TECNAM P2006T LANDING GEAR DETAIL FULL

^ a b TYPE-CERTIFICATE DATA SHEET EASA.A.185 P2006T (pdf) (11 ed.).Wing loading: 78 kg/m 2 (16 lb/sq ft) at MTOWĪircraft of comparable role, configuration, and era.Propellers: 2-bladed MT Propeller MTV-21, 1.78 m (5 ft 10 in) diameter constant-speed, fully feathering.Powerplant: 2 × Rotax 912S3 horizontally opposed four-cylinder geared piston engines, 75 kW (100 hp) each.Fuel capacity: 200 litres (44 imp gal 53 US gal).

TECNAM P2006T LANDING GEAR DETAIL FULL

Capacity: 3 passengers or 618 pounds (280 kg) payload with full fuel.NASA's all electric X-57 Maxwell prototype aircraft is being developed using a P2006T as its basic structure. The P2006T first flew on 13 September 2007 and was certified by EASA on 5 June 2009. The linkage between the flight controls and the flight surfaces is provided by pushrod, rather than the more common use of cables and pulleys. The engines have automatic mixture adjustment, so there is no mixture control required on the panel. The pilot's power quadrant contains three controls for each engine: throttle, propeller rpm, and carburetor heat. Thus, for FAA certification, the company was required to add a backup battery in addition to the standard battery. The electric starters, used to start the engines on the ground, must also be used for an inflight restart, since the highly geared engines cannot be turned by airflow past the stopped propeller. Thus both cooling airflow through the nacelle, and a cooling radiator, are required in each cowl. The Rotax engine cylinder heads are liquid-cooled there are cooling vanes on the cylinder barrels. A door on each side of the fuselage provides access to the seating area in addition an escape hatch is provided above the two forward seats, to be used if fuselage deformation in a crash prevents those doors from being operable. The fuselage section is a slightly rounded rectangle, higher than it is wide. The nosewheel of the tricycle landing gear retracts into the nose cone the trailing-link main units retract into stubs which extend from the lower fuselage. Its stabilator is attached to the fuselage, mostly aft of the vertical fin (the stabilator is a single unit with a cutout in its leading edge where it mounts to the tailcone). The P2006T is a twin-engined four-seat cantilever high-wing monoplane with a retractable tricycle landing gear.

Tecnam p2006t landing gear detail