SPECIFICATION & DESCRIPTION Pag. | 1 TECNAM ASTORE Specification & Description INTRODUCTION INDROD UCTION This document is published for the purpose of providing general information for the evaluation of design, performance and equipment of the Tecnam model Astore. Should more information be required, please contact: This document describes only the Tecnam model Astore, its powerplant and equipment. www.tecnam.com Pag. | 2 SPECIFICATION & DESCRIPTION Table of Contents General description .......................................................................................................................................... 3 Construction ...................................................................................................................................................... 3 Landing Gear ................................................................................................................................................... 3 Powerplant and propeller ............................................................................................................................. 3 Cabin .................................................................................................................................................................. 3 Three views ........................................................................................................................................................ 6 Astore Standard equipment list ........................................................................................................................ 7 OPTION 1 – Astore Six pack ............................................................................................................................. 10 OPTION 2 - DYNON SV1000 TWO SCREENS + GPS796 .................................................................................... 11 OPTION 3 – G3X TWO SCREENS ...................................................................................................................... 12 Engine Upgrade ............................................................................................................................................... 13 OPTIONALS ...................................................................................................................................................... 14 TECNAM COLORS ............................................................................................................................................. 16 INTERIORS ........................................................................................................................................................ 18 www.tecnam.com SPECIFICATION & DESCRIPTION Pag. | 3 General description All information here applies to the Tecnam model Astore equipped with the Rotax 912 ULS2 / IS engine and the Astore equipped with the Rotax 914 Turbo engine. Construction The Tecnam Astore is a low wing, two-place, single-engine airplane equipped with tricycle landing gear. The all metal airframe structure is complemented by the selective use of an epoxy reinforced matrix of carbon/glass fiber for the upper radome and fairings. Landing Gear The main landing gear consists of two 7075T6 light alloy springs which are hinged inside the fuselage in order to maximize the wheel deflection and energy absorption efficiency. These springs are supported by robust machined components which spread the load directly onto the main bulkheads. Two rawhide liners are inserted between each spring-leaf and the external machined beam. Two bolts secure the individual spring-leaf to the edge of the beam via a light alloy clamp while a single bolt secures the inboard end of the leaf-spring to the hinge and inner machined beam. The nose gear is free castering and is supported by an oleo-pneumatic shock absorber connected directly to the firewall. Differential toe brakes for steering are standard for both pilot and co-pilot with redundant brake master cylinders (4 in total). The horizontal tail is made up of a stabilizer and elevator with tip balancing horns. All the control surfaces, except for the flaps and trim tab, are balanced, and all the surfaces, except for the rudder and fuselage aileron line, are controlled via push-pull rods. Powerplant and propeller Standard engine is the well-known Rotax 912ULS2 but the injected (912iS2) and turbocharged (914UL2) version are also available. The standard propeller is a two blade fixed pitch wooden-composite wrapped Sensenich, with composite made propellers from the same brand also available in two and three bladed versions. The total usable fuel is 29 Gal (110lt) while the entire fuel system runs below the cabin structure, protecting the occupants from the fuel lines, which consist of rigid hoses and AN fittings. The canopy forms an integral part of the upper radome sliding forward and aft with final closing achieved by pulling the canopy vertically down onto an automotive-type seal. Three latches and 4 pins secure the canopy to the radome ensuring the best sound proofing possible. Cabin The Cabin offers newly designed seats and seat rails which are easily operated and adjustable fore and aft via a single handle with a reinforced area between the rails to make cabin access even easier. A roomy baggage compartment accommodates voluminous items with both external and internal access. A strong automotive seal is used on the baggage door and a courtesy lamp illuminates when this big door is opened. A newly designed and wide cockpit panel provides the largest choice of avionics on offer with a comfortable armrest and USB charger rounding out the luxurious interior. The avionics package always includes an iPad Mini with a built in application called "Tecnam Astore Owner app" containing a lot of relevant and useful information. www.tecnam.com Pag. | 4 SPECIFICATION & DESCRIPTION Everything about the Tecnam Astore is designed to allow you and your passenger to experience the most outstanding style, comfort, beauty and technology. Enjoy the Astore! • Certification The Tecnam Astore is delivered in full compliance with the requirements of US LSA ASTM F2245 (Package 02) • Engine & Propeller Allowed engine power: 98 to 115hp Manufacturer: ROTAX Models: 912ULS2 - 912is - 914 Propeller diameter: 1.73 to 1. 8mt (5.67 to 5.90ft) Number of blades: 2/3 Approved manufacturers: GT-Tonini-Sensenich- Approved prop. types: Fixed - Ground adj. • Dimensions Overall Height: 7.54ft 2.3mt Overall Length: 23.0ft 7.0mt • Wing Span (overall): 28.4ft 8.65mt Area: 131ft2 12.2mt2 Dihedral: 5° Aspect ratio: 6.2 • Cabin Height (max): 3.21ft 0.98mt Width (trim to trim): 3.8ft 1.15mt • Baggage door (optional) Height: 9.8in 0.25mt Width: 15.7in 0.40mt • Baggage Compartment Width: 2.95in 0.90mt Length: 2.39ft 0.73mt Height: 1.64ft 0.5mt Volume: 11,6cu.ft 329lt Max. permissible load: 77lb 35kg www.tecnam.com SPECIFICATION & DESCRIPTION Pag. | 5 • Performance (600kg\1320lbs-912 ULS-Sensenich propeller) Service Ceiling: 15.000ft 4572mt Takeoff Distance S.L. (Ground Roll): 715ft 218mt Takeoff Distance S.L. (To Clear 50ft. Obstacle): 1180ft 360mt Max Climb Rate S.L: 1100ft/min 5,6mt/sec Max Speed S.L: 127kt 235km/h Max Range: 750nm Cruise Speed (75% pwr at 6.500ft): 118kt 219km/h Vne (never exceed this speed) 150kt 278km/h Landing Distance (Ground Roll): 505ft 154mt Landing Distance (To Clear 50 ft Obstacle): 990ft 302mt Stall Speed, flap UP 44kt 81km/h Stall Speed, flap DW 38kt 70km/h • Design weight and capacities Standard empty weight 809lb 367kg Max Take-off Weight: 1320lb 600kg Landing Weight: 1320lb 600kg Maximum Useful Load: 511lb 233kg Fuel Capacity: 29US Gal 110lt www.tecnam.com Pag. | 6 SPECIFICATION & DESCRIPTION Three views www.tecnam.com SPECIFICATION & DESCRIPTION Pag. | 7 Astore Standard equipment list The following list of equipment is included in the standard aircraft Analog Avionics Package and does not reflect optional equipment. Flight instruments and indicators • MAGNETIC COMPASS • AIRSPEED IND., Kt • ALTIMETER • VERTICAL SPEED • SIDESLIP INDICATOR • PITOT SYSTEM • STATIC SYSTEM Engine instruments Dynon D10 Includes: • TACHOMETER • HOUR RECORDER • OIL PRESS • OIL TEMP. • HEAD TEMP. • FUEL PRESS. • VOLTMETER • ELEVATOR TRIM POSITION INDICATOR • FLAP INDICATOR • LH + RH FUEL QTY Flight controls • HYDRAULIC TOE BRAKES • PARKING BRAKE • ELECTRICAL FLAPS • DUAL FLIGHT CONTROLS • CASTORING NOSE WHEEL • STABILATOR TRIM (Electric actuated from Stick) • ENGINE CONTROLS: o CENTRAL QUADRANT WITH SINGLE THROTTLE LEVER o CHOKE • FLIGHT TRIM CONTROLS: o ELEVATOR TRIM with INDICATOR o FUEL CONTROL SELECTOR ANDAIR Panel switches • SPLIT STARTER • AVIONICS MASTER • STARTER KEY ACS • FUEL PUMP www.tecnam.com Pag. | 8 SPECIFICATION & DESCRIPTION Electrical system • 13,2V 7 AMP. ALLIANT BATTERY • 14V ALTERNATOR-20 AMP. • ROCKER SWITCHES INTERNALLY LIGHTED o Master switch o Landing light o Nav light o Strobe light • CIRCUIT BREAKER PANEL • LANDING/TAXI LIGHT LED • WING LIGHT GREEN/RED, WHITE and STROBE AVEO Full LED • 12 VOLT SOCKET Fuel system • TWO INTEGRAL FUEL TANKS WITH 110lt\29USgal total capacity • ENGINE DRIVEN FUEL PUMP • AUXILIARY FUEL PUMP, ELECTRIC • FUEL TANK QUICK DRAIN , TWO • 1 X SHUT OFF AND FUEL SELECTOR VALVE (Andair) Interiors • PILOT and CO-PILOT SEATS o Eco leatherette o Adjustable fore and aft • SEAT BELTS 3 POINTS ALL SEATS • WALL TO WALL CARPETING • MAP & STORAGE POCKETS • RADIO CALL PLATE • SOUNDPROOFING • LUGGAGE COMPARTMENTS • EMERGENCY HAMMER Exterior • EPOXY CORROSION PROOFING, All structure • CANOPY,