- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500328
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- January 29, 2016
- Certificate issued
- February 11, 2026
- Expires
- February 28, 2033
- Mode S code
- A48438
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 N390QSMatched 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 N390QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026010706438Unknown · odorAT 31000' WE NOTICED A FURLING HAZE IN THE CABIN. IT DID NOT SMELL SMOKY BUT RESEMBLED A PROFESSIONAL STERILE SMELL. CALLED FODM AND THE HAZE DISSIPATED. HE CONTACTED MX MGR AND WAS DIRECTED TO DIVERT TO KFLL AS THEY FELT THE DUCTS NEEDED MORE PURGING FROM THSDR DXTA2026010206358Engine · faultyUPON CLIMBING THROUGH APROX 2500', RECEIVED A E2 OIL LOW PRESSURE CAS MESSAGE. ADVISED NEEDED TO RETURN TO AIRPORT. ABOUT A MINUTE LATER DETECTED A BURNING ODOR WHICH WAS SHORTLY FOLLOWED BY SMOKE FILLING THE CABIN. DECLARED AN EMERGENCY & ADVISED RETURNING. RSDR DXTA2025110305512Battery Pack · defectiveEMERGENCY LIGHTS ARE STAYING ILLUMINATED IN THE ARM POSITION. REPLACED BATTERIES. OPS CHECK GOOD. IAW AMM 33-52-01/400SDR DXTA2025072804348Battery Pack · inoperativeDURING CRUISE THE EMERGENCY LIGHTS (WHILE IN THE ARM POSITION) PROCEEDED TO STAY ILLUMINATED AND THEN CONTINUOUSLY FLICKER. REMOVED AND REPLACED #1 FWD & #2 AFT EMERGENCY BATTERY REF EMS PHENOM 300 MM 33-52-01, OPS CHECKS GOOD AT THIS TIME NO DEFECTS NOTEDSDR DXTA2024120301347Hydraulic System · low pressureMAIN HYDRAULICS: HYDRAULI LOW PRESSURE FAILURE- FAILED -PUSHER, BRAKES, GEAR, SPEEDBRAKE, RUDDER BOOSTER. ONCE AIRCRAFT WAS PLACED IN A HANGER TECHS NOTED HYDRAULIC FLUID LEAKAGE FROM BELLY AREA AFT OF LANDING GEAR. REACHED OUT TO MCC AND DISCUSSED FINDINGS. SDR DXTA2024120301348Priority Valve · leakingEMERG BRAKE: USED EMERGENCY BRAKE BECAUSE HYDRAULIC SYSTEM FAILED BLOWING BOTH MAIN TIRES. PERFORMED REQUESTED ENGINE RUN AND IMMEDIATELY NOTICED HYDRAULIC FLUID LEAK FROM THE PRIORITY VALVE. REMOVED LEAKING PRIORITY VALVE. INSTALLED RECEIVED TESTED PRIORITSDR DXTA2024103000984Rod · out of adjustMAIN CABIN DOOR HANDLE IS VERY STIFF & DIFFICULT TO CLOSE AND SECURE FROM THE INSIDE. ADDITIONALLY, WHEN HANDLE IS SECURED IN CLOSED POSITION THE STATUS PAGE SHOWS THE CABIN DOOR IS STILL OPEN. THERE IS NO GREEN FLAG PRESENT IN LOCK SIGHT WINDOW LOCATED ON BOTSDR DXTA2024102800973Handle · bindingWHEN CLOSING MAIN CABIN DOOR FROM THE INSIDE THE RED HANDLE IS STICKING IN POSITION HALF WAY DOWN. IT TAKES A LOT OF FORCE TO MOVE THE HANDLE TO THE LOCKED POSITION ACCOMPLISHED PHENOM 300 AMM TASK 52-10-00-820-805-A -MAIN-DOOR LOCKING AND ACTUATING MECHANISSDR DXTA2023082894010Battery · defectiveCABIN EMERG LIGHT: CABIN EMER LIGHTS ILLUMINATED WITH THE EMER LIGHT SWITCH IN THE "ARMED" POSITION. CYCLED THE EMER LIGHT SWITCH OFF, THEN BACK TO ARM - CABIN EMER LIGHTS CONTINUED TO STAY ILLUMINATED. PERFORMED INERTIA SWITCH REACTIVATION WITH NO FIX. PERFSDR DXTA2021081847160Power Supply · defectiveCABIN EMERG LIGHT: IN CRUISE AT FL430 CABIN EMER LIGHTS FLICKERING ON AND OFF. CONTINUED THROUGH FLIGHT. GAINED ACCESS BY REMOVING CO-PILOTS SEAT AND CENTER FLOORBOARDS AFT OF PEDISTAL. REMOVED 3 EA VERTICAL PANELS IN AFT LAV. REMOVED THE FOLLOWING POWER SUPSDR 2021FA0000065Balance 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 AILERON: AILERON MASS WEIGHT PART NUMBER PE915109-L31 (1 EACH BELOW MINIMUM OF 1787G),WEIGHT HAS BEEN RESDR DXTA2021013100465Battery Pack · malfunctionedCABIN EMERGENCY LIGHTS FLASHING IN FLIGHT WITH THE EMER LT SWITCH IN ARM. CORRECTIVE ACTION: REMOVED FWD EMER BATTERY P/N 6450LS-00, S/N 001098 AND AFT EMERGENCY BATTERY P/N 6450LS-00, S/N 000966 AND INSTALLED MODIFIED UNIT. OPERATIONS CHECKS GOOD.SDR DXTA2021011804598Battery · defectiveCABIN EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY IN FLIGHT WITH LIGHT SWITCH IN "ARMED" POSITION. REMOVED AND REPLACED DEFECTIVE FWD AND AFT EMERGENCY BATTERIES, IAW EMB 24-65-03. OPERATONS CHECK GOOD.
Reports on N390QS not matched to an aircraft · 12
They name N390QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200807243197Bearing · wornON CLIMB, FELT VIBRATION IN ALL CONTROLS AND COCKPIT SEATS. AT LEVEL OFF FELT VIBRATION SAME AS IN CLIMB BUT ALSO IN CABIN SEATS AND CABIN SIDEWALLS LT SIDE REPORTED WORSE THAN RT SIDE, DESCENT FELT VIBRATIONS ALSO. FOUND RUDDER TRIM AND LT ELEVATOR TRIM TABSSDR DXTA200803197Unknown · vibrationON CLIMB FELT VIBRATION IN ALL CONTROLS AND COCKPIT SEATS. (A)SDR DXTA200802829Connector · brokenWHILE AT CRUISE ALT 32000 WITH 28 MIN INTO THE FLIGHT, ACFT FAIL LIGHT CAME ON WITH MASTER WARNING. ACFT FAIL LIGHT STAYED ON UNTIL WE RESET MASTER WARNING AFTER 5 MIN. DURING THIS TIME VOLTS SHOWED 28 AND GENS SHOW 50 AMPS EACH AND WERE STEADY. INVERTERS SHOW
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