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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