- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500175
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 22, 2013
- Certificate issued
- August 20, 2026
- Expires
- August 31, 2033
- Mode S code
- A38D77
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 N328QSMatched 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 N328QSMatched 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
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026092109742Relief Valve · defectiveDURING CRUISE RECEIVED AN EMER BRK LOW PRESSURE CAS. PRESSURE WAS APPROXIMATLEY 150PSI AND CONTINUED TO DROP. SOMETIME BETWEEN TOUCHDOWN AND ENGINE SHUTDOWN PRESSURE CAME BACK UP TO 2900 THEN DROPPED TO 2400PSI WITHIN 10 MINUTES. TWO MORNINGS IN A ROW AIRCRAFTSDR DXTA2025092405053Battery · faultedDURING FLIGHT ALL INTERIOR EMER LIGHTS ILLUMINATED. EMER LIGHT SWITCH IN ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY LIGHT BATTERIES WITH CUSTOMER SUPPLIED PART IAW EMBRAER PHENOM 300 AMM CHAPTER 33-52-01/400. PERFORMED FUNCTIOAL AND OPERATIONASDR DXTA2024090900454Light · detachedCABIN EMERG LIGHT: EMER AISLE LIGHT BETWEEN SEATS 1 AND 2 IS NOT MOUNTED PROPERLY CORRECTIVE ACTION: REINSTALLED EMERGENCY AISLE LIGHT BETWEEN SEATS 1 AND 2. OPS CHECK OK IAW EMB PHENOM 300 AMM 33-52-11.SDR DXTA2023080492240Unknown · unknownCABIN EMERG LIGHT: DURING BEFORE START FLOW AFTER ARMING EMG LIGHTS THEY REMAINED EMG LT NOT ARM. TRIED CHARGING THEM FOR 20MINS WITH GPU BUT DID NOT HELP. PERFORMED PHENOM 300 FIM TASK 33-50-00-810-801-A. FOUND #2 EMERGENCY BATTERY HAS FAILED. REMOVED #2 EMSDR DXTA2023062689470Battery Pack · defectiveCABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLASH WHILE IN FLIGHT. TURNING SWITCH TO OFF TURNS THEM OFF BUT WHENEVET THE SWITCH IS IN THE ARM POSITION THEY FLASH. REMOVED FAULTY #1 EMERGENCY BATTERY & INSTALLED MODIFIED EMERGENCY BATTERY IAW MM 33-52-01. PERFORMSDR DXTA2023062689550Unknown · unknownEMERGENCY LIGHTS FLASH WHILE IN FLT. TURNING SWITCH TO OFF TURNS THEM OFF BUT WHEN EVER THE SWITCH IS IN THE ARM POSITION THEY FLASH. REMOVED FAULTY #1 EMERGENCY BATTERY AND INSTALLED MODIFIED EMERGENCY BATTERY IAW MM 33-52-01. PERFORMED OPS TEST OF THE EMERGSDR DXTA2023020980180Pressure Switch · defectiveBRK FAIL YELLOW CAS: WHITE HYD SYS FAULT ADVISORY POSTED DURING CLIMB APPROXIMATELY 12000', FOLLOWED BY BRK FAIL YELLOW CAS APPROXIMATELY 15 MINUTES LATER. COMPLIED WITH QRH PROCEDURES. UPON EXTENSION LANDING GEAR DEPLOYED NORMALLY AT A SLOWER THAN NORMAL RASDR DXTA2021081646890Battery · defectiveCABIN EMERG LIGHT: IN FLIGHT EMER LT NOT ARM YELLOW CAS MESSAGE CAME ON INTERMITTANTLY. EMERGENCY LIGHTING CAME AND STAYED ON WITH THE SWITCH IN ARM. // SIGNOFF // CW FIM (4885) » 33 LIGHTS» FIM-4885 - 33-50-00-810-801-A. EMERGENCY LIGHTS INADVERTENTLY OPERATSDR 2021F00025Balance 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 NUMBERPE915109-L33 (9 EACH BELOW MINIMUM OF 84G). LEFT ELEVATOR HORN WSDR 2021F00020Battery Pack · no testTHE COCKPIT LOCATION EMERGENCY LIGHTS BATTERY FAILED SCHEDULED FUNCTIONAL TEST. BATTERY ASSEMBLY WAS REPLACED WITH A REPAIRED BATTERY AND NO FURTHER DEFECTS WERE NOTED. THIS REPORT COMPLIES WITH 14CFR PART 135 OPERATOR'S GMM REQUIREMENTS.SDR DXTA2019091102836Warning System · false activationFLAP FAIL YELLOW CAS ILLUMINATED - IN CRUISE AT FL410 CREW RECEIVED THE FOLLOWING CAS MESSAGES (ALL CONSISTENT WITH FCE 1 FAIL): YELLOW SWPS FAULT, FLAP FAIL, AND PTRIM BKP FAIL, AS WELL AS WHITE SPOILER FAULT MESSAGE. CREW RAN APPROPRIATE QRH CHECKLISTS ANDSDR DXTA2015092206089Engine · odorRETURNING TO THE GATE, ODOR IN CABIN DURING TAXI. R & R THE NR 1 ENGINE IAW AMM 71-00-00-400-801-A & 71-00-00-400-802-A. PERFORMED 5 POINT CALIBRATION RUN ON THE NR 1 ENGINE, NO DISCREPANCIES NOTED. ALL WORK WAS PERFORMED IAW MM 72-00-00.SDR DXTA2014043005749Unknown · odorFROM INITIAL APPLICATION OF TAKEOFF POWER TO 20,000 FT THERE WAS A STRONG ODOR LIKE HOT OIL OR JET FUEL IN THE CABIN. PERFORMED GROUND RUN TO DUPLICATE FAULT, NO DEFECT NOTED. INSPECTED ACFT FOR FUEL LEAKS, NONE NOTED. INSPECTED ENGINES FOR FUEL LEAKS, NONE SDR DXTA2014042905746Unknown · odorDURING INITIAL CLIMB, NOTICED A STRONG ODOR LIKE HOT DUCT THAT DID NOT DIMINISH DURING THE CLIMB OUT. SELECTING ECS 1, THEN ECS 2 DID NOT CHANGE THE ODOR. RETARDING TO CRUISE POWER INITIALLY DIMINISHED THE ODOR, BUT IT CAME BACK AS THE ENGINES STABILIZED AT
Reports on N328QS not matched to an aircraft · 14
They name N328QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2010102804278Power Supply · inoperativeAFTER ROTATION, SEC FLT DISPLAY C/B POPPED, WITH ASSOCIATED STANDBY GYRO AMBER LIGHT ILLUMINATION. R & R STANDBY GYRO POWER SUPPLY IAW MM 34-21-14. OPS CHECKED GOOD.SDR DXTA2010050604086Brake Assy · malfunctionedWHEN EQUAL BRAKE PRESSURE IS APPLIED TO BOTH BRAKES, AIRCRAFT JERKS TO THE LT. LT BRAKE IS GRABBY AND SENSITIVE. RT BRAKE FEELS LESS EFFECTIVE. R & R RT MAIN BRAKE ASSY IAW MM CH 32-42-01. OPS AND LEAK CHECKS GOOD.SDR DXTA2010031004024Brake Sys · sensitivityLT BRAKE PEDAL VERY SENSITIVE. RT BRAKE PEDAL ALMOST TO FLOOR TO ACHIEVE SAME BRAKING ACTION. THIS HAPPENS FROM BOTH SIDES. BLED THE BRAKES IAW MM 32-42-00. OPS & LEAK CKS GOOD.
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