- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500331
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- February 17, 2016
- Certificate issued
- August 6, 2026
- Expires
- August 31, 2033
- Mode S code
- A487EF
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 N391QSMatched 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
Investigations on N391QS not matched to an aircraft · 1
They name N391QS, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
FAA incident reports
No FAA accident or incident reports matched to N391QSMatched 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
Reports on N391QS not matched to an aircraft · 1
They name N391QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026072708959Tab · out of positionMAIN CABIN DOOR WILL NOT UNLOCK. MED KEY LOCK CYLINDER IS NOT ROTATING, KEY INSERTS BUT NO MOVEMENT.CLEANED AND LUBRICATED MULTIPLE TIMES. LUBED BACKSIDE OF LOCK ASSEMBLY. KEY TURNED BUT VERY DIFFICULT. FOUND LOCKING TAB OUT OF POSITION CAUSING IT TO JAM. RE SDR DXTA2025022802532Battery · faultyEMERGENCY LIGHTS ARE FLICKERING ENROUTE AND UPON LANDING AND AFTER SHUTDOWN. CORRECTIVE ACTION; REMOVED FORWARD AND AFT EMERGENCY BATTERJES AND REPLACED WITH REPAIRED UNITS PROVIDED BY CUSTOMER IAW EMB AMM 33-52--01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TISDR DXTA2023070390130Fuel Control · defectiveRIGHT FUEL QUANTITY INDICATION: IN FLIGHT, RIGHT AND TOTAL FUEL QUANTITY WAS YELLOW XED ON THE EICAS. ON THE FUEL SCHEMATIC PAGE THERE WERE 19 YELLOW XS. ALL VENTS, VALVES ETC. ONLY RIGHT FUEL QUANTITY AND FUEL USED WERE DISPLAYED.//CORRECTIVE ACTION// R/R ELSDR DXTA2023060587960Battery · abnormalDURING DESCENT THE CABIN EMERGENCY LIGHTS WERE FLASHING ON AND OFF. AFTER LANDING, WITH GROUND POWER APPLIED, THE CABIN EMERGENCY LIGHTS ARE ON STEADY WITH THE EMER LT SWITCH IN ARM. PERFORMED ISOLATED FUNCTIONAL CHECK OF EMERGENCY LIGHT BATTERY PACKS, NOTED SDR DXTA2023030681900Battery · dischargedCABIN EMERG LIGHT: IN FLIGHT WITH EMER LT SWITCH IN THE ARM POSITION, CABIN EMER LIGHTS FLASHING. *** CORRECTIVE ACTION *** REMOVED AND REPLACED BOTH FWD AND AFT EMERGENCY BATTERY WITH REFERENCE TO EMB-505 AMM 33-52-01, OPS CHECKS GOOD.SDR DXTA2021092048990Battery · defectiveEMERGENCY LIGHTS BATTERY: DURING FLIGHT WE NOTICED THAT ALL THE EMERGENCY LIGHTS WERE ON WITH THE SWITCH IN THE ARM POSITION. THE EMERGENCY LIGHTS THEN BEGAN TO FLICKER, AND WE THEN TURNED THE SWITCH TO OFF. // SIGNOFF // REMOVED AND REPLACED EMERGENCY LIGHT BSDR 2021FA0000014Balance 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: RUDDER ADJUSTABLE WEIGHTS PART NUMBER PE915109-L27 (19 EACH BELOW MINIMUM OF 455G), WE ALSO NOTED THE FOLLOWINGSDR DXTA2018032600766Brake Sys · contaminatedBRAKES WERE APPLIED EVENLY AFTER TOUCHDOWN. BRAKES APPEARED TO QUIT BELOW 40 KNOTS AND THEN STARTED WORKING AGAIN AT A SLOWER SPEED. OVERALL BRAKES FEEL SOFT. SUP: COMPLIED WITH BRAKE ASSY GVI IAW AMM 32-41-60. NO LEAKS OR DEFECTS NOTED. COMPLIED WITH MAIN B
Reports on N391QS not matched to an aircraft · 16
They name N391QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2010082004199Engine · shutdownNR 2 ENGINE SHUTDOWN ON THE SPEED BRAKE TEST. 2 ATTEMPTS, AND BOTH TIMES THE ENGINE SHUTDOWN. THE THROTTLE WAS NOT SLAMMED TO THE STOPS.SDR DXTA2010021503987Brake Sys · weakCO-PILOTS RT BRAKE PEDAL WENT TO THE FLOOR DURING TAXI. PEDAL REQUIRED MULTIPLE PUMPS TO BUILD ANY PRESSURE. PERFORMED VISUAL INSP OF BRAKE SYS. NO LEAKS NOTED. IAW CUSTOMER REQUEST TO COMPLIED WITH BRAKE BLEEDING PROCEDURE. COMPLIED WITH BRAKE BLEEDING. SDR DXTA2010020103964Brake Sys · weakCO-PILOTS RT BRAKE PEDAL GOES TO THE FLOOR AT BRAKE APPLICATION; VERY LIMITED BRAKING FROM THE RT PEDAL. PERFORMED MANUAL AND POWER BRAKE SYS BLEEDING PROCEDURE. OPS CHECK GOOD. WORK PERFORMED IAW AMM 32-42-00.
See all 16 unmatched reportsSTCs 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