The Tecnam line employs a monocoque tail cone section with the forward fuselage using sheet aluminium over steel tubing.
The wing is an all aluminium conventional structure with a single strut.
The fuel tanks hold 11.9 gal/45l each, located in the wing leading edge separated from the fuselage for safety.
A wide rear window together with large side windows complete the extraordinary visibility allowing 360° of vision in the cockpit.
The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column.
The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height.
The large flaps are deployed electrically.
The low stall speed and the general slow flying characteristics of the aircraft allow it to operate with ease on short runways
Seats are adjustable and increase in height as they are moved forward.
The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with easy access in flight.
All Tecnam aircraft have dual control sticks, throttles and rudder pedals.
The trim tab and the flaps are electrically activated with a position indicator on the instrument panel.
The fresh air vents are conveniently located in the doors.
The aircraft has dual rudder pedals with a steerable nose wheel.
The wide instrument panel is designed to accommodate a full variety of instrumentation
The main landing gear legs are made of spring steel, directly connected to the main structure.
The landing gear is robust enough for rough strips and require no maintenance.
The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance.
The main landing gear wheels and brakes are conventional aircraft size (5.00x5).
The brake lever control and the parking brake are located forward between the seats
The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish. The top cowl has a large opening for easy access to the engine compartment for effective pre-flight inspections.
The engine's mount is steel-tubing with shock mounts. It also supports the nosewheel that is not anchored directly to the cabin's structure.
Two power plant options are available: Rotax 912UL 80HP four-cylinder, four-stroke engine and Rotax 912 ULS 100HP four-cylinder, four-stroke engine. Both engines come with an integrated 1:2.4286 reduction gear.
A fixed pitch wood and composite propeller comes as standard.
The quick drain gascolator is installed in the engine compartment with easy outside access.
The fuel system uses a mechanical engine driven pump along is with an electrical back-up pump.
The battery is located in the rear of the fuselage with easy access through a hinged door.
|FLIGHT INSTRUMENTS AND INDICATORS|
- MAGNETIC COMPASS
- AIRSPEED IND., Kts
- ALTIMETER (IN)
- VERTICAL SPEED
- BANK INDICATOR
- PITOT SYSTEM
- STATIC SYSTEM
- STABILATOR TRIM POSITION INDICATOR
DYNON D10 including:
- HOUR RECORDER
- OIL PRESS
- OIL TEMP.
- HEAD TEMP.
- FUEL PRESS.
- LH + RH FUEL QTY
- TRIM INDICATOR
- FLAP INDICATOR
| ||FLIGHT CONTROLS|
- HYDRAULIC BRAKES
- PARKING BRAKE
- ELECTRICAL FLAPS
- DUAL FLIGHT CONTROLS
- STEERABLE NOSE WHEEL
- STABILATOR TRIM (Between the seats)
- ENGINE CONTROLS
_ THROTTLE, TWO
- FLIGHT TRIM CONTROLS
_ STABILATOR with INDICATOR
- FUEL CONTROL SELECTOR WITH ON/OFF
- PANEL SWITCHES:
_ ENGINE LH and RH IGNITION SWITCHES
- 12 VOLT 18A AMP. BATTERY
- 12 VOLT ALTERNATORS-20 AMP.
- Landing Light
- 12 VOLT socket
- CIRCUIT FUSES PANEL
| ||FUEL SYSTEM|
- TWO INTEGRAL FUEL TANKS WITH 100 LITRES
- ENGINE DRIVEN FUEL PUMP
- FUEL QUICK DRAIN
- PILOT and COPILOT SEATS
- Adjustable Fore and Aft
- Arm Rest
- SEAT BELTS & Shoulder Harness, All Seats
- WALL TO WALL CARPETING
- MAP E STORAGE POCKETS
- LUGGAGE COMPARTMENTS
- REAR WINDOW
- ALL LATERAL AND REAR WINDOWS TINTED BROWN
- TIE DOWN RINGS
- MAIN WHEELS, 5,00 X 5
- NOSE WHEEL, 5,00 X 5
- WHEEL PANTS
- TAXI LIGHT
| ||CABIN COMFORT SYSTEM|
- VENTILATOR ADJUSTABLE, 2 place
| ||POWERPLANT AND PROPELLER|
- ENGINES - 1 ROTAX 912UL 80/100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
- DUAL IGNITION SYSTEM
- THROTTLE CONTROL LH/RH
- TUBULAR STEEL ENGINE MOUNT
- PROPELLER - GT Propeller, 2 Blade fix
- PROPELLER SPINNER
- AIR FILTER
- OIL FILTER
- OIL AND WATER COOLERS
- MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
- PILOTS OPERATION HANDBOOK
- MAINTENANCE MANUAL