- Registered owner
- Asa Parts LLC
- Location
- Dallas, TX
- Owner type
- LLC
- Serial number
- 50000194
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- December 21, 2010
- Certificate issued
- August 24, 2021
- Expires
- August 31, 2028
- Mode S code
- A8870B
Embraer-Empresa Brasileira De EMB-500TCDS A59CEAirframe · Embraer-Empresa Brasileira De EMB-500TCDS E00080ENEngine · Pratt & Whitney Canada PW617F-E
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.
| 2009 | 2 |
|---|---|
| 2010 | 5 |
| 2011 | 2 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2022 | 1 |
| 2023 | 1 |
Airframe · Embraer-Empresa Brasileira De EMB-500
AD 2023-10-02Indicating/Recording System, NavigationAD 2021-24-21OperationsAD 2018-07-10Flight ControlsAD 2016-22-02Equipment/FurnishingAD 2014-15-51StabilizersEmergency ADAD 2011-17-15Flight ControlsAD 2011-01-04Wiring ElementsAD 2010-23-16PneumaticAD 2010-21-15Flight controlsAD 2010-15-09Ice and Rain ProtectionAD 2009-24-14Flight controlsAD 2009-05-06Flap systemEngine · Pratt & Whitney Canada PW617F-E
AD 2010-17-01Fuel Filter Bypass Valve poppetSuperseded and historical ADs · 1
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Embraer-Empresa Brasileira De EMB-500
SAIB AIR-21-04Hydraulic Power SystemNTSB investigations
No NTSB investigations matched to N649DXMatched 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-Empresa Brasileira De EMB-500 aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20200331003009ICruise/Level Flight · Birmingham, ALDuring cruise flight, the pilot noted that the gear had unlocked from the up and locked position and observed a hydraulic low pressure cas message. The pilot diverted to Birmingham international airport, kbhm, where he landed without further incident.Incident 20190227010579ILanding: Rollout · Kansas City, MOThe pilot reported that he received weather and runway reports prior to initiating his approach to runway 19 at kmkc. The runway conditions were reported as wet with deicing fluid. After touchdown, the pilot stated he applied the brakes normally, but noted no…
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR Q5QA2020040233104Powerpack · failedDURING CRUISE FLIGHT, THE PILOT NOTED THAT THE GEAR HAD UNLOCKED FROM THE UP AND LOCKED POSITION AND OBSERVED A HYDRAULIC LOW PRESSURE CAS MESSAGE. THE PILOT DIVERTED TO BIRMINGHAM INTERNATIONAL AIRPORT, KBHM, WHERE HE LANDED WITHOUT FURTHER INCIDENT, ALTHOUGSDR Q5QA2019092003Powerpack · failedPILOT POWERED UP THE AIRCRAFT AND IMMEDIATELY NOTED THE HYDRAULIC PUMP WAS CYCLING CONTINUOUSLY. PILOT PROCEEDED TO SHUT DOWN THE AIRCRAFT. CORRECTIVE ACTION INVOLVED INSTALLING AN OVERHAULED POWERPACK. OPERATIONAL CHECK WAS SATISFACTORY.SDR Q5QA2019071103Powerpack · failedPILOT REPORTED THE HYDRAULIC PUMP WAS RAPIDLY CYCLING WHILE IN CRUISE FLIGHT. PILOT EXTENDED THE LANDING GEAR NORMALLY AND HYDRAULIC OPERATION RETURNED TO NORMAL. PILOT LANDED AT HIS DESTINATION WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION INVOLVED REPLACINGSDR Q5QA2019061802Powerpack · failedPILOT EXPERIENCED THE HYDRAULIC PUMP CYCLING CONTINUOUSLY TO HOLD PRESSURE, FOLLOWED BY PARTIAL GEAR EXTENSION. THE PILOT EXTENDED THE LANDING GEAR USING EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. CORRECTION ACTION INVOLVED REPLACING THE HYDRAULIC POWSDR Q5QA2018043000001Pump · failedPILOT EXPERIENCED A TOTAL HYDRAULIC FAILURE. WITHOUT HYDRAULIC PRESSURE, THE LANDING GEAR FELL OUT AND CYCLED TO DOWN AND LOCKED. THE PILOT DIVERTED AND LANDED WITHOUT INCIDENT UTILIZING EMERGENCY BRAKES. REPLACED THE HYDRAULIC PUMP ASSEMBLY. THIS IS THESDR Q5QA20170612010Pump · failedHYDRAULIC PUMP FAILED IN FLIGHT.SDR Q5QA20170404009Hydraulic System · low pressureLOW HYD CAS, HYDRAULIC PRESSURE DROPPED TO 800 PSI IN FLIGHT. HYDRAULIC POWER-PACK ASSEMBLY WAS FOUND TO BE FAILED.SDR Q5QA20161115006Pump · failedWHILE CRUISING AT 22,000 FT, PILOT EXPERIENCED HYD AUTO PRESSURE FLUCTUATION BETWEEN 1600/3200. HYD ON, PRESSURE FLUCTUATIONS AND SPIKES TO 3800. HYD OFF, PRESS 0 AND LANDING GEAR FALLS OUT. PILOT LANDED WITH HYD PRESSURE ON AND SEEING PRESSURE FLUCTUATIONS ANSDR 2012FA0000145Pitot Tube · erodedDURING A POST FLIGHT INSPECTION, DISCOVERED PLATING MATERIAL ON THE INLET LIP SURFACE WAS SEPARATING FROM THE LIP AND HAD FLARED BACKWARDS INTO THE THROAT OF THE PITOT TUBE. THE PITOT TUBE WAS REMOVED FROM THE ACFT AND THE PITOT LINE WAS CLEARED OF DEBRIS. TSDR 2011FA0000460Fuel Filter · missingDURING THE FIRST SCHEDULED INSP (600HR/12 MONTH) THE RT ENGINE FUEL FILTER WAS FOUND TO HAVE NEVER BEEN INSTALLED AT THE FACTORY. THE MFG WAS NOTIFIED AND THEY REQUESTED AN ENGINE HOT SECTION BOROSCOPE INSP BE PERFORMED. NO ENGINE DISTRESS WAS OBSERVED AND CO
STCs that may be installed · 26
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.