- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500152
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 26, 2013
- Certificate issued
- September 17, 2024
- Expires
- September 30, 2031
- Mode S code
- A34230
Embraer S A EMB-505TCDS A60CEAirframe · Embraer S A 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 S A 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 S A 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 N309QSMatched 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 S A EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N309QSMatched 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 S A EMB-505 aircraft
Reports on N309QS not matched to an aircraft · 1
They name N309QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025120505973Light · inoperativeLOWER EMERGENCY EXIT SIGN LIGHT DOES NOT ILLUMINATE TECHS GOT ONISTE AND VERIFIED THAT THE AFT EMER LIGHT WAS INOP. TECHS THEN SWAPPED THE AFT EMER LIGHT TO THE FWD AND FAULT DID NOT FOLLOW. WE THEN PUT EVERYTHING INTO NORMAL CONFIGURATION AND ALL LIGHTS ARE SDR DXTA2025040702971Sign · inoperativeMAIN EXIT SIGN/LIGHT: MAIN EXIT DOOR LIGHT INOP. CORRECTIVE ACTION: REMOVED FAULTY EXIT SIGN AND INSTALLED A CUSTOMER SUPPLIED NEW EXIT SIGN IN ACCORDANCE WITH EMBRAER PHENOM 300 AIRCRAFT MAINTENANCE MANUAL 33-52-13 WITH NO DEFECTS NOTED. P/N ON/OFF: 5315-00 NSDR DXTA2025032802809Spoiler Sys · faultedDRAG CONTROL (SPEEDBRAKES & SPOILERS): SPOILER WAS COMMANDED OPEN, BUT THEY SLAMMED CLOSED AND JOLTED THE AIRCRAFT. VISUAL INSPECTION SHOWED THE SPOILERS FLUTTERING WHILE IN FLIGHT. MULTIPLE SPOILER MESSAGES OCCURRED. CORRECTIVE ACTION: VISUALY CHECKED THE SPOSDR DXTA2024091600538Battery · failedCABIN EMERG LIGHT: CABIN EMERG LIGHT ON IN FLIGHT WITH THE SWICH ON ARM POSITION CORRECTIVE ACTION: REMOVED AND REPLACED BATTERIES AT POSITIONS #1 AND #2.PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. WORK PERFORMED IAW: PHENOM 300 AMM 33-52-01. POSITION #SDR DXTA2023070390150Unknown · unknownFLAP: ON APPROACH RECEIVED A FLAP FAIL CAS MESSAGE. FLAP INDICATOR DISPLAYED FLAPS BETWEEN 3 AND FULL WHILE HANDLE WAS SELECTED TO FULL. COMPLETED CHECKLISTS INCLUDING CYCLING FLAPS 3 TIMES AND THEY DID NOT MOVE UP OR DOWN.//CORRECTIVE ACTION//DOWNLOADED CMC DSDR DXTA2023021080320Gcu · abnormalBATTERY OVERHEAT & TEMP INDICATION: BATTERY EXCEDENCE EICAS MESSAGE ILLUMINATED IN FLIGHT AT FL410. EMERGENCY CHECKLIST COMPLIED AND ELECTRICAL EMERGENCY BUTTON PUSHED. BOTH #1 BATTERY AND #1 GENERATOR WERE HIGH VOLTAGE. // SIGNOFF// REMOVED AND REPLACED LH GESDR DXTA2023010677940Gcu · faultedWITHIN 200' OF LEVELLING AT FL450, BATTERY EXEEDANCE YELLOW CAS. LATER IT EXTINGUISHED. SHORTLY AFTER IT WOULD COME ON & OFF & THEN REMAINED ON, HAD ALREADY BEGUN TO RUN QRH. DIVERTED TO KSTL. BATTERY VOLTAGE ON SCHEMATIC SHOWED 29 V & GEN 1 SHOWED 29.1. SDR DXTA2023010377600Bulb · inoperativeEMERG EXIT SIGN/LIGHT: MAIN DOOR EMERGENCY EXIT SIGN HAS ONE BULB INOP. ALSO, THE FORWARD ATTACH POINT IS LOOSE. THE SIGN STILL WORKS AND IS READABLE. REMOVED AND REPLACED NEW MAIN ENTRY DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL. WORK PERFORMED IAW PHENOM ASDR DXTA2022112374560Battery · abnormalEMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ILLUMINATED WITH EMER LT SWITCH IN ARM POSITION AND ELECTRICAL POWER APPLIED. LIGHTS APPEAR DIM. // SIGNOFF // POWERED UP AIRCRAFT AND VERIFIED DISCREPANCY, NOTED THAT EXIT SIGN ON MED DOOR AND EMERGENCY DOOR WAS DIM. MSDR DXTA2021091648890Warning Light · false activationDURING INITIAL MLG RETRACTION, CREW HEARD A WHINING NOISE FROM REAR OF ACFT & GOT A RED MLG DISAGREE CAS MESSAGE & 3 YELLOW CAS MESSAGES,: HYD PRESS LO, BRK FAIL, & PUSHER FAIL. NOTED ON SYS SYNOPTIC PAGE, HYD PRESS INDICATING 0. RAN MLG DISAGREE QRH & CAS SDR DXTA2020123004533Handle · brokenWHEN PRIME APPEARANCE WAS FINISHED WITH THERE SERVICE HUB EVENT THEY ATTEMPTED TO CLOSE THE MAIN ENTRY DOOR AND THE HANDLE BROKE OFF IN THEIR HAND. PRIME APPEARANCE CONTACTED ME AND I ADVISED GAMA. AIRCRAFT WAS QUICKLY REPOSITIONED INTO THE HANGAR AND GAMA TSDR 2020FA0000418Balance 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 (9 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PA
Reports on N309QS not matched to an aircraft · 12
They name N309QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2010031504029Engine · malfunctionedRT ENGINE IDLE SPEED AT 10,000 FEET AND 150KTS WAS 52.9 PERCENT. COMPLIED WITH ADJUSTMENT OF MINIMUM FLOW OF THE RT ENGINE FCU IN REF TO THE MM CH 71-00-00. ALL FINAL OPS CHECKS SATISFACTORY.SDR 2009FA0000778Indicator · reads lowAT TAKEOFF BOTH AIRSPEED INDICATORS SHOWED A YELLOW "IAS". THE CO-PILOT AIRSPEED SHOWED 40KTS SLOWER THAN THE LT SIDE AIRSPEED INDICATOR.SDR 2009FA0000775Indicator · reads highDURING INITIAL TAKEOFF ROLL, AIRSPEED INDICATIONS APPEARED NORMAL. AT 70KTS INDICATED F/O NOTED IAS CAPT SIDE + CAPT A/S JUMPED APPROX 30KTS TO APPROX 100KTS. WE CALLED ABORT - ABORT ON THE RUNWAY W/NO ISSUES.
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