N55000 - 2003 MAULE M7 260C


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    Aircraft Summary


    General

    Year
    2003
    Manufacturer
    MAULE
    Model
    M7-260C
    Serial Number
    30031C
    Registration #
    N55000
    Condition
    Used
    Description
    Complete Log Books, Always Hangered This aircraft is in Very Good condition - Always Hangared / impeccably maintained

    Airframe

    Total Time
    1195
    Airframe Notes
    Total Time: 1195 TTSN

    Engine

    Engine Manufacturer
    LYCOMING
    Engine Model
    IO-540
    Engine Horsepower
    260 HP
    Engine Time
    285
    Engine Time Since
    SMOH
    Engine TBO
    2000
    Engine Notes
    Lycoming IO-540 – 260 HP – 2000 TBO - Crankshaft AD C/W

    Props

    Prop Notes
    285 TTSN

    Avionics

    Avionics/Radios
    Garmin 650 Garmin G5’s – (Two) Garmin 345 ADS-B Transponder Garmin Com – Flip Flop Garmin 340A Audio Panel JPI Engine Analyzer 460 ELT

    Additional Equipment

    Additional Equipment
    85 Gallon - Long Range Fuel Patroller Door Package – Pilot / Co-Pilot Vortex Generators Gami Injectors Fifth Seat Rosen Sun Visor System – STC’d Factory Sun Roof Alaskan Airframes – Baby Bushwheel Tailwheel

    Exterior

    Exterior Notes
    9/10 Original Paint – Red & White

    Interior

    Interior Notes
    8/10 Original Interior – Grey Material: Vinyl w/Fabric Inserts Has the Fifth Seat!

    Inspection Status

    Inspection Status
    Annual: Next Due January 2024 Damage History - 2015 - forced landing with airframe damage, flipped on its back – tail rebuilt / top of wings reskinned - airframe repaired locally. Wings and Fabric repainted after repairs. Engine majored locally after accident / installed new propeller & spinner - 285 hours flight time since repairs. Call for log copies of repairs. Specifications: Landing Gear Configuration: Taildragger Landing Gear Type: Spring Aluminum or Oleo Strut Gear Engine Type: Lycoming IO-540-V4A5 Engine Model: (see above) (fuel injected) Propeller: McCauley Constant Speed Prop - 3 blade No. of Seats: Five Useful Load: (avg.) 829 lbs. (260C) Cruising Speed: (75% power at optimum altitude): 164 mph Wing Span: 32.9 feet Wing Area: 165.6 sq. feet. Length: 23.5 feet Height: 8.3 feet Cabin Width: 42 inches Gross Weight: 2500 lbs. Empty Weight: 1610 lbs. (260) 1671 (260C) Fuel Capacity: 85 gal. Stall speed (with full flaps, 1 pilot, 1/2 tank of fuel) 40 mph Takeoff distance: (1 pilot, 1/2 tank of fuel) 250 feet Takeoff distance at gross over 50’ high obstacle: 600 feet Rate of Climb: (1 pilot, 1/2 tank of fuel) 1650 fpm Land at gross over 50’ obstacle: 500 feet Best Climb Speed: 90 mph Service Ceiling: 20,000 feet Fuel Consumption (65% power): 15 gph Flap Settings: -7, 0, 24, Specifications, performance, equipment, STC’d equipment, included STC’d equipment, component times, damage history and condition subject to verification upon inspection


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