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    1972 ROBIN HR100/200B1972 ROBIN HR100/200B
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    1972 ROBIN HR100/200B

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    Aircraft Summary

    General
    Year
    1972
    Manufacturer
    ROBIN
    Model
    HR100/200B
    Condition
    Used
    Based at
    LSZL
    Description
    Robin HR100-200B
All Metal Airframe, Fixed Gear
5 seats
Sliding roof and rear trunk
463.2 kg Payload!
Fuel capacity 400 liters
Maximum take-off weight: 1200 kg
Empty weight: 736,80
Cruising speed 75% at 8000 feet: 264 Km/h Range, 75% at 5500 feet: 2550 km
New Lycoming 200 hp engine
Total engine and propeller 65 hours
    Airframe
    Total Time
    1700
    Range
    1,240 NM
    Max Takeoff Weight
    2,645.55 lb
    Basic Empty Weight
    1,609.37 lb
    Fuel Capacity Volume
    102.5 gal
    Auxiliary Fuel Tank
    Yes
    Complete Logs
    Yes
    Engine
    Engine Manufacturer
    LYCOMING
    Engine Serial Number
    New engine Lycoming IO-360-A1D6
    Engine Horsepower
    200 HP
    Engine Time
    65
    Engine Time Since
    SOH
    Engine TBO
    2000
    Year Engine Overhauled or Installed as New
    2021
    Engine Time Remaining To Overhaul
    1940
    Engine Notes
     New engine Lycoming IO-360-A1D6 200 HP and propeller total time after overhaul 2021 65 hours.


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