# N335QS: 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: 50500200
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: February 26, 2014
- Certificate issued: January 9, 2026
- Expires: January 31, 2033
- Mode S code: A3A9D1
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=335QS
- Page: https://openairdocs.org/aircraft/N335QS

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 N335QS.

## FAA accident and incident reports

None matched to N335QS.

## Service difficulty reports (19)

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 JGVR20260612201](https://openairdocs.org/sdr/JGVR20260612201), Jun 12, 2026: FLAP TRACK. WORN. FOUND WEAR AND GOUGES ON LH AND RH WING FLAP INBOARD AND OUTBOARD TRACKS, REMOVED FASTENERS AS REQUIRED, BLENDED AREAS SMOOTH, PERFORMED NDT AND REPORTED FOR RE
- [SDR DXTA2026010206381](https://openairdocs.org/sdr/DXTA2026010206381), Dec 30, 2025: BATTERY PACK. FAULTED. ALL EMER LIGHTS IN CABIN FLICKERING. REPEAT WRITE UP. REMOVED AND REPLACED NR 1 & 2 EMERGENCY BATTERY PACK AND PERFORMED OPS CHKD IAW AMM 33-52-01. OPS CHKD GOO
- [SDR DXTA2025122906297](https://openairdocs.org/sdr/DXTA2025122906297), Dec 25, 2025: LIGHT. MALFUNCTIONED. OBSERVED ALL EMER LIGHTS INTERMITTENTLY FLICKERING. OBSERVED ALL EMER LIGHTS REMAINING ON FOR 20+ MINUTES WHEN SWITCH IN ARM POSITION. POWERED THE PLANE AND CHA
- [SDR DXTA2025060903807](https://openairdocs.org/sdr/DXTA2025060903807), Jun 7, 2025: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: EMERGENCY LIGHTS STAYING ON IN THE ARM POSITION. EVEN WITH ENGINES RUNNING. CORRECTIVE ACTION: REPLACED BOTH THE FWD AND AFT EMERGENCY BATTER
- [SDR DXTA2025052303585](https://openairdocs.org/sdr/DXTA2025052303585), May 21, 2025: DRAIN. BROKEN. HAD A NOTICABLE VIBRATION IN FLIGHT IN COCKPIT. WAS MORE NOTICABLE ON LEFT SIDE OF COCKPIT. SPEED OF AIRCRAFT SEEMED TO CHANGE THE SOUND AS WE GOT FASTER. SOUND
- [SDR DXTA2024092200592](https://openairdocs.org/sdr/DXTA2024092200592), Sep 18, 2024: BATTERY. FAILED. ABOUT 45 MIN INTO FLIGHT CABIN EMERGENCY LIGHTS STARTED FLASHING, FLASHING BECAME FASTER AS FLIGHT WENT ON. ON GROUND AFTER SHUTDOWN AND TURNING OFF AND BACK ON
- [SDR DXTA2023100297020](https://openairdocs.org/sdr/DXTA2023100297020), Oct 2, 2023: MOTOR. DEFECTIVE. VENTRAL RUD FAIL WHITE CAS: DURING ENROUTE CLIMB AT ABOUT FL350 WE GOT AN INTERMITTENT VENTRAL RUD FAIL WHITE CAS WHICH THEN STAYED ON PERMANENTLY UNTIL LANDING
- [SDR DXTA2023100296880](https://openairdocs.org/sdr/DXTA2023100296880), Sep 29, 2023: UNKNOWN. UNKNOWN. FLAP FAIL YELLOW CAS: DURING FLIGHT RECEIVED SWPS FAULT FLAP FAIL PTRIM BKP FAIL SPOILER FAULT VENTRAL RUDER FAIL PERFORMED APPROPRIATE CHECK LIST AND LANDED IN
- [SDR DXTA2023051786420](https://openairdocs.org/sdr/DXTA2023051786420), May 16, 2023: BATTERY PACK. DEFECTIVE. CABIN EMERG LIGHT: C CAME ON STEADY AND THEN STARTED FLASHING. REMOVED FAULTY #1 EMERGENCY BATTERY AND REPLACE WITH "MODIFIED" EMERGENCY BATTERY. PERFORMED SATI
- [SDR DXTA2023022881190](https://openairdocs.org/sdr/DXTA2023022881190), Feb 24, 2023: BATTERY. DISCHARGED. EMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ON WITH THE EMER LT SWITCH IN THE ARM POSITION. *** CORRECTIVE ACTION *** TROUBLESHOT AND REMOVED DEFECTIVE #2 EMERGENC
- [SDR DXTA2023022481190](https://openairdocs.org/sdr/DXTA2023022481190), Feb 24, 2023: NONE. NONE. EMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ON WITH THE EMER LT SWITCH IN THE ARM POSITION.
- [SDR DXTA2022091970650](https://openairdocs.org/sdr/DXTA2022091970650), Sep 17, 2022: NONE. DEFECTIVE. MAIN DOOR LOCK: MAIN CABIN DOOR LOCK STUCK IN THE LOCKED POSITION. CANNOT OPEN THE MAIN CABIN DOOR FROM OUTSIDE AIRCRAFT. // SIGNOFF// REMOVED MAIN ENTRY DOOR L
- [SDR DXTA2022032158740](https://openairdocs.org/sdr/DXTA2022032158740), Mar 21, 2022: LENS. DEFECTIVE. MAIN DOOR VISUAL INDICATOR: MAIN CABIN DOOR LOCK INDICATION VISOR (LENS) IS MISSING.//CORRECTIVE ACTION// CLEANED AREA OF MISSING VISOR AND INSTALLED NEW VISOR.
- [SDR DXTA2021072645830](https://openairdocs.org/sdr/DXTA2021072645830), Jul 24, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: ON DESCENT INTO KEGE WE NOTICED THAT THE CABIN EMER LIGHTS WERE FLASHING.WE RECYCLED THE EMER LIGHT SWITCH BUT IT CONTINUED TO FLASH WITH THE
- [SDR JGVR20200209001](https://openairdocs.org/sdr/JGVR20200209001), Feb 9, 2020: BALANCE WEIGHT. CORRODED. LEVEL 1 CORROSION FOUND ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS. REMOVED LEVEL 1 CORROSION ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS IN 
- [SDR DXTA201804260879](https://openairdocs.org/sdr/DXTA201804260879), Apr 25, 2018: WARNING MESSAGE. MULTIPLE FAIL. RECEIVED A FLAP FAIL, SWPS FAULT, PTRIM BKP FAIL, AND SPOILER FAULT CAS MESSAGES ALONG WITH MAX SPD ABOVE THE AIRSPEED TAPE AND A DATA PATH HAS FAILED MESSAGE O
- [SDR DXTA2018012400509](https://openairdocs.org/sdr/DXTA2018012400509), Jan 23, 2018: UNKNOWN. ODOR. DETECTED A BURNING ODOR IN THE COCKPIT, SHORTLY AFTER TAKEOFF WITH THE COCKPIT TEMP CONTROL ABOUT 10 O'CLOCK. NOTICED A BURNING RUBBER ODOR. WE PUT THE TEMP CON
- [SDR DXTA2017092900001](https://openairdocs.org/sdr/DXTA2017092900001), Sep 26, 2017: VALVE. BROKEN. IN CRUISE AT FL410 WHEN DUCT 2 OVERTEMP CAS ILLUMINATED. FOLLOWED CHECKLIST PROCEDURES BUT DUCT TEMP CONTINUED TO RISE, ULTIMATELY REACHING 232F. AFTER APPROXIM
- [SDR DXTA2014072505832](https://openairdocs.org/sdr/DXTA2014072505832), Jul 24, 2014: GENERATOR. FAILED. AFTER LEFT ENGINE START WITH NO GPU ASSIST, RIGHT GEN FAIL CAS CAME ON. ELECTRIC SYNOPTIC SHOWED RIGHT GEN OFF. ALSO HAD ELECTRIC OZONE ODOR IN CABIN. REMOVED A

## Service difficulty reports on N335QS not matched to an aircraft (19)

They name N335QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200702723](https://openairdocs.org/sdr/DXTA200702723), Dec 30, 2007: UNKNOWN. UNKNOWN. ACFT DID NOT PRESSURIZE ON DEPARTURE. GROUND RAN AIRCRAFT CK LEFT AND RIGHT ENGINE SEPARATELY FOR PRESSURIZATION. OPS CK GOOD. CHECK PRE PRESS. OP'S CK GOOD. IN
- [SDR DXTA200702728](https://openairdocs.org/sdr/DXTA200702728), Dec 28, 2007: LINE. CONTAMINATED. EMERGENCY DECLARED, LOST PRESSURIZATION WHILE IN CRUISE AT FL390. HEARD AUDIBLE "POP" FOLLOWED BY AIR "HISSING" AND CABIN CLIMBING AT >4000 FPM. CABIN ALT REACH
- [SDR DXTA200702697](https://openairdocs.org/sdr/DXTA200702697), Dec 20, 2007: CONTROLLER. INOPERATIVE. WINDSHIELD OVERHEAT ANNUNCIATOR ILLUMINATED WITH WINDSHIELD HEAT SELECTED ON IN THE LOW POSITION. RAN CHECKLIST AND SELECTED OFF. CONDITION OCCURED ABOUT 30 TO 
- [SDR DXTA200702346](https://openairdocs.org/sdr/DXTA200702346), Jul 18, 2007: UNKNOWN. ODOR. STRONG BURNING ODOR ENCOUNTERED IN FLIGHT. TURNED OFF AIR CONDITIONER AND ODOR DISSIPATED. INSPECTED FWD AND AFT AIR CONDITIONING EVAPORATOR UNITS FOR BURNING S
- [SDR DXTA200702308](https://openairdocs.org/sdr/DXTA200702308), Jun 29, 2007: MASTER CYLINDER. LEAKING. DURING AIRCRAFT TAXI, CAPTAINS AND F/O RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE F/O PEDAL WENT TO THE FLOOR CAPTAINS SIDE WENT 
- [SDR DXTA200702300](https://openairdocs.org/sdr/DXTA200702300), Jun 25, 2007: BRAKE ASSY. WEAK. DURING AIRCRAFT TAXI, CAPTAINS SIDE RT BRAKE PEDAL LOSSES PRESSURE WHEN APPLYING BRAKES. WHEN LOSING PRESSURE, PEDAL GOES IN ABOUT 2 INCHES FARTHER, THEN SEEMS 
- [SDR DXTA200702037](https://openairdocs.org/sdr/DXTA200702037), Mar 18, 2007: ENGINE. SHUTDOWN. RT ENG SPOOLED DOWN TO 10-15 PERCENT N1 APPROX 2 MIN AFTER START WITH NO THROTTLE MOVEMENT, RAPID INCREASE IN ITT AT THE SAME TIME BUT NOT ABOVE LIMITATIONS. AL
- [SDR DXTA200601792](https://openairdocs.org/sdr/DXTA200601792), Dec 10, 2006: OXYGEN MASK. INOPERATIVE. PILOTS (LT) O2 MASK WILL NOT WORK IN EMERG NR O2 FLOW. REMOVED AND REPLACED O2 MASK. OPS CHECK GOOD IAW MM CH 35-10-01.
- [SDR DXTA200601678](https://openairdocs.org/sdr/DXTA200601678), Oct 22, 2006: ACTUATOR. INTERMITTENT. ON APPROACH TO KLUK, RT MAIN GEAR LIGHT WAS INOP. WENT AROUND AT ALT. DID EMERG CHECKLIST AND TROUBLESHOT. SPEED BRAKES, FLAPS PAST 35*, NO LIGHT ROTARY TEST DI
- [SDR DXTA200601642](https://openairdocs.org/sdr/DXTA200601642), Oct 9, 2006: POTENTIOMETER. MALFUNCTIONED. PUT GEAR DOWN NO RIGHT GEAR LIGHT, NO RED LIGHT. NO SECONDARY GEAR UNSAFE INDICATIONS. TROUBLESHOT, TURN DAY/NIGHT DIMMER SWITCH ON/OFF GOT ALL THREE GREEN INDI
- [SDR DXTA200601571](https://openairdocs.org/sdr/DXTA200601571), Aug 21, 2006: INDICATOR. UNKNOWN. DURING TAKEOFF, LEFT SIDE AIRSPEED LAG BEHIND RIGHT AIRSPEED, SUBSEQUENT "INASP" IN YELLOW ILLUMINATED, ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. SUSPEC
- [SDR DXTA200601456](https://openairdocs.org/sdr/DXTA200601456), Jun 25, 2006: SEAL. LEAKING. LOST CABIN PRESSURE AT FL 400. REMOVED & REPLACED SECONDARY DOOR SEAL. DOOR SUPPLY GROMMET & CHECK VALVE IAW CESSNA 560 M/M CHPT. 52-10-01, 52-10-00 & 21-30-00.
- [SDR DXTA200500924](https://openairdocs.org/sdr/DXTA200500924), Aug 25, 2005: BATTERY. OVERTEMP. BATTERY OVERTEMP AT 145 DEGREES STEADY, ANNUNCIATOR LIGHT ILLUMINATED, DELARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200500679](https://openairdocs.org/sdr/DXTA200500679), Apr 14, 2005: PRESSURE SYSTEM. FLUCTUATES. WILD PRESSURIZATION FLUCTUATIONS ON TAKEOFF SHORTLY FOLLOWED BY A PECULIAR ODOR. PRESSURE FLUCTUATIONS APPEARED TO BE ASSOCIATED WITH POWER CHANGES. ITEM IS UND
- [SDR DXTA200400431](https://openairdocs.org/sdr/DXTA200400431), Oct 23, 2004: BULB. BURNED OUT. RIGHT MAIN GEAR INDICATOR LIGHT INOP, EMERGENCY/ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTING AND RAN LANDING GEAR WILL NOT EXTEND CHECKLIST, FOUND
- [SDR DXTA200400303](https://openairdocs.org/sdr/DXTA200400303), May 2, 2004: IGNITER. FAILED. ON FIRST ATTEMPT RT ENGINE WOULD NOT LIGHT, ON SECOND ATTEMPT ENGINE LIGHT OFF AND STARTED. AFTER ENGINE START, WHILE AT IDLE THE RT ENGINE FLAMED OUT PRIOR TO 
- [SDR DXTA200400259](https://openairdocs.org/sdr/DXTA200400259), Mar 11, 2004: DOOR. STUCK. DURING EMERGENCY EGRESS TRAINING, FOUND EMERGENCY EXIT DOOR WOULD NOT OPEN. FOUND SEALANT BONDED TO EXIT STRUCTURE. REMOVED EXIT AND CLEANED SEAL, REMOVED AND R
- [SDR DXTA200300146](https://openairdocs.org/sdr/DXTA200300146), Oct 24, 2003: BULB. INOPERATIVE. DURING APPROACH AT TEB LT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED, EXTENDED GEAR WITH PNEUMATIC BLOW DOWN SYSTEM. REMOVED 4 INOPERATIVE LIGHT BULBS AND I
- [SDR 98ZZZX882](https://openairdocs.org/sdr/98ZZZX882), Feb 16, 1998: PANEL. MALFUNCTIONED. DURING INSPECTION, ATTEMPTED TO REMOVE THE EMERGENCY EXIT DOOR. FOUND NUMEROUS PROBLEMS. EXTERIOR HANDLE ROTATION DIFFICULT. HATCH HAD TO BE HIT HARD AT TOP TO 

## 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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