P92 Tail Dragger

Flying on “classic” wheels

The Tecnam P92-TD is a metal, 2 place, high wing, tail dragger 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 Tail Dragger.

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Quick facts

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Take-Off Run

443 ft

120 kts

Max Cruise Speed

222 km/h

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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 P92 Tail Dragger is a high wing, two place, single engine airplane equipped with tail landing gear.
The Tecnam P92 Tail Dragger is the first new ‘tail wheel aeroplane a ailable to the General Aviation community in quite a while. Consumers clearly indicated that they wanted a tail wheel aeroplane constructed from metal rather than fabric. They wanted their passenger to sit right next to them, rather than behind as in most legacy ‘tail wheel aeroplanes.
TecnamTail Dragger has been designed to offer many more functions including as a perfect towing airplane. It also a great cargo carrier and is with an optional, large underside cargo pod, designed with two hinged doors.

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.
Everything about the Tecnam P92 Tail Dragger is designed to allow you and your passenger to experience the most outstanding style, comfort, and beauty of flight.. Enjoy the Tail Dragger!

Standard Equipment

Flight instruments and indicators

· Magnetic Compass
· Airspeed Ind., Km
· Altimeter
· Vertical Speed
· Bank Indicator
· Pitot System
· Static System
– Stabilator Trim POSITION INDICATOR

Engine instruments (Only For Rotax)

Dynon D10 Includes:
· Tachometer
· Hour Recorder
· Oil Press
· Oil Temp.
· Head Temp.
· Fuel Press.
· Voltmeter
· Lh+Rh Fuel Q.ty
· Flap Indicator

Flight controls

· Hydraulic Toe Brakes
· Parking Brake
· Electrical Flaps
· Dual Flight Controls
· Free Tail Wheel
· Stabilator Trim (Electric actuated from Stick)
· Engine Controls
– Throttle (Two)
– Choke
· Flight Trim Controls
– Stabilator With Indicator
· Fuel Control Selector With Lh/Rh Off (AND AIR)

Panel switches

• Avionics Master
• Fuel Pump
• Starter Key Acs

Electrical system

• 12 Volt 18A Amp Battery
• 12 Volt Alternators-20 Amp.
• Rocker Switches Internally Lighted
• Switches:
– Landing Light
– Strobe Light
• Circuit Breaker Panel
• 12 Volt Socket

Fuel system

• Two Integral Fuel Tanks With 92 LT, xx US Gal Total Capacity
• Engine Driven Fuel Pump
• Fuel Tank Quick Drain

Interiors

• Pilot And Co-Pilot Seats:
– Arm Rest
– Adjustable Fore And Aft
• Seat Belts & Shoulers, All Seats
• Wall To Wall Carpeting
• Luggage Compartments

Exterior

• Epoxy Corrosion Proofing, All Structure
• LH/RH Front Door, Lock And Key
• Main Wheels, 5.00 X 5
• Nose Wheel, 5.00 X 5
• All Window Tinted

Exteriors lights

• Wing Light Green/Red, White Strobe and Aveo Non TSO
• Taxi Light

Cabin comfort system

• Windshield Defroster
• Ventilator Adjustable, 2 place
• Heating System with Defrots

Powerplant and Propeller

• Engines 1 Rotax 912Uls2 100 Hp:
– 4 Cylinders
– Liquid/Air Cooled
– Integrated Reduction Gear
• Dual Ignition System
• Throttle Control LH/RH
• Tubular Steel Engine Mount
• Propeller 2 Blade Fixed Pitch
• Propeller Spinner
• Air Filter
• Oil Filter
• Oil And Water Coolers

Product Support and Documents

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

Category Upgrades

A1002 Advanced

• Firewall Inox
• Radio ICA210 COM installed
• Transponder GTX 327 installed
• Firewall Inox
• ELT AK 450 installed
• Fire Sleeve on fuel and oil tube
• Paracachute 600 KG

A1003 US-LSA

• Firewall Inox
• Airspeed Ind. Its
• Panel Switches:
– Split Starter
– Avionic
– Starter Key Acs
• Tie Down Ring
• Fire Sleeve on fuel and oil tube
• Thermostatic Valve Oil
• Baggage Compartment Net
• External Power Supply
• Extended Warranty for ROTAX Engine ( 1 year extension)
• Taxi Light LED
• Wing Strut Larger Size

Engine Upgrades

A-EUP 01 ROTAX 912 IS

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Replacement of the engine Rotax 912ULS2. Non-Additive.
Replaces all Standard Equipment.
Also Includes the following equipment:

• Engine ROTAX 912 IS
• Andair Fuel Selector

A-EUP 04 ROTAX 914 Turbo V. P.

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Replacement of the engine Rotax 912ULS2. Non-Additive.
Replaces all Standard Equipment.
Also Includes the following equipment:

• Engine ROTAX 914 Turbo
• MAP
NEUFORM  V.P. PROPELLER ELECTRIC with regulator 2 Blades

A-EUP 05 ROTAX 914 Turbo

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Replacement of the engine Rotax 912ULS2. Non-Additive.
Replaces all Standard Equipment.
Also Includes the following equipment:

• Engine ROTAX 914 Turbo
• MAP
SENSENICH  Ground Adjustable 2 Blades Propeller

Specification

Aircraft Dimensions

Fuselage Height 2,0 mt -6.6 ft
Fuselage Length 6,5 mt – 21.3 ft
Wingspan 8.70 mt – 28.5 ft
Cabin Height (seat to cover) 0.91 mt – 3 ft
Cabin Width 1.14 mt – 3.74 ft
Max Seating capacity 2
Fuel tank capacity 2 x 45 lt – 2 x 11.9 US Gal

Powerplant

Engine Manufacturer ROTAX 912 ULS – 914
Engine Power 98 to 115hp
Time Before Overhaul 2000 hrs
Propeller Two-Bladed Fixed Pitch – Wood
Fuel Consumption 17 lt/h – 4.50 US Gal/h
Fuel Type mogas and Avgas

Design Weight & Loading

Maximum Take Off Weight Design Weight: 600 kg – 1320 lb
Baggage allowance 20 kg – 44 lb

Performance

Max Cruise Speed (KTAS) 222 km/h – 120 kts
Stall Speed (Flaps Down Power Off) KCAS 70 km/h – 38 kts
Practical ceiling 4267 mt – 14,000 ft
Take off run 135 mt – 443 ft
Take off distance 393 mt – 1289 ft
Landing Run 204 mt – 669 ft
Landing Distance 467 mt – 1204 ft
Rate of climb 870 ft/min
Range 456 NM – 845 km

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

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