listing placed 04 March 2014 United Kingdom

TROPHY TT-2000STOL 2010 zenith/Zenair STOL CH-701

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LIGHT AIRCRAFT ?29000

Trophy TT -2000 STOL
( GB license variety Zenair STOL CH -701 )
SP- SWMW
Price: ?29000
(nineteen thousand nine hundred ninety euro 00/100)


Manufacture 2010
Built under the supervision of the state , the ultra-light class .
Current checks , inspections, flys, insurance .
The continuous readiness for flight, hangared , no accidents, raided 110 h
Season volatile start from 1 May each year, from the day the opportunity to learn on the fly.
If interested, I invite you to the airport.

I. Description of the overall structure

Aircraft Trophy TT 2000 is a two-seat, single-engine high-wing , metal structure . The wings are modified NACA profile 680-18 with fixed slots and flaperons.
The hull construction with grid cab box made of steel pipes. Fixed tricycle landing gear . Castors controlled , coupled with the rudder . On the main wheels , hydraulic disc brake . The main stanchions made of steel pipes used shock absorbers. Front shin padded spring steel . Two fuel tanks of aluminium in the wings and one small outgoing behind the passenger seat . Place in the cabin next to each other , tiller doubled . Upholstered Armchairs from epoxy - glass mounted spring handles to the grid cabin. Two doors opened up.
Two lights, taxiway and landing.
Side lights green and red .
Warning light , strong reflector - strobe .
II. Technical aircraft Trophy TT 2000




Materials
Sheets for roofing gr. 0.04 mm , grade 5754 - T18 ( AlMg3 )
Plates for structural components gr. 0.06 mm , grade 2017A - T4 ( ALCu4MgSi )
grade 2024 -T3 ( ALCu4Mg1 )
Truss frames - steel pipe 20x0 , 8mm grade 18G2A
Rivets - 3.20 x10 , 4 AVEX 1661-00410 ( Al-Mg 2.5 )
4,00 x12, 5 AVEX 1661-00512 ( Al-Mg 2.5 )
Manufacturer: AVDEL Great Britain
III. Motor BMW 1100

Capacity 1.085 ccm
Power 90 hp at 7200 rev / min
Torque 95 Nm at 5500 rev / min
Fuel consumption 12 l / h
Unleaded 95
Weight 64 kg

IV. equipment
fuselage
Trimmer electrically controlled
Manual control of the front wheel and rudder
Doubled the control plane

Avionics pilot
speedometer
Altimeter
Clinometers ( ball )
Compass
Variometer
Multifunction Timer Clock
Radio ICOM IC- A200 / antenna hull
2 x headphones
Avionics Engine
Tachometer
Flydat engine (measurement : oil pressure , oil temperature , vacuum pressure in the intake manifold , fuel pressure , temperature, head temperature of the engine compartment , cabin temperature , voltage electrical installation )
Light fuel reserve
Oil pressure light
Light (battery charge indicator)
Fuel gauge indicator and optical expansion tank

Cabin
4 point seat belts
Luggage space behind the seats

Documentation
Instruction in flight
Engine manual
Book airframe
MOR INFO OR MORE PICTURE ASK PLZ.