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Since July 2007, Tecnam Hellas is the exclusive Distributor-Promoter for TECNAM Aircrafts for Greece, Cyprus and the Balkans. | ENGINE | | | | PERFORMANCE MTOW | | | | Manufacturer | Rotax | | | Speed | Kts | Km | | Model | 912 ULS2 | | | Maximum at Sea Level, Gross Weight | 120 | 222 | | Power | 100 hp | | | Cruise, 75% power | 112 | 208 | | Number of Cylinders | 4 | | | Vne | 146 | 270 | | PROPELLER | | | | Stall Speed | | | | Manufacturer | Tonini | | | Flaps up, power off | 45 | 83 | | Model | GT | | | Flaps Down, power off | 37 | 68 | | Number of Blades | 2 | | | Rate of Climb at Sea Level | 850 ft/m | | | Type | Fix | | | Service Ceiling | 13,110 ft | 4300 m | | DIMENSION | | | | Takeoff Performance | ft | m | | Wing | ft | m | | Ground roll | 610 | 280 | | Wing Span | 29,5 | 9 | | Total over 50 fr obstacle | 1067 | 380 | | Wing Area | 133 sq/ft | 12,4 | | Landing Performance | | | | Fuselage | | | | Ground roll | 488 | 160 | | Length | 2,3 | 6,5 | | Total over 50 fr obstacle | 915 | 300 | | Height | 8,5 | 2,6 | | | | | | LH-RH Cabin Door | in | m | | | | | | Height | 33 | 0,83 | | | | | | Width | 30 | 0,76 | | | | | | WEIGHTS | lb | kg | | All estimated performance data are based on - airplane weights at 992lb,
- standard atmospheric condition level,
- hard surface,
- dry runways and no wind.
| | Maximum Take-off weight | 992 | 450 | | | Maximum Ramp Weight | 992 | 450 | | | Standard Equipped weight | 730 | 331 | | | Standard Useful Load | 593 | 269 | | | Ultimate Loads | +6 – 3 | +6 – 3 | | | Baggage Allowance | 44 | 20 | | | P92 EAGLET STANDARD EQUIPMENT | | FLIGHT INSTRUMENTS and INDICATORS
- MAGNETIC COMPASS
- AIRSPEED IND., Km
- ALTIMETER DUAL MODE (IN)
- VERTICAL SPEED
- BANK INDICATOR
- FLAP INDICATOR
- PITOT SYSTEM
- STATIC SYSTEM
- STABILATOR TRIM POSITION INDICATOR
ENGINE INSTRUMENTS
- TACHOMETER
- HOUR RECORDER
- OIL PRESS
- OIL TEMP.
- HEAD TEMP.
- FUEL PRESS.
- VOLTMETER
- LH + RH FUEL QTY
FLIGHT CONTROLS
- HYDRAULIC BRAKES
- PARKING BRAKE
- ELECTRICAL FLAPS
- DUAL FLIGHT CONTROLS
- STEERABLE NOSE WHEEL
- STABILATOR TRIM (Electric actuated from Stick)
- ENGINE CONTROLS
_ THROTTLE, TWO
_ CHOKE
- FLIGHT TRIM CONTROLS
_ STABILATOR with INDICATOR
- FUEL CONTROL SELECTOR WITH ON/OFF
- PANEL SWITCHES:
_ STARTER
_ AVIONIC MASTER | | ELECTRICAL SYSTEM
- 12 VOLT 18A AMP. BATTERY
- 12 VOLT ALTERNATORS-20 AMP.
- SWITCHES
_Landing Light
_Strobe Light
- 12 VOLT socket
- CIRCUIT BREAKERS PANEL
FUEL SYSTEM
- TWO INTEGRAL FUEL TANKS WITH 92 LITRES
TOTAL CAPACITY
- ENGINE DRIVEN FUEL PUMP
- FUEL QUICK DRAIN
INTERIOR
- PILOT and CO-PILOT SEATS
_ Adjustable Fore and Aft
_Arm Rest
- SEAT BELTS & Shoulder Harness, All Seats
- WALL TO WALL CARPETING
- MAP E STORAGE POCKETS
- LUGGAGE COMPARTMENTS
EXTERIOR
- EPOXY CORROSION PROOFING, All structure
- LH/RH FRONT DOOR Pilot/Co-pilot, Lock and Key
- REAR WINDOW
- ALL WINDOWS TINTED
- MAIN WHEELS, 5,00 X 5
- NOSE WHEEL, 4,00 X 6
EXTERIOR LIGHTS
- VERTICAL TAIL STROBE
- TAXI LIGHT
CABIN CONFORT SYSTEM
- VENTILATOR ADJUSTABLE, 2 place
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 - GT Propeller, 2 Blade fix
- PROPELLER SPINNER
- AIR FILTER
- OIL FILTER
- OIL AND WATER COOLERS
PRODUCT SUPPORT/DOCUMENTS
- MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
- PILOTS OPERATION HANDBOOK
- MAINTENANCE MANUAL | | There is a wide list of available options... |
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Tecnam Hellas 
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