Register
    1998 EMBRAER EMB-145EP N-NUMBER N802HK1998 EMBRAER EMB-145EP N-NUMBER N802HK
    Photos(14)
    N802HK - 1998 EMBRAER EMB 145EP

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    Aircraft Summary

    General
    Year
    1998
    Manufacturer
    EMBRAER
    Model
    EMB-145EP
    Serial Number
    145066
    Registration #
    N802HK
    Condition
    Used
    Description
    •	50 Passenger
•	Forward Galley
•	Rear Lavatory
    Airframe
    Total Time
    37744.9
    Total Landings
    34938
    Engine Program
    Engine Maintenance Program
    None
    Engine 1
    Engine 1 Manufacturer
    ROLLS ROYCE
    Engine 1 Model
    AE3007A1/1
    Engine 1 Serial Number
    CAE-310131
    Engine 1 Time
    36710.9
    Engine 1 Time Since
    SNEW
    Engine 1 TBO
    4500
    Engine 1 Cycles
    34538
    Engine 2
    Engine 2 Manufacturer
    ROLLS ROYCE
    Engine 2 Model
    AE3007A1/1
    Engine 2 Serial Number
    CAE-312594
    Engine 2 Time
    23854.9
    Engine 2 Time Since
    SNEW
    Engine 2 TBO
    4500
    Engine 2 Cycles
    22216
    Auxiliary Power Unit
    APU Notes
    T-62T-40C14 - Not Installed. In Storage
    Avionics
    Avionics/Radios
    • Avionics Package: Honeywell Primus 1000
• ADF: Dual Honeywell Primus II
• Autopilot: Honeywell IFCS (CAT I & CAT II)
• Comms: Dual Honeywell Primus II w/8.33 kHz
• CVR: Honeywell SSCVR
• DME: Dual Honeywell Primus II
• EFIS: Honeywell 5-tube 7X-inch
• FDR: Honeywell SSFDR (88 parameters)
• Flight Director: Dual Honeywell IFCS (CAT I & CAT II)
• Flight Phone: AEROCOM 1000
• FMS & GPS: Dual Honeywell
• Hi Frequency: Dual w/SELCAL
• IRS: Dual
• Navigation Radios: Dual Honeywell Primus II
• Radar Altimeter: Yes
• SATCOM: AirCell Iridium ST-3100 w/dual handsets
• TAWS: EGPWS w/windshear & escape guidance
• TCAS: Honeywell TCAS-II w/change 7.1
• Transponder: Dual Honeywell Mode S w/diversity
• Weather Radar: Yes w/dual control panels & turbulence detection
    Additional Equipment
    Additional Equipment
    • Dual radio management units
• Aural warning unit
• ISIS, ADS-B Out, ELT, EICAS
• Auxiliary flight data acquisitions unit
• Dual stall protection systems
• Central maintenance computer
• Dual digital clocks
• Dual air data computers
• Automatic environmental control system
• Dual integrated computers
• Airborne audio system
• Cabin interphone system
    Interior
    Number of Seats
    50


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