9, 1996: CONTROL. MALFUNCTIONED. ON TAKEOFF, THE RIGHT ENGINE RPM ROLLED BACK 10 PERCENT AND THE I.T.T. INCREASED TO 700 DEGREES. AIRCRAFT RETURNED AND ENGINE WAS INSPECTED. NO PROBLEM WAS FOUN

## 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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