HB-DIF - 1995 MOONEY M20M BRAVO




    Aircraft Summary


    General

    Year
    1995
    Manufacturer
    MOONEY
    Model
    M20M BRAVO
    Serial Number
    27-0026
    Registration #
    HB-DIF
    Condition
    Used
    FlightRules
    IFR
    Description
    Very nice private Mooney M20M TLS Bravo. Very well maintained and hangared.

    Airframe

    Total Time
    1688
    Complete Logs
    Yes
    Airframe Notes
    Private aircraft Always hangared since arrival in Switzrland Imported in Switherland in October 1995 with 719:54 Hours Maximum Take Off Weight: 1528 kg Empty Weight: Noise Level: 76.6 dB(A) According ICAO Annex 16, Vol. 1, Chapter 10 (10.4b) Light Hail Damage on Surfaces Leading Edges Specifications subject to verification by purchaser Aircraft subject to withdrawal from the market at any time and without notice

    Engine

    Engine Manufacturer
    LYCOMING
    Engine Model
    TIO-540-AF1B
    Engine Time
    1688
    Engine Time Since
    SNEW
    Engine TBO
    2000
    Year Engine Overhauled or Installed as New
    1995
    Turbocharged
    Yes
    Engine Notes
    Shock Load Inspection performed by Cermec Motor in 2010 at TT: 1090 hours, after propeller ground strike Magnetos, Propeller Governor, Overhauled and Vacuum Pump, Replaced at Shock Load Inspection

    Props

    Prop Manufacturer
    MT
    Prop Model
    MTV-14-B
    Prop Time
    598
    Prop Time Since
    SNEW
    Number of Blades
    4
    Blade Composition
    Composite
    Swept Blade Propellers
    Yes
    Prop Notes
    MTV-14-B/185-59b, 4 Bladed Composite with Electric De-Ice, Polished Spinner TT: 598 hours

    Modifications/Conversions

    Modifications/Conversions
    4 Bladed, Composite, Deiced MT-Propeller: MTV-14-B/185-59b EASA: EASA.A.S.01212 (issued Nov. 02, 2005) FAA: SA09689AC (issued Aug. 03, 2006) Advantages: Best vibration damping characteristics Bonded on stainless steel leading edge for best erosion protection of the blades Shorter take-off distance by approx. -8 % (SL, ISA conditions) Enhanced climb by approx. 2 % (SL, ISA conditions) Enhanced cruise performance by approx. 2 kts (MTOW, ISA conditions) Approx. 10 lbs less weight than the original propeller Significant inside and outside noise reductions Unlimited blade life FOD repairable blades Speed Brakes Standby Electric Vacuum Pump

    Avionics

    Avionics/Radios
    Bendix King KMA24 Audio Panel, Marker Beacon Bendix King KX165A COM-NAV 760 Channels 8.33 kHz Bendix King KX155 COM-NAV VHF COM 2 Ground Switch Intercom System Bendix King KCS55 Slaved Compass System with KI525A HSI Bendix King VOR/GS Indicator Garmin GPS155 coupled to HSI/Autopilot with MSI Avionics MSI-7-10334A Source Selector Panel Switch Bendix King KN62A DME Bendix King KR87 ADF Bendix King KFC150 Autopilot with KAS97B Altitude Preselect BF Goodrich WX1000+ Stormscope with Map Hoskins FT101A Digital Fuel Flow Indicator 406 MhZ ELT with Panel Mount Activation Switch Copilot Altimeter and Attitude Indicator Digital Clock

    Additional Equipment

    Oxygen System
    Yes
    Additional Equipment
    4 Bladed, Composite, Deiced MT-Propeller: MTV-14-B/185-59b EASA: EASA.A.S.01212 (issued Nov. 02, 2005) FAA: SA09689AC (issued Aug. 03, 2006) Advantages: Best vibration damping characteristics Bonded on stainless steel leading edge for best erosion protection of the blades Shorter take-off distance by approx. -8 % (SL, ISA conditions) Enhanced climb by approx. 2 % (SL, ISA conditions) Enhanced cruise performance by approx. 2 kts (MTOW, ISA conditions) Approx. 10 lbs less weight than the original propeller Significant inside and outside noise reductions Unlimited blade life FOD repairable blades Speed Brakes Standby Electric Vacuum Pump 2 Batteries (Standard Installation) 2 Alternators (Standard Installatio) External Power Receptacle Oxygen System

    Exterior

    Year Painted
    1995

    Interior

    Year Interior
    1995
    Number of Seats
    4
    Configuration
    Passenger
    Interior Notes
    Original Grey Fabric/Velour Seats with Grey Leather Headrests, in good condition Light Hail Damage on Surfaces Leading Edges

    Inspection Status

    Inspection Status
    Annual inspection to be completed in July 2025
    Airworthy
    Yes


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