£114,458
Posizione dell' Aereomobile:Locarno, Ti, Svizzera
Informazioni sul venditore
Visualizza le informazioni sul venditoreGenerale
Anno
1995
Produttore
Modello
Numero di serie
27-0026
Registrazione #
HB-DIF
Condizione
Usati
Normative di volo
IFR
Descrizione
Very nice private Mooney M20M TLS Bravo.
Very well maintained and hangared.
Struttura velivolo
Tempo totale
1,688
Complete Logs
Si
Fusoliera
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
Motore
Engine 1 Make/Model
LYCOMING TIO-540-AF1B
Engine 1 Time
1,688 SNEW
Engine TBO
2000
Anno del motore revisionato o installato come nuovo
1995
Turbocompressore
Si
Motore/i
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
Stima
Prop Manufacturer
MT
Prop Model
MTV-14-B
Prop Tempo di revisione
598 SNEW
Numero di lame
4
Composizione della lama
Composite
Lame di elica
Si
Prop Specs
MTV-14-B/185-59b, 4 Bladed Composite with Electric De-Ice, Polished Spinner
TT: 598 hours
Modifications/Conversions
Modifiche/Conversioni
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
Avionica
Avionica/Radio
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
Attrezzatura Aggiuntiva
Sistema di ossigeno
Si
Attrezzature aggiuntive
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
Esteriore
Anno dipinto
1995
Interno
Anno Interno
1995
Numero di posti a sedere
4
Configurazione
Passenger
Interiore
Original Grey Fabric/Velour Seats with Grey Leather Headrests, in good condition
Light Hail Damage on Surfaces Leading Edges
Stato Ispezione
Stato di ispezione
Annual inspection to be completed in July 2025
Idoneo alla navigazione aerea
Si
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