説明
Very nice private Mooney M20M TLS Bravo.
Very well maintained and hangared.仕様
年式1995
メーカーMOONEY
モデルM20M BRAVO
シリアル番号27-0026
Registration #HB-DIF
状態中古
FlightRulesIFR
Total Time1,688
Complete Logsはい
AirframePrivate 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 1 Make/ModelLYCOMING TIO-540-AF1B
Engine 1 Time1,688 SNEW
Engine TBO2000
Year Engine Overhauled or Installed as New1995
Turbochargedはい
Engine(s)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
Prop ManufacturerMT
Prop ModelMTV-14-B
Prop Time598 SNEW
ブレード数4
Blade CompositionComposite
Swept Blade Propellersはい
Prop SpecsMTV-14-B/185-59b, 4 Bladed Composite with Electric De-Ice, Polished Spinner
TT: 598 hours
Modifications/Conversions4 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/RadiosBendix 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
Oxygen Systemはい
Additional Equipment4 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
Year Painted1995
Year Interior1995
Number of Seats4
ConfigurationPassenger
InteriorOriginal Grey Fabric/Velour Seats with Grey Leather Headrests, in good condition
Light Hail Damage on Surfaces Leading Edges
Inspection StatusAnnual inspection to be completed in July 2025
Airworthyはい
年式1995|
メーカーMOONEY|
モデルM20M BRAVO|
シリアル番号27-0026|
Registration #HB-DIF|
状態中古|
FlightRulesIFR|
Total Time1,688|
Complete Logsはい|
AirframePrivate 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 1 Make/ModelLYCOMING TIO-540-AF1B |
Engine 1 Time1,688 SNEW |
Engine TBO2000|
Year Engine Overhauled or Installed as New1995|
Turbochargedはい|
Engine(s)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|
Prop ManufacturerMT|
Prop ModelMTV-14-B|
Prop Time598 SNEW |
ブレード数4|
Blade CompositionComposite|
Swept Blade Propellersはい|
Prop SpecsMTV-14-B/185-59b, 4 Bladed Composite with Electric De-Ice, Polished Spinner
TT: 598 hours|
Modifications/Conversions4 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/RadiosBendix 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|
Oxygen Systemはい|
Additional Equipment4 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|
Year Painted1995|
Year Interior1995|
Number of Seats4|
ConfigurationPassenger|
InteriorOriginal Grey Fabric/Velour Seats with Grey Leather Headrests, in good condition
Light Hail Damage on Surfaces Leading Edges|
Inspection StatusAnnual inspection to be completed in July 2025|
Airworthyはい|