- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500289
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- August 19, 2015
- Certificate issued
- November 14, 2025
- Expires
- November 30, 2032
- Mode S code
- A44416
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 N374QSMatched 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 N374QSMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026100509949Control Module · faultedGOT A BRK FAIL CAS MESSAGE WHILE TAXIING OUT. HAD TO APPLY MAX PEDAL PRESSURE TO GET ANY BRAKES AT ALL AND IT SEEMED AS IF THE LEFT BRAKE WOULD GRAB WHEN I FINALLY GOT ANY BRAKES. R & R RT WHEEL SPEED XDUCER IAW AMM 32-41-06. OPS CHKD GOOD. PERFORMED PEDALSDR DXTA2026012006593Battery Pack · faultedEMER LIGHT NOT ARM CAS ON WITH SWITCH IN ARM, ENGINES RUNNING AND NO GPU. GROUND RESET PROCEDURE UNSUCCESFUL. REVIEWED SL505-33-0005 REV 5 "EMER LIGHT T/S" AND FOUND THAT BOTH BATTERY PACKS ARE CAUSING THE ISSUE CONFIRMED 'G' SWITCH NOT TRIPPED. REMOVED FWD ESDR DXTA2025120505944Pressure Switch · faultedPASSING FL215 "FUEL 1 FEED FAULT" WHITE CAS DISPLAYED. ON FUEL SYNOPTIC PAGE, DISPLAYED AMBER X OVER EJECTOR PUMP 1. REMOVED AND REPLACED LEFT FAULTY PRESSURE SWITCH & REPLACED WITH NEW UNIT. REMOVED AND REPLACED RT FAULTY PRESSURE SWITCH & REPLACED WITH NEWSDR 2025FA0000772Skin · corrodedCORROSION FOUND ON TOP OF BOTH WINGS FWD OF SPEED BRAKESSDR DXTA2025092905113Light · brokenTHE WHITE EMER LIGHT LOCATED IN THE LAV AREA BELOW THE TOILET IS INOP WHEN TESTING THE EMERGENCY LIGHTS CORRECTIVE ACTION: TECHS FOUND THE EMERGENCY LIGHTING ASSY BROKEN. TECHS REMOVED THE DAMAGED UNIT ANDINSTALLED AN OPERATOR SUPPLIED EMERGEMCY LIGHTING ASSY SDR DXTA2025021802406Door · out of alignmentMAIN DOOR: DOOR MISALIGNED AND WILL NOT CLOSE. TOP RIGHT PIN IS NOT SEATING FOUND MED TOP TRIM PEICE GETING HUNG UP ON THE DOOR CAUSING IT TO NOT CLOSE ALL THE WAY PRIOR TO CLOSING THE HANDLE. ADJUSTED TRIM PEICE AS NEEDED SO THE DOOR OPENS AND CLOSES SMOOTHLYSDR DXTA2025021202290Door · out of adjustMAIN DOOR: MAIN CABIN DOOR WILL NOT CLOSE. THE DOOR IS MISALIGNED WITH AN INCH GAP. FROM THE OUTSIDE THE DOOR SEAL IS PINCHED. SEE PICSDR DXTA2024051011733Control Panel · faultedAFTER POWERING DOWN THE AIRCRAFT WITH THE EMER LIGHT SWITCH IN THE OFF POSITION THE EMERGENCY LIGHTS REMAINED ON. AFTER CYCLING THE SWITCH WE WERE ABLE TO GET THE EMERGENCY LIGHTS TO EXTINGUISH. BATTERIES WERE OFF AND NO GPU WAS CONNECTED. BATTERIES HAVE BEENSDR DXTA2024042911640Battery · failedALL CABIN EMERGENCY LIGHTS ILLUMINATE AND REMAIN ON WITH THE EMER LT SWITCH IN THE ARM POSITION. REMOVED FAULTY EMERGENCY BATTERY. REF. AMM 33-52-01. REPLACED FAULTY. REF AMM 33-52-01. NO DEFECTS NOTED.SDR DXTA2024040511409Valve · failedSTARTED ENGS TO DEPART & ACFT BEGAN ROLLING WITH PARKING BRAKE SET & GOOD PRESSURE IN EM BRK ACCUMULATOR. REGULAR BRAKES WORKED, BUT EM BRAKE DID NOT. RESET EM BRAKE- NO CHANGE. NO BRAKE FAIL OR ANY OTHER CAS MESSAGES. VERIFIED SQUAWK NOT GETTING ANY BREASDR DXTA2023032883310Unknown · unknownEMERGENCY LIGHTS FLICKER INFLIGHT AND REMAIN ON WITH THE SWITCH SET TO ARM. R/R FWD AND AFT EMERGENCY LIGHT BATTERY PACKS IAW PHENOM 300 AMM 33-52-01. OPS CHECK OK.SDR 2020FA0000389Balance Weight · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING LEFT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE: PART NUMBER PE915109-L33 (4 EACH) UNDER THE WEIGHT LIMITS AS FOLLOWS (4=82 GRAMS), AS PRESCRIBSDR DXTA2018093001482Not Reported · malfunctionedWITH THE AIRCRAFT POWERED WITH A GPU, WE RECEIVED AN OVERVOLTAGE OF 30V AND THE GPU AUTOMATICALLY DISCONNECTED. AT THE SAME TIME A STRONG ACRID, BURNING, ELECTRICAL SCENT WAS SMELLED IN THE COCKPIT. THERE WERE NO UNUSUAL CAS MESSAGES DISPLAYED NOR POPPED CIRCUSDR DXTA2016030806195Control Module · failedON LANDING ROLL OUT, WHEN BRAKING APPLIED TO DECELERATE, BRAKE FAIL MSG ILLUMINATED ON CAS. ZERO BRAKING ACHIEVED USING NORMAL BRAKES. EMERGENCY BRAKE SYS USED. BOTH MLG TIRES FAILED. REMOVED LT & RT WHEEL & TIRE ASSEMBLY. INSTALLED REPAIRED LT & RT WHEEL
Reports on N374QS not matched to an aircraft · 9
They name N374QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200802960Trim Tab · obstructedJAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF MM 27-31-00.SDR DXTA20082960Sprocket · obstructedJAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF. CE560 M/M 27-31-00.SDR DXTA200802753Wire · damagedON INITIAL CLIMB OUT LANDING GEAR HANDLE WOULD NOT MOVE. REPLACED 5 EA WIRE SPLICES AT LT MAIN GEAR SQUAT SWITCH, REPACKED LT MAIN GEAR STRUT, SERVICED STRUT, IAW 560 MM 32-11-02, 32-61-00, 32-42-01, 12-14-01 PERFORMED GEAR SWING, OPS CHECKED GOOD, IAW 560 M
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