N312LL - 1969 THORP T18


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    Aircraft Summary


    General

    Year
    1969
    Manufacturer
    THORP
    Model
    T18
    Registration #
    N312LL
    Serial Number
    194
    Condition
    Used
    Total Time
    1110.0
    Description
    Price just reduced! Lycoming O-320 B2B with hollow crank 160hp, 868 Smoh, Sensenich wood Prop, "T" panel minimum IFR. Dual VHF and VOR. Moving map GPS. Autopilot. Always hangared

    Airframe

    Airframe Notes
    1110 Hours Total Time

    Engine

    Engine Notes
    Lycoming O-320 B2B with hollow crank 160hp 868 Hours Since Overhaul

    Props

    Prop Notes
    Sensenich wood Propeller "T" panel minimum IFR. Dual VHF and VOR. Moving map GPS. Interior and landing lights. Audio panel with intercom. Autopilot. Always hangared. Two Seat Aerobatic, Interior and landing lights. The T-18 design was originally developed with the Lycoming 0-290G (ground auxiliary power unit) in mind, by John Thorp. Which was easily converted to a Lycoming 0-290D engine producing 125 HP. The T-18 is an all metal 2 place side-by-side high performance aircraft. Control response is exceptional and control forces are well harmonized. The T-18 is a very capable cross-country airplane. It will carry 2 people, 80 lbs. of baggage, and depending on engine and prop, can cruise around 180 mph. Powerplants range from Lycoming O-235 (115hp) to IO-360 (180). The T-18 was designed to be built from twelve 4' x 12' sheets of aluminium ranging in thickness from 0.016 to 0.040. Ribs and fuselage frames were designed to be hand formed with a mallet over plywood form blocks. Simple aluminium angle extrusions are used for stringers and longerons. The main wing spar caps are made from 1/4 "U" channel on top and angle on bottom with flat sheet for spar webs. John Thorp designed the aircraft to be small, yet strong with excellent take-off and climb performance. The landing gear is a simple "A" frame of heavy wall 4130 steel tubing, heat treated to 180,000 lbs./sq. in. and bolted to the firewall with (3) 3/8" bolts. The engine mount is also attached to the "A" frame allowing landing stresses not to be transmitted directly to the fuselage. This landing gear system has proven to be rugged and durable. The T-18 incorporates the "flying tail" which John Thorp held the patent for. This design also incorporates a sliding bubble canopy, like a fighter style.

    Inspection Status

    Inspection Status
    AVAILABLE IMMEDIATELY, CONTACT ERIC ECKARDT Specifications and/or descriptions are provided as introductory information. They do not constitute representations or warranties of Flight Source International, Inc. Accordingly, you should rely on your own inspection of the aircraft.


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