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Aircraft record

N649DX2010 Embraer EMB-500

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply10 service difficulty reports

Registration
Valid
expires Aug 31, 2028
Based in
Dallas, TX
owner city / state
Owners
1
since 2021
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Asa Parts LLC
Owner type
LLC
City, state
Dallas, TX
Certificate issued
Aug 24, 2021
Expires
Aug 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Dec 21, 2010

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Embraer
Model
EMB-500
Year
2010
Serial number
50000194
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
2
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
A59CE
Mode S code
A8870B

Engine

Make and model
P&W Canada Pw617f-E
Type
Turbo-fan
Power
1,820 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2021 – nowAsa Parts LLCDallas, TX · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (4)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2021-24-21OperationsJan 25, 2022Airframe (EMB-500)Only with: EMB-500 with PW617F-E or PW617F1-E engines installed, or EMB-505 with PW535E engines installed.
2016-22-02Equipment/ FurnishingDec 1, 2016Airframe (EMB-500)Serial numbers per Embraer S.A. SB No. 500-25-0016 and SB No. 505-25-0020, dated December 8, 2015. Only with: Applies to passenger seats installed at manufacture; seats replaced during routine maintenance are not affected.
2014-15-51StabilizersAug 21, 2014Airframe (EMB-500)Certain serial numbers: EMB-500 50000218–50000333; EMB-500 50000336; EMB-500 50000337; EMB-500 50000339; EMB-500 50000341
2010-17-01Pratt & Whitney Canada Corp. PW617F-E Turbofan EnginesSep 27, 2010Engine (PW617F-E)Only with: Fuel/oil heat exchanger (FOHE) P/N 35C4540-01 installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (10)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Hydraulic power · powerpack · failedMar 31, 2020

    DURING 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, ALTHOUGH HE HAD TO BE TOWED OFF OF THE ACTIVE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · powerpack · failedSep 20, 2019

    PILOT 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.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · powerpack · failedJul 11, 2019

    PILOT 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 REPLACING THE HYDRAULIC POWER PACK. SUBSEQUENT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Hydraulic power · powerpack · failedJun 18, 2019

    PILOT 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 POWER PACK ASSEMBLY. SUBSEQUENT OPERATIONAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedApr 27, 2018

    PILOT 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 THE 4TH HYDRAULIC PUMP FAILURE IN THIS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedJun 12, 2017

    HYDRAULIC PUMP FAILED IN FLIGHT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · hydraulic system · low pressureApr 4, 2017

    LOW HYD CAS, HYDRAULIC PRESSURE DROPPED TO 800 PSI IN FLIGHT. HYDRAULIC POWER-PACK ASSEMBLY WAS FOUND TO BE FAILED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedNov 9, 2016

    WHILE 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 AND SPIKES TO 3800. ALSO DURING PRESSURE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · pitot tube · erodedMar 9, 2012

    DURING 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. THE DEBRIS WAS COLLECTED FROM THE INSIDE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · fuel filter · missingJul 9, 2011

    DURING 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 CONTINUED OPERATION WAS AUTHORIZED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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