- Owner type
- Co-owned
- Serial number
- 50500432
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 17, 2017
- Certificate issued
- August 4, 2025
- Expires
- August 31, 2032
- Mode S code
- A4D946
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 N411QSMatched 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
No FAA accident or incident reports matched to N411QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Embraer Executive EMB-505 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026081409255Elec Connector · not seatedEMERGENCY EXIT SIGN LIGHT INOP ABOVE MAIN CABIN DOOR CORRECTIVE ACTION: FOUND THE EMERGENCY EXIT LIGHT CONNECTOR WAS NOT FULLY SEATED ON ITS RECIPROCAL, WHEN TECHS ATTEMPTED TO RESEAT THE CONNECTOR WE NOTED IT WAS PREVIOUSLY INSTALLED 180 DEGREES / OUT. TECHS SDR DXTA2025060903811Seal · fodEMERG EXIT DOOR SEAL: PAX COMPLAINED THAT A VERY LOUD WHISTLE SOUND WAS COMING FROM THE EMERG EXIT DOOR DURING FLIGHT. CORRECTIVE ACTION: CLEANED DEBRIS FROM DOOR SEAL. OPS CHECK GOOD. WORK IAW PHENOM 300 AMM CH 52-20-00SDR DXTA2025060903810Battery · defectiveCABIN EMERG LIGHT: WHILE TAXIING IN, CABIN EMER LIGHTS WERE BLINKING WITH THE SWITCH IN ARM POSITION. CORRECTIVE ACTION: REMOVED FWD AND AFT EMERGENCY LIGHT BATTERIES, WITH CUSTOMER SUPPLIED BATTERIES IAW PHENOM 300 AMM CH 33-52-01. OPS CHECKS GOOD.SDR DXTA2024120301336Battery Pack · faultedCABIN EMERGENCY LIGHTS DID NOT EXTINGUISH DURING THE ENTIRE FLIGHT WITH THE EMER LT SWITCH IN THE ARM POSITION. AFTER LANDING WITH MAIN BATT 1/2 OFF ALL EMERGENCY LIGHTS BEGAN TO FLICKER UNTIL EMER LT SWITCH TURNED OFF. CORRECTIVE ACTION; REMOVED AND REPLACED SDR DXTA2024031311178Battery · inoperativeCABIN EMER LIGHTS STAY ILLUMINTED WHEN THE SWITCH IS IN THE ARM POSITION. REMOVED DEFECTIVE FWD EMR BATTERY PACK AND REPLACED WITH A NEW CUSTOMER SUPPLIED BATTERY. REMOVED INOP AFT EMR BATTERY PACKS AND REPLACED WITH A TESTED, CUSTOMER SUPPLIED BATTERY PACK ISDR DXTA2024020910840Battery · defectiveSELECTING EMERGENCY. EXIT LIGHTS (CABIN EMERGENCY EXIT LIGHTS REMAIN ON). REMOVED AND REPLACED AFT CABIN EMERGENCY BATTERY (#2 BATTERY) PACK WITH "TESTED" UNIT. OPS CHECKS IN ARMED AND ON/OFF POSITIONS. MX IAW MM33-52-01.SDR DXTA2023092796570Unknown · unknownAT 400FT WE SELECTED FLAPS UP AND GOT THE FLAP FAIL INDICATION. RAN QRH CHECKLIST WITH NO CHANGE. LANDING WITHOUT INCIDENT. UPON ARRIVAL, NOTED LH AND RH FLAPS WERE NOT FULLY STOWED. CYCLED THE FLAPS 10 TIMES WITHOUT GETTING A FLAP FAIL CAS MESSAGE. THE FLAPSDR DXTA2023021780540Drive Assy · abnormalWHILE TROUBLESHOOTING AN INOP VCS TECHS DISCOVERED THERMAL DAMAGE TO COMPRESSOR DRIVE MODULE CONTROL UNIT AND ASSOCIATED POWER LUG. REMOVED COMPRESSOR DRIVE MODULE PN: 1133640-5, SN: 559. INSTALLED REPAIRED COMPRESSOR DRIVE PN: 1133640 9, SN: 880 WITH NEW O-SDR DXTA2021041940900Sensor · defectiveGND SPLR FAIL YELLOW CAS: IN THE DESCENT FROM APPROXIMATELY 22,000', SPOILERS WERE SELECTED AND IMMEDIATELY FAILED. WHITE SPOILER FAULT CAS APPEARED SIMULTANEOUSLY WITH THE YELLOW GND SPLR FAIL CAS. // SIGN OFF // REMOVED AND REPLACED THE LH MULTIFUNCTION SPOISDR 2020FA0000523Balance Weight · corrodedDURING 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 ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (7 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PASDR DXTA2019121003182Starter Gen · failedGEN 2 OFF BUS YELLOW CAS ILLUMINATED - SOON AFTER TAKEOFF CREW NOTICED AN UNUSUAL AND SIGNIFICANT VIBRATION IN THE RUDDER PEDALS AS WELL AS AN AUDIBLE RUMBLE, MORE NOTICEABLE WITH NOISE CANCELLING HEADSETS BUT ALSO WITHOUT. CLIMBING THRU APPROX FL180 CREW RECE
Reports on N411QS not matched to an aircraft · 9
They name N411QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR N93A29092007Steering Sys · malfunctionedNOSE STEERING PULLS TO RIGHT WHEN HANDWHEEL IS CENTERED. (OPEN)SDR N93A18062007Frame · crackedDURING 5000 LANDING INSPECTION, THE FRAME AT THE 793 BULKHEAD WAS FOUND CRACKED.SDR N93A18062007AFrame · crackedDURING 5000 LANDING INSPECTION, THE FRAME AT THE 793 BULKHEAD WAS FOUND CRACKED.
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