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    1967 SOCATA RALLYE1967 SOCATA RALLYE
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    1967 SOCATA RALLYE

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    Aircraft Summary

    General
    Year
    1967
    Manufacturer
    SOCATA
    Model
    RALLYE
    Condition
    Used
    Description
    MTOW 1 050 kg
Empty Weight  606,3 kg
Useful Load  443,7 kg
    Airframe
    Total Time
    5359
    Airframe Notes
    Socata Rallye MS893A, low-wing, 4 seat, capable of STOL (short takeoff and landing) performance. is equipped with a cantilever wing, which incorporated interconnected full-span automatic leading edge slats, wide-chord slotted ailerons, and wide-span Fowler-type trailing edge flaps. The aircraft is towing equipped for glider tugs or banner bearers. Good technical status with all required SB and ADs complied until last 100-hrs inspection 2018-07-27. When Airworthy on CAMO and operated on SPO. DH 1970-12-22. Original Exterior and Interior 5/10. It is a project or buy it as a spare part airplane.
    Engine
    Engine Manufacturer
    LYCOMING
    Engine Model
    O-360-A2A
    Engine Time
    1772
    Engine Time Since
    SOH
    Engine TBO
    2000
    Props
    Prop Notes
    Sensenich 76E M8-056 s/n 10529-K, OH 2016-06-24 TSO:  1 997 hrs TBO:  2 000 hrs
    Avionics
    Avionics/Radios
    Gyropanel
Becker Com
King KT76A Transponder
AK350 Encoder
    Additional Equipment
    Additional Equipment
    Towing equipped
ELT (U/S)
Fire Extinguisher
First Aid Kit


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