Astore US-LSA

Fun with room and a view

The Tecnam Astore is a metal, 2 place, low wing fun machine. Equally at home flying formation or to that far off destination. So much room for entry, long legs and baggage. The performance and control feel are only matched by the incredible view, both looking out and looking at the Astore.

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Quick facts

0NM

Max Range

Fuel Capacity
2 x 14.,5 US Gal – 2 x 55 lt

120 kts

Max Cruise Speed

222 km/h

0

Seating

Two seats side by side

17 l/h

Fuel Consumption

Only 4.5 US Gal  per hour,
AVGAS and MOGAS Automotive Fuel

Exteriors

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.
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 springleaf and the external machined beam. Two bolts secure the individual springleaf to the edge of the beam via a light alloy clamp while a single bolt secures the inboard end of the leafspring 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 copilot 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 pushpull rods.

Interiors Details

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 type seal is used on the baggage door and a courtesy lamp illuminates when opened. A wide cockpit panel provides plenty of room for glass panel avionics. A comfortable armrest and USB charger round out the luxurious interior.
Everything about the Tecnam Astore is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight..
Enjoy the Astore!

Avionics

Option 1 Astore Six pack

Non additive, replaces standard equipment and avionics
Flight instruments and indicators
• ATTITUDE, electric
• DIRECTIONAL, electric
• TURN & BANK
• ELEVATOR TRIM POSITION INDICATOR • FLAP INDICATOR
Engine analog instruments
• TACHOMETER
• HOUR RECORDER • OIL PRESS
• OIL TEMP.
• HEAD TEMP.
• FUEL PRESS.
• VOLTMETER
• AMMETER
• LH RH FUEL QTY

AVIONICS PACKAGE

• GARMIN GMA 240 Audio Panel
• GARMIN GTR 200 COM
• GARMIN GTX 327 TRANSPONDER
• GARMIN 796 GPS XM VERSION
• STICK PUSHNTONTALK SWITCHNPILOT/COPILOT • MIC & PHONE JACKSNPILOT/COPILOT
• ANTENNAS:
o TRANSPONDER o VHF
o GPS

Option 2 – DYNON SV1000 + GPS796

Non additive, replaces standard equipment and avionic
DYNON SKY VIEW SV1000 TWO SCREENS AVIONICS PACK FOR ROTAX 912 ULS2 & IS
• SKYVIEW SV 1000 10” 2 SCREEN DISPLAY (includes main wiring harness) • SVNADAHRSN200
• SVNADAHRSN201
• SVNEMSN221/A ENGINE MONITORING MODULE FOR ROTAX 912
• SVNGPSN250
• SVNBATN320
• BACKUP ALTIMETER AND AIRSPEED INDICATOR

AVIONICS PACKAGE

• Dynon SVNINTERCOMN2S
• Dynon SVNCOMNC25 COM (25 KhZ)
• Dynon SVNXPNDRN261 TRANSPONDER
• STICK PUSHNTONTALK SWITCHNPILOT/COPILOT • MIC & PHONE JACKSNPILOT/COPILOT
• ANTENNAS:
o TRANSPONDER o VHF
o GPS
• GPS 796 GPS XM VERSION

Option 3 – GARMIN G3X

Non additive, replaces standard equipment and avionics
Garmin G3X two screens Avionics Package for Rotax 912 ULS2
• GDU460
• GDU465
• ADAHRS GSU 25
• GEA 24 Engine Instrument Module
• GMU 22 Magnetometer
• GTP 59 Temperature Probe
• GA 35 GPS/WAAS Antenna
• LRU KIT
• INSTALLATION KIT
• G3X SENSOR KIT
• BACK UP AIRSPEED. And ALTIMETER 3
GSU CONFIGURATION
• AMPS (AMMETER SHUNT OR HALL EFFECT) • MONITOR CHT
• AIRCRAFT BUS VOLTAGES
• OIL TEMPERATURE
• OAT
• OIL PRESSURE
• MANIFOLD PRESSURE • FUEL PRESSURE
• RPM
• TRIM INDICATOR

AVIONICS PACKAGE

• GARMIN GMA 240 Audio Panel
• GARMIN GTR 200 COM
• GTX 23 Transponder mode S remote mounted • STICK PUSHNTONTALK SWITCHNPILOT/COPILOT • MIC & PHONE JACKSNPILOT/COPILOT
• ANTENNAS:
o TRANSPONDER
o VHF

Standard Equipment

Flight instruments and indicators

• Magnetic Compass
• Airspeed Ind. Kts
• 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
• Stabilator 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:
– Central Quadrant with Single Throttle Lever
– Choke
• Flight Trim Controls:
– Stabilator Trim With Indicator
• Fuel Control Selector ANDAIR

Panel switches

• Split Starter
• Avionics Master
• Fuel Pump
• Starter Key Acs

Electrical system

• 13.2 Volt 7 Amp. ALLIANT Battery
• 14 Volt Alternators-20 Amp.
• Switches:
– Master Switch
– Landing Light
– Nav Light
– Strobe Light
• Circuit Breaker Panel
• Landing/Taxi Led Light
• Wing Light Green/Red, White And Strobe Aveo Full Led
• 12 Volt Socket
• External Power Supply

Fuel system

• Two Integral Fuel Tanks With 110Lt\29 US gal Total Capacity
• Engine Driven Fuel Pump
• Auxiliary Fuel Pump, Electric
• Fuel Tank Quick Drain , Two
• 1 x Shut Off Valve ANDAIR

Interiors

• Pilot And Copilot Seats:
– Eco Leather
– 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, Lock And Key
• All Windows Tinted
• Main Wheels, 5,00 X 5
• Nose Wheel, 5,00 X 5
• Tie Down Rings

Exteriors lights

• Wing Tip Light Strobe and Position Led Light
• Landing/Taxi Light Led

Cabin comfort system

• Windshield Defroster
• Ventilator Adjustable

Powerplant and Propeller

• Fire Wall Inox
• Engines 1 Rotax 912Uls2 100 Hp, 4 Cylinders
• Liquid/Air Cooled, Integrated Reduction Gear
• Dual Ignition System
• Throttle Control Central
• Tubular Steel Engine Mount
• Propeller Sensenich, 2 Blade Fixed Pitch
• Propeller Spinner
• 2 Air Filter
• Oil Filter
• Oil And Water Coolers
• Fire Sleeve On Fuel And Oil Tubes
• Termostatic Oil Valve

Standard Avionics Package

• APPLE I-PAD Mini
• ELT 406 Mhz With Antenna & Remote Mounted Switch

Product Support and Documents

• Manufacturers Full Two Year Limited Warranty
• Pilots Operation Handbook
• Maintenance Manual
• Parts Catalog

Specification

Aircraft Dimensions

Fuselage Height 7.54 ft – 2.3 mt
Fuselage Length 23 ft -7 mt
Wingspan 28.4 ft – 8.65 mt
Cabin Height (seat to cover) 3.21 ft – 0.98 mt
Cabin Width 3.8 ft – 1.15 mt
Max Seating capacity 2
Fuel tank capacity 2 x 14.5 US Gal – 2 x 55 lt

Powerplant

Engine Manufacturer ROTAX 912ULS2 / 912is / 914Turbo
Engine Power 98 to 115hp
Time Before Overhaul 2.000 hrs
Propeller Sensenich 2/3 blades
Fuel Consumption 4.50 US Gal/h – 17 lt/h
Fuel Type Mogas and Avgas

Design Weight & Loading

Maximum Take Off Weight 600 kg – 1320 lb
Empty Weight, Standard 827 lb – 375 kg
Useful Load 496 lb – 225 kg
Baggage allowance 77.16 lb -35 kg
Design Weight 600 kg – 1320 lb

Performance

Max Cruise Speed (KTAS) 120 kts – 222 km/h KTAS
Stall Speed (Flaps Down Power Off) KCAS 39 kts – 72 km/h KCAS
Practical ceiling 13110 ft – 3996 mt
Take off run 489 ft – 149 mt
Take off distance 984 ft – 300 mt
Landing Run 620 ft – 189 mt
Landing Distance 1100 ft – 335 mt
Rate of climb 923 ft/min – 4.69 mt/sec
Range 642 NM – 1188 km

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.

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