- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500772
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- December 28, 2023
- Certificate issued
- January 7, 2025
- Expires
- January 31, 2032
- Mode S code
- A5C9F7
Embraer Executive EMB-505TCDS A60CEAirframe · Embraer Executive EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 13
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2011 | 1 |
|---|---|
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 2 |
Airframe · Embraer Executive EMB-505
AD 2026-10-18Flight Control SystemAD 2026-03-05Autopilot Main ServoAD 2024-22-06Cabin Equipment/FurnishingsInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Embraer Executive EMB-505
SAIB CE-16-23Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) SignalSAIB CE-10-46Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight ManualNTSB investigations
No NTSB investigations matched to N472QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Embraer Executive EMB-505 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025012102008Battery Pack · defectiveMAIN EXIT SIGN/LIGHT: THE EMERGENCY LIGHTS STARTED FLASHING AFTER TAKE OFF. CORRECTIVE ACTION: REPLACED #1 & #2 EMERGENCY BATTERY PACK. OPS CHECK GOOD. IAW PHENOM 300 MM 33-52-01. OSD: 1/21/2025SDR DXTA2024120501374Window · failedON DEPARTURE, AN UNKNOWN OBJECT STRUCK THE CO-PILOTS SIDE FRONT WINDSHIELD. WINDOW WAS SMASHED. RETURNED TO SNA. CORRECTIVE ACTION; REMOVED AND REPLACED RH WINDSHIELD. PERFORMED CABIN PRESSURIZATION LEAK CHECK AND TEST OF THE WINDSHIELD HEATING SYSTEM WITH NO SDR DXTA2024102200909Brake Sys · contaminatedAFTER LEAVING THE CHOCKS WE HAD A SUCCESFULL BRAKE CHECK ON BOTH SIDES. UPON ENTERING THE TAXIWAY WE HAD A VIOLENT SHIMMY AND PULL TO THE RIGHT WHENEVER BRAKES WERE APPLIED. AFTER SHUTDOWN ON THE RAMP POST FLIGHT EXAMINATION DID NOT REVEAL ANY ABNORMALITIES. SDR DXTA2024092000594Brake Assy · vibrationLEFT MLG BRAKE: UPON LEAVING THE CHOCKS I APPLIED BRAKE PRESSURE AND THE BRAKES CONTINUOUSLY VIBRATED AND BECAME VERY "GRABBY". CORRECTIVE ACTION: BLEED BRAKE AND EMERGENCY/PARKING BRAKE SYSTEM BLEED IAW TC-E50-32-1001, REV 0 AND EMB505 AMM TASK 29-10-00-910-8SDR DXTA2024012510726Control Module · faultedUPON GEAR DOWN, 3 GREEN, BRK FAIL YELLOW CAS ILLUMINATED. TROUBLESHOT FOR FAULT CODE 32421300 PER FIM 32-41-00. R & R BRAKE CONTROL MODULE IAW AMM 32-41-07. REPAIRED BRAKE CONTROL MODULE INDUCED ANTI-SKID CAS MESSAGE & FAILURE OF RT BRAKE TRANSDUCER IN CM
Reports on N472QS not matched to an aircraft · 12
They name N472QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015031605996Unknown · smokeAFTER STARTING APU, BEFORE POWERING ANY AVIONICS, ETC SMOKE COMING FROM COPILOTS SIDE OF THE INSTRUMENT PANEL. PERFORMED A VISUAL INSPECTION FOR SECURITY, FRAYING OF WIRE BUNDLES, ANY SIGNS OF OVERHEATING OR SMOKE DAMAGE IN THE FOLLOWING AREAS: AFT EQUIPMENT SDR DXTA2015030905990Control Panel · failedDURING LEVEL FLIGHT AT 15,000 FEET, EXPERIENCED AUTO THROTTLES DISCONNECT THREE TIMES, AUTOPILOT DISCONNECT ONE TIME. DADC FAIL CAS MESSAGES, EPR 1 ADC FAIL CAS MESSAGE & FIRE DETECTION LT ENGINE LOOP A ALERT. CAS MSGS WOULD CYCLE ON FOR 3 - 5 SECONDS & TOSDR DXTA2013101165539Brake · stickingRIGHT BRAKE STICKING AND PULLING TO RIGHT.
STCs that may be installed · 47
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 47 STCs