- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500470
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- August 31, 2018
- Certificate issued
- September 10, 2025
- Expires
- September 30, 2032
- Mode S code
- A50BEA
Embraer Executive EMB-505TCDS A60CEAirframe · Embraer Executive EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E
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 N424QSMatched 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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20250706012009ILanding: Rollout · Ludington, MI- See also sas/task #T-GL07-FY26-0012 - Because the NTSB elected to defer the inIncident 20200118005139ITaxi · Lincoln, NEOn January 18, 2020, at approximately 1529Z, N424QS which was operated as a part 91K flight by netjets aviation, inc., experienced a taxiway excursion. The excursion resulted in collapse of the left main landing gear and the left wingtip striking the ground.…
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026052108156Brake Sys · abnormalDURING TAXI OUT, AIRCRAFT BRAKING SYSTEM BEGAN TO SHUDDER. NOTICEABLE IN BOTH LEFT AND RIGHT BRAKES, HOWEVER THE RIGHT SIDE WAS MUCH MORE EXTREME. NO CAS MESSAGES WERE DISPLAYED. NO ABNORMALITIES WERE NOTED ON POST FLIGHT VISUAL INSPECTION. PERFORMED BLEEDINSDR DXTA2025071004151Brake Sys · failedUPON LANDING I APPLIED BOTH MAIN BRAKES AND HAD NO RESPONSE FOR STOPPING. FO THEN TRIED HIS BRAKES WITH NO RESPONSE EITHER. I THEN PULLED THE EMERGENCY BRAKE AND HAD NO RESPONSE FOR STOPPING. ANTI-SKID FAIL CAS MESSAGE APPEARED ON LANDING ROLLOUT. NR 1 WHEEL SDR DXTA2025021002303Brake Assy · malfunctionedMLG BRAKE PRESSURE: TAXIING OUT, THERE WAS AN ABNORMAL AND VERY PRONOUNCED SHUTTERING OF THE BRAKES AS IF WE WERE ON ICE SKIDDING. WE STARTED TAXIING BACK TO THE FBO THEN THE LEAD PAX NOTICED ALSO AND ASKED IF THE BRAKES WERE OK. CORRECTIVE ACTION: PERFORMED TSDR DXTA2024110100997Battery Pack · defectiveCABIN EMERG LIGHT: EMER LIGHTS ILLUMINATE IN THE ARMED POSITION CORRECTIVE ACTION; REPLACED #1 EMERGENCY BATTERY IAW PHENOM 300 AMM 33-52-01-960-801-A. OPS CHECK SATISFACTORY.SDR DXTA2024100300741Indicator · out of alignmentMAIN DOOR VISUAL INDICATOR: BOTH HANDLE INDICATORS ARE MISALIGNED WHEN THE DOOR IS CLOSED AND LATCHED. CORRECTIVE ACTION: ADJUSTED MED VISUAL INDICATORS TO BE VISIBLE WHEN THE MED IS CLOSED AND LATCHED. IAW EMB-505 AMM CH 52-10-00/200SDR DXTA2023092596380Brake · faultedWHEN BRAKING, FEELING AN HEARING ABRUPT GRINDING VIBRATION FEELING AS IF ON GRAVEL. REMOVED WORN LH BRAKE AND INSTALLED OVERHAULED BRAKE ASSEMBLY IAW AMM 32-45-21. SERVICED MAIN HYDRAULIC SYSTEM WITH 1QT FLUID 881 IAW AMM 12-13-00. LEAK AND OPS CHECKS GOODSDR DXTA2023071891190Unknown · unknownFLAP FAIL YELLOW CAS: FLAP FAIL YELLOW CAS ILLUMINATED DURING TAKE-OFF. FLAPS STUCK IN THE NUMBER ONE POSITION.SDR DXTA2022122076740Seal · leakingMAIN DOOR ACOUSTIC SEAL: 4TH WRITEUP; DURING CLIMB AT7.4 PSI AND 22,000 FEET, A LOUD WHINE NOISE AROUND UPPER LEFT QUADRANT OF MAIN CABIN DOOR STARTED AND BECAME PROGRESSIVELY LOUDER THROUGH FLIGHT. SOUND BEGAN TO DISSIPATE DURING DESCENT THROUGH 17000 FEET ATSDR DXTA2022121275930Indicator · missingLOWER LT (WITH MAIN DOOR CLOSED) LATCH INDICATOR MISSING. REMOVED THE LATCH PIN AND INSTALLED A NEW LATCH PIN IAW AMM 52-11-21. OPS CHECK GOOD. NO DEFECTS NOTED. CONFIGURED AIRCRAFT BACK TO ORIGINAL CONFIRGURATION.SDR DXTA2022120575350Seal · damagedLOUD WHISTLING SOUND EMANATING FROM UPPER PART OF MAIN CABIN DOOR AT ALTITUDE WHERE DELTA P RANGED FROM 9.2 PSI TO 6.5 PSI. PASSENGER WAS DISTURBED BY THE NOTICEABLE SOUND AND CONTACTED CREW. SEAL AROUND MAIN CABIN DOOR APPEARS TO HAVE BEEN PATCHED WHERE SOU
Reports on N424QS not matched to an aircraft · 12
They name N424QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2012FA0000541Flap Track · corrodedRT "B" FLAP TRACK CORRODED, REF BP SE45811104, REV B FOR REPAIR.SDR 2012FA0000538Structure · corrodedRIGHT WINGLET ATTACH HOLES CORRODED, REFERENCE BP SE5809903 REV. C FOR REPAIR.SDR 2012FA0000537Structure · corrodedLEFT WINGLET ATTACH HOLES CORRODED, REF BP SE35809903, REV C FOR REPAIR.
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