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    General Specs

    • For Sale
    • 1986
    • Not Listed
    • Not Listed
    • San Luis Obispo, CA USA


    Call for Price

    Epsilon TB-30 LLC

    • (805) 594-0726
    • Wayne Fulton

      903 Airport Drive #2

      San Luis Obispo, CA 93401 USA

    Show Additional Aircraft From This Seller

    Call for Price

    General Specs (cont.)




    Additional Classifications

    Detailed Description

    1986 Socata Epsilon TB-30. 208 kt cruise/281 kt VNE French Air Force primary trainer. 300 HP Lyc. AEIO 540 w/ 870 SMOH, Hartzell CS prop. 3498 TTAF Aerobatic, tandem seat, retractable gear w/ inverted systems and fully complimented dual inst. panels. Released from military 2017. Certification in Experimental Exhibition category. Call for quote.

    Avionics / Equipment

    Dual Annunciator Panels 
    Individually Switched Taxi and Landing Lights
    Dual RMI’s 
    2 Electric Artificial Horizons 
    Stall Warning System Audio patched into Audio Panel
    Emergency Backup Battery for #1 Horizon 
    DuAl Audio Panels w/Intercom 
    Gear Warning System Audio
    3 Light Marker Beacon
    UV Panel Lighting
    Nicad Battery 
    Battery Overtemp Warning System
    Baggage Compartment
    Dual G Meters 
    Cleveland Wheels and Brakes
    Recording Electronic Accelerometer 
    Inverted Fuel & Oil System
    Dual Vibrating Altimeters 
    U.S. APU Plug
    Dual Fuel Flow Indicators 
    Pitot Heat
    Dual OAT Indicators 
    Canopy Alert System
    Dual Voltmeters 
    Alternate Static Source
    Dual Clocks 
    Canopy Jettison System
    Dual EGT Indicators
    Dual CHT Indicators
    Dual VSI’s
    Dual Airspeed Indicators
    Electric Flaps
    Electric/Hydraulic Actuated Landing Gear
    Emergency Gear Extension System
    Seat Height Adjustable
    Rudder Pedal Depth Adjustable
    3 Strobes (Linked, wingtips & tail)


    The Epsilon is a tandem seat, retractable tri-gear, all metal, western technology production aircraft manufactured by Socata (Group Aerospatiale) in France.
    Max Level Speed 208 kts. 
    Engine - 300 HP Lycoming AEI0 540L
    VNE 281 kts. 
    Propeller-Hartzell constant speed 78"
    Stall speed 63 kts. 
    Gross Weight 2,755 Ibs.
    G Limits + 6.75G/-3.35G 
    Empty Weight 2,046 Ibs.
    Inverted Flight Duration 2 minutes 
    Fuel (useable) 55.4 gallons
    Wing span 26' Length 24.9' Height 8.6'