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Mooney M20M Bravo TLS B |
US$ 165,569
€ 149,000 |
Overview
| Base data | | Type: | Single Prop | | Make: | Mooney | | Model: | M20M Bravo TLS B | | Year built: | 1995 | | Registration No.: | HB-DIF | | Location: | Switzerland | | Price: | € 149,000
(~ US$ 165,569) | | Full details |
| Seller |
Aeromeccanica S.A
Aeroporto Cantonale di Locarno
6596 Gordola
Switzerland
Tel: +41-91-2103128
Fax: +41-91-7450037 |
| Contact seller |
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Full Details
| Base data | | Type: | Single Prop | | Make: | Mooney | | Model: | M20M Bravo TLS B | | Year built: | 1995 | | Registration No.: | HB-DIF | | Location: | Switzerland | | Price: | € 149,000
(~ US$ 165,569) |
| Avionics | | 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 |
| Exterior | | Original White with red and Gold Accents, in good condition |
| Interior | | Original Grey Fabric/Velour Seats with Grey Leather Headrests, in good condition Light Hail Damage on Surfaces Leading Edges |
| Other remarks | 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
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)
S/N: 27-0206 Total Time: 1688 hours Engine Lycoming TIO-540-AF1B, S/N: L-9645-61A TT: 1688 Hours Shock Load Inspection performed by Cermec Motor in 2010 at TT: 1090 hours, after propeller ground strike MT-PROPELLER ENTWICKLUNG GMBH, MTV-14-B/185-59b, 4 Bladed Composite with Electric De-Ice, Polished Spinner TT: 598 hours
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 |
Pictures
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