- Owner type
- Co-owned
- Serial number
- 50500452
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- March 14, 2018
- Certificate issued
- April 27, 2026
- Expires
- April 30, 2033
- Mode S code
- A4F347
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 N418QSMatched 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 N418QSMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025121206092Pressure Switch · defectiveFUEL 2 FEED FAULT, APPEARED WHEN CLIMBING THROUGH FL400. NO OTHER MESSAGES APPEARED. WHEN PULLING UP THE FUEL SCHEMATIC WE SAW THAT JET PUMP INDICATOR HAD A YELLOW X OVER IT AND WAS BEING FED BY THE ELECTRIC FUEL PUMP. REPLACED PRESSURE SWITCH. OPS CHECK GOODSDR DXTA2025102705426Battery · faultedWITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION THE CABIN EMERGENCY LIGHTING BLINKS ON AND OFF. REMOVED AND REPLACED FORWARD AND AFT BATTERIES WITH REPAIRED UNITS AND COMPILED WITH DEPLETE AND FULL CHARGE PROCEDURE IAW AMM 33-52-01, OPS CHECK GOODSDR DXTA2025072104275Wire · damagedDOOR PAX CAS ILLUMINATED THREE TIMES IN FLIGHT. FIRST FOR ABOUT 20 SECONDS EXTINGUISHED BEFORE LEVELING OFF AND BEING ABLE TO ACCOMPLISH QRH. ILLUMINATED 2 MORE TIMES FOR ABOUT 5 SECONDS. NO ILLUMINATION BELOW 15,000 FEET. CORRECTIVE ACTION: REPAIRED WIRE. OPSSDR DXTA2025050203299Flap System · malfunctionedFLAP FAIL YELLOW CAS: IN CRUISE FLIGHT AT FL 430 RECEIVED FLAP FAIL YELLOW CAS MESSAGE AS WELL AS SWPS FAULT AND PTRIM BKP FAIL CAS ASSOCIATES WITH FCE FAILURE. FLAP INDICATION HAD YELLOW X OVER IT AS WELL AS DID THE PITCH TRIM INDICATIONS. PITCH TRIM WORKED NSDR DXTA2025031702705Structure · no discrepancyDAMAGE INSPECTION: AIRCRAFT OVER SPEED CROSSING A LINE OF WEATHER AT FLIGHT LEVEL 450 DESCENDING TO FLIGHT LEVEL 430 WE ENCOUNTERED MODERATE TURBULENCE IN CLEAR AIR. AIRPLANE ACCELERATED RAPIDLY AND OVERSPEED APPROXIMATELY 10 KTS AND WE RECEIVED ONE HIGH-SPEEDSDR DXTA2024110401019Spring · brokenMAIN DOOR HANDLE: EXTERIOR MAIN ENTRANCE DOOR HANDLE DOES NOT STOW WHEN DOOR IS CLOSED AND LATCHED USING EITHER THE INTERIOR OR EXTERIOR HANDLE. CORRECTIVE ACTION; FOUND THAT THE SPRING INSIDE THE DOOR HANDLE TO BE BROKEN. REPLACED WITH A NEW SPRING. REATTACSDR DXTA2023121910374Battery Pack · faultedEMERGENCY LIGHTS BLINKING FOR THE LAST 35 MIN OF FLIGHT IN TO SDL. COMPLIED WITH FIM TASK 33-50-00-810-802-A. FOUND WITH ELECTRICAL CONNECTOR P1360 DISCONNECTED, EMERGENCY LIGHTS DO NOT COME ON IN ARM POSITION. PER FIM TASK, REPLACEMENT OF THE EMERGENCY LIGHT SDR DXTA2023100297050Unknown · defectiveAUTOPILOT SYSTEM: FLIGHT CONTROL ELECTRONIC FAILURE -FCE2 FAILURE TO INCLUDE GND SPLR FAIL, PTRIM NML FAIL, SPOILER FAULT //SIGNOFF// ARRIVED AT THE AIRCRAFT AND APPLIED POWER WITH A GPU REF EMBSOS AFM. TECHS NOTED NO ACTIVE FAULTS AT THIS TIME. PERFORMED OPERSDR DXTA2022053163030Battery Pack · defectiveCABIN EMERG LIGHT: CABIN EMERGANCY LIGHTING FLICKERED ON AND OFF, IN FLIGH. POWERED UP AIRCRAFT AND TURNED EMERGENCY LIGHTS ON, EMERGENCY LIGHTS BEGAN TO FUCKER, GAINED ACCESS TO THE FWD AND AFT EMERGENCY BATTERY PACKS, REMOVED THE FWD EMERGENCY BATTERY P/N: SDR DXTA2020112504395Module · leakingCLIMBING THROUGH FL260 ALL OF SUDDEN A VERY STRONG ELECTRICAL BURNING SMELL. FO CONFIRMED, AS WELL AS, THE PASSENGER. DECLARED EMERGENCY AND PERFORMED CHECKLIST. DIVERTED INTO LOCAL AIRPORT AND AS WE DESCENDED SMELL DISSIPATED. ON BASE TO FINAL AFTER GEAR SDR 2020FA0000405Balance 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 (6 EACH) AS FOLLOWS 5=83G,82G (MINIMUM 84G) AND HORN MASS WEIGHT PART
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