# N330QS: 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: 50500180
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: December 18, 2013
- Certificate issued: July 5, 2024
- Expires: July 31, 2031
- Mode S code: A3973E
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=330QS
- Page: https://openairdocs.org/aircraft/N330QS

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 N330QS.

## FAA accident and incident reports

None matched to N330QS.

## Reports on N330QS not matched to an aircraft (1)

They name N330QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20020927030099I](https://openairdocs.org/incident/20020927030099I), Sep 27, 2002: Cessna 560CESSNA (N330QS), Lincoln, NE. (-23) On September 27, 2002 at approximately 06:00 CDT a Cessna 560, N330QS operated by netjets aviation inc. under certificate number DXTA401D departed…

## 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 DXTA2026101610157](https://openairdocs.org/sdr/DXTA2026101610157), Oct 12, 2026: CONTROL MODULE. FAULTED. RECEIVED BRAKE FAIL CAS MESSAGE ON FINAL INTO KAPF, EXECUTED GO AROUND, RAN QRH AND DIVERTED TO KRSW. LANDED SAFELY AND UTILIZED EMERGENCY BRAKE TO STOP AIRCRAF
- [SDR DXTA2025082904741](https://openairdocs.org/sdr/DXTA2025082904741), Aug 27, 2025: WIRE. MISINSTALLED. DURING CLIMB OUT WE RECEIVED THE EMER LT NOT ARM CAS MESSAGE AND OUR BATTERIES BEGAN TO DISCHARGE. DURING THE SHUTDOWN CHECKLIST THE AIRCRAFT WENT INTO ELECTRIC
- [SDR DXTA2025072804372](https://openairdocs.org/sdr/DXTA2025072804372), Jul 26, 2025: POWER SUPPLY. FAULTED. REPEAT WRITE UP: IMMEDIATELY AFTER GEAR RETRACTION, WE RECEIVED EMER LIGHT NOT ARMED CAS MESSAGE. THE EMERGENCY LIGHTS WERE ALL ILLUMINATED IN THE CABIN. THE BA
- [SDR DXTA2025072804343](https://openairdocs.org/sdr/DXTA2025072804343), Jul 23, 2025: ELEC CONNECTOR. DAMAGED. ALMOST IMMEDIATELY AFTER GEAR RETRACTION, WE REVEIVED EMER LIGHT NOT ARMED CAS MESSAGE. THE EMERGENCY LIGHTS WERE ALL ILLUMINATED IN THE CABIN. THE BATTERY VOLT
- [SDR DXTA2025070304100](https://openairdocs.org/sdr/DXTA2025070304100), Jun 30, 2025: CONTROL PANEL. FAULTED. DEPARTING KTYQ, RECEIVED AN EMER LT NOT ARM CAS MESSAGED AT 400FT EVEN THOUGH THEY WERE ARMED & NOTICED BOTH BATTERIES WERE YELLOW & DISCHARGING. DID NOT HAVE A
- [SDR DXTA2025042303163](https://openairdocs.org/sdr/DXTA2025042303163), Apr 20, 2025: BATTERY PACK. DEFECTIVE. CABIN EMERGENCY LIGHT: CABIN EMERGENCY LIGHTS STAY ON OR ARE FLASHING WITH THE SWITCH IN THE ARMED POSITION CORRECTIVE ACTION; REPLACED FORWARD AND AFT EMERGENC
- [SDR DXTA2025012702092](https://openairdocs.org/sdr/DXTA2025012702092), Jan 23, 2025: EXCITER. DEFECTIVE. LEFT ENGINE HUNG START: 80-10-06-01 WHEN STARTING ENGINE 1 OBSERVED IGNITION B FUEL FLOW, AND N1 HANG AT 4% ABORTED THE START, RAN THE ENGINE START MALFUNCTION 
- [SDR DXTA2024121101443](https://openairdocs.org/sdr/DXTA2024121101443), Dec 8, 2024: DOOR. UNSECURE. CABIN OXYGEN MASK STORAGE COMPARTMENT: THE PAX OXYGEN MASK COVER WILL NOT STAY ON. FOUND MASK COVER VELCRO WORN OR MISSING AND TAPE APPLIED AS A TEMPORARY FIX. 
- [SDR DXTA2024060511971](https://openairdocs.org/sdr/DXTA2024060511971), Jun 5, 2024: CONTROLLER. DEFECTIVE. FAINT BURNING ELECTRICAL SMELL COMING FROM RIGHT SIDE OF THE COCKPIT. ON THE PREVIOUS FLIGHT WINDSHIELD HEAT REMAINED OFF, THERE WAS NO SMELL. ON THIS FLIGHT TH
- [SDR DXTA2024060311959](https://openairdocs.org/sdr/DXTA2024060311959), Jun 3, 2024: UNKNOWN. ODOR. INTERMITTENT BURNING ELECTRICAL ODOR IN COCKPIT. ODOR STRONGEST TOWARDS RT END OF INSTRUMENT PANEL. REMOVED INSTRUMENT SCREENS & INSPECTED WIRING BEHIND PANEL, 
- [SDR DXTA2023120410229](https://openairdocs.org/sdr/DXTA2023120410229), Dec 3, 2023: UNKNOWN. FAULTED. ON POST FLIGHT NOTICED EMERGENCY LIGHT UNDER SEAT FOUR NOT SECURED. OPERATIONAL CHECK REVEALED NOT WORKING. REMOVED LED ESCAPE PATH MARKING P/N 0434LS00-01 DUE 
- [SDR DXTA2023082894060](https://openairdocs.org/sdr/DXTA2023082894060), Aug 27, 2023: UNKNOWN. UNKNOWN. RIGHT MLG BRAKE: RIGHT MAIN LANDING GEAR BRAKE WEAR INDICATOR NEARING LIMIT WHILE LEFT MAIN BRAKE WEAR INDICATOR ALMOST FULLY EXTENDED. BRAKES SEEM TO GO FROM V
- [SDR DXTA2022080267150](https://openairdocs.org/sdr/DXTA2022080267150), Aug 1, 2022: NONE. NONE. AVIONICS POWER: AS WE WERE CLIMBING THROUGH THE MID 20S WE STARTED TO NOTICE A STRANGE SMELL, IT WAS FAINT BUT IT DEFINITELY SMELLED ELECTRICAL. IT CONTINUED AS
- [SDR DXTA2021122153940](https://openairdocs.org/sdr/DXTA2021122153940), Dec 20, 2021: NONE. BROKEN. FIRST OFFICER COCKPIT WINDOW: COPILOT SIDE WINDSCREEN SHATTERED SHORTLY AFTER LEVELING OFF AT CRUISE ALTITUDE OF FLIGHT LEVEL 330. AFTER A NORMAL LANDING AND SH
- [SDR 2021FA0000087](https://openairdocs.org/sdr/2021FA0000087), Mar 23, 2021: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEV
- [SDR DXTA2020080543938](https://openairdocs.org/sdr/DXTA2020080543938), Aug 4, 2020: ACTUATOR. DEFECTIVE. CRUISING AT FL380 A GEA 1 FAIL ILLUMINATED. ALSO HAD NUMEROUS OTHER CAS MESSAGES. PRESN AUTO FAIL ADS 2 SLIP FAIL ADS 1 SLIP FAIL ENG NO DISPATCH THE AUTO PILOT
- [SDR DXTR2020011701](https://openairdocs.org/sdr/DXTR2020011701), Jan 16, 2020: FEEDER CABLE. SHORTED. OXY LO PRES YELLOW CAS - UNABLE TO COMPLETE PRE-FLIGHT OF OXYGEN MASK/SYSTEM. OXYGEN PRESS ON MFD SHOWS 1900 PSI / FULL. AMBER CAS MSG APPEARS DURING TEST AND S
- [SDR DXTA2017040806392](https://openairdocs.org/sdr/DXTA2017040806392), Apr 8, 2017: AUTOPILOT SYS. MALFUNCTIONED. GEA 1 FAIL CAS DISPLAYED. FOLLOWED BY: PRESN AUTO FAIL/OXY LO PRES CAUTIONS. ALSO ENG NO DISPATCH/ADS 1-2 SLIP ADVISORY MESSAGES. LOSS OF #1 ENG OIL PRESS/OIL T
- [SDR DXTA201504086002](https://openairdocs.org/sdr/DXTA201504086002), Apr 7, 2015: CONTROL UNIT. FAILED. SWPS FAULT & SPOILER FAULT EICAS IN FLIGHT. ASSOCIATED NO FLAP INDICATION YELLOW X'S & NO PITCH INDICATION YELLOW X'S. FOLLOWED QRH PROCEDURE & EXECUTED FLAPLES

## Service difficulty reports on N330QS not matched to an aircraft (44)

They name N330QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2008FA0000811](https://openairdocs.org/sdr/2008FA0000811), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000810](https://openairdocs.org/sdr/2008FA0000810), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000809](https://openairdocs.org/sdr/2008FA0000809), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000808](https://openairdocs.org/sdr/2008FA0000808), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000807](https://openairdocs.org/sdr/2008FA0000807), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000806](https://openairdocs.org/sdr/2008FA0000806), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000805](https://openairdocs.org/sdr/2008FA0000805), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000804](https://openairdocs.org/sdr/2008FA0000804), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000803](https://openairdocs.org/sdr/2008FA0000803), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000802](https://openairdocs.org/sdr/2008FA0000802), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000801](https://openairdocs.org/sdr/2008FA0000801), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000800](https://openairdocs.org/sdr/2008FA0000800), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000799](https://openairdocs.org/sdr/2008FA0000799), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000798](https://openairdocs.org/sdr/2008FA0000798), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000797](https://openairdocs.org/sdr/2008FA0000797), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000796](https://openairdocs.org/sdr/2008FA0000796), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000795](https://openairdocs.org/sdr/2008FA0000795), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000794](https://openairdocs.org/sdr/2008FA0000794), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000793](https://openairdocs.org/sdr/2008FA0000793), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000792](https://openairdocs.org/sdr/2008FA0000792), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR 2008FA0000791](https://openairdocs.org/sdr/2008FA0000791), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH 
- [SDR DXTA2008111403355](https://openairdocs.org/sdr/DXTA2008111403355), Oct 24, 2008: RIB. CRACKED. WHILE COMPLETING A LUBRICATION SEVERAL CRACKS HAVE BEEN FOUND IN HORZ STAB RIBS, P/N 65320XX-XXX.
- [SDR DXTA200702675](https://openairdocs.org/sdr/DXTA200702675), Dec 13, 2007: UPLOCK SWITCH. OUT OF ADJUST. AFTER RETRACTING THE GEAR, THE HYD PRESS ON LIGHT AS WELL AS THE GEAR UNLOCKED LIGHTS WERE ON. WE RAN THE CHECKLISTS BROUGHT THE GEAR DOWN AND USED THE BLOW DOW
- [SDR DXTA200702665](https://openairdocs.org/sdr/DXTA200702665), Dec 9, 2007: CONTROLLER. OBSTRUCTED. ON TAKE-OFF CABIN CONTROLLER FAILED TO MAINTAIN CABIN PRESSURIZATION. TROUBLESHOT TO VENT BLOCKAGE ON CONTROLLER. CLEARED BLOCKAGE AND PERFORMED OPS CHECK. OPS 
- [SDR DXTA200702282](https://openairdocs.org/sdr/DXTA200702282), Jun 21, 2007: LANDING GEAR. INOPERATIVE. ON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. AUXILLARY GEAR CONTROL WAS ACTIVATED AS A PRECAUTION. [07-12-07] T/S FOUND LEFT GEAR SQUAT SWITCH OUT OF ADJUSTMEN
- [SDR DXTA200702272](https://openairdocs.org/sdr/DXTA200702272), Jun 17, 2006: DISPLAY. FAILED. ON TAXI OUT PFD NR 2 FAILED. BURNED ELECTRONIC SMELL WAS OBSERVED. [07-10-07] REMOVED AND REPLACED NR 1 PFD IAW CESSNA 560 MM 34-23-02. PFD OPS CHECKS SERVICEAB
- [SDR DXTA200601293](https://openairdocs.org/sdr/DXTA200601293), Mar 13, 2006: HYDRAULIC SYSTEM. UNDERSERVICED. CO-PILOTS SIDE RT BRAKE PEDAL IS SOFT. WILL STOP AIRCRAFT HOWEVER WILL TRAVEL APPROX 1.5 INCHES BEFORE PRESSURE IS FULL. WHEN APPLYING BRAKES LEFT SIDE WILL HOL
- [SDR DXTA200601257](https://openairdocs.org/sdr/DXTA200601257), Feb 22, 2006: PROXIMITY SWITCH. MALFUNCTIONED. AFTER TAKEOFF, GEAR RETRACTION THE GEAR HORN WARNING SOUNDED. IT LASTED FOR A COUPLE SECONDS, THEN THE GEAR UNSAFE LIGHT WENT OUT AS WELL AS THE HORN STOPPED. A
- [SDR DXTA200601230](https://openairdocs.org/sdr/DXTA200601230), Feb 2, 2006: WARNING SYSTEM. MALFUNCTIONED. AFTER TAKEOFF UPON GEAR RETRACTION, THE GEAR WARNING HORN SOUNDED. IT LASTED FOR A COUPLE SECONDS THEN GEAR UNSAFE LIGHT (RED LIGHT) WENT OUT AS WELL AS THE HOR
- [SDR DXTA200500684](https://openairdocs.org/sdr/DXTA200500684), Apr 18, 2005: BRACKET. DAMAGED. AFTER DEPARTURE GEAR UNSAFE LIGHT REMAINED LIT AND HYD PRESS LIGHT ALSO REMAINED ILLUMINATED. GEAR RETURNED TO DOWN AND LOCKED AFTER PERFORMING CHECK LIST ITEMS
- [SDR DXTA200400361](https://openairdocs.org/sdr/DXTA200400361), Aug 16, 2004: POSITION SWITCH. MALFUNCTIONED. AFTER POSITIVE RATE OF CLIMB DURING TAKEOFF THE GEAR WOULD NOT FULLY RETRACT, WHEN THE GEAR SELECTOR WAS MOVED TO THE UP POSITION THE MAIN GEARS WOULD NOT STOW 
- [SDR DXTA200300172](https://openairdocs.org/sdr/DXTA200300172), Nov 29, 2003: ODOR. DETECTED. LOUD BANG WAS HEARD AND FELT WHILE CLIMBING THROUGH FL 37 AN ODOR WAS MOMENTARILY ASSOCIATED WITH IT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS
- [SDR DXTA200300144](https://openairdocs.org/sdr/DXTA200300144), Oct 21, 2003: RELAY. FAILED. AFTER SELECTING GEAR DOWN, POWER BRAKE LOW PRESS, ANTI SKID INOP ANNUNICATORS CAME ON, NO BRAKE PRESS EITHER SIDE. GO AROUND, ON SECOND APPROACH BOTH LIGHTS REM
- [SDR DXTA200300138](https://openairdocs.org/sdr/DXTA200300138), Oct 15, 2003: SCREW. LOOSE. AFTER LANDING AT BUY, BRAKES FAILED ON BOTH PILOT’S AND FIRST OFFICER’S SIDES, HAD TO USE EMERGENCY BRAKE TO STOP AIRCRAFT. FOUND LOOSE SCREW ON RT SPEED TRANSD
- [SDR DXTA200300137](https://openairdocs.org/sdr/DXTA200300137), Oct 14, 2003: BRAKE. MALFUNCTIONED. ON TAXI OUT FIRST 5 BRAKE APPLICATIONS WERE NORMAL, ON THE SIXTH APPLICATION BRAKE PEDALS WENT TO THE FLOOR, CO-PILOTS BRAKES WERE SPONGY BUT AFTER PUMPING BRAK
- [SDR DXTA200300091](https://openairdocs.org/sdr/DXTA200300091), Aug 15, 2003: BRAKE. FAILED. COPILOT'S BRAKE FAILED ON TAXI, PILOT'S BRAKES PULSATING DURING SLOW TAXI. - PERFORMED BRAKE BLEED PROCEDURE IAW CE560 MM CHAPTER 32-42-01 LEAK CHECK GOOD. FUNC
- [SDR DXTA200300047](https://openairdocs.org/sdr/DXTA200300047), Jun 14, 2003: WIRE HARNESS. DEFECTIVE. ON LANDING, BRAKE PRESSURE AVAILABLE BUT SLOW TO APPLY. DURING TAXI IN, ABOUT 10 MPH, BRAKES RELEASE AND ENGAGE INTERMITTENTLY. TROUBLESHOT AND FOUND RT ANTI-SK
- [SDR DXTA200300046](https://openairdocs.org/sdr/DXTA200300046), Jun 11, 2003: BRAKE. FAILED. ON TAXI IN DEPRESSED BRAKE AND AIRCRAFT WOULD NOT STOP FOR 2-3 SECOND . WITH BRAKE PEDALS DEPRESSED AIRCRAFT CONTINUED TO ROLL FOR SHORT DISTANCE. ITEM IS UNDER
- [SDR DXTA200300007](https://openairdocs.org/sdr/DXTA200300007), Feb 10, 2003: WIRE. CHAFED. DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY
- [SDR DXTA20030007](https://openairdocs.org/sdr/DXTA20030007), Feb 10, 2003: WIRE. CHAFED. DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY
- [SDR DDXTA20030007](https://openairdocs.org/sdr/DDXTA20030007), Feb 10, 2003: WIRE. CHAFED. DURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY
- [SDR 98ZZZX4821](https://openairdocs.org/sdr/98ZZZX4821), Oct 19, 1998: WIRE. FAILED. SMOKE OBSERVED COMING FROM THE AFT LAVATORY AREA. BATTERY SWITCH WAS TURNED OFF, AND GROUND POWER UNIT DISCONNECTED FROM ACFT. A CHECK OF CIRCUIT BREAKERS IN TH
- [SDR 97DXTA091](https://openairdocs.org/sdr/97DXTA091), Nov 8, 1996: INVERTER. FAILED. FLT 72905 - NR 2 INVERTER INOPERATIVE. (X)
- [SDR 96ZZZX6171](https://openairdocs.org/sdr/96ZZZX6171), Oct 30, 1996: RUDDER SKIN. CRACKED. LT RUDDER SKIN HAS 2 INCH CRACK APPROX 3 INCHES BELOW TRIM TAB FWD OF HINGE LINE. THIS IS THE SECOND DISCOVERED VERTICAL CRACK, AND THE SIXTH RUDDER SKIN CRACK 

## 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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