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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 | 135 | 250 | | Power | 100 hp | | | Cruise, 75% power | 124 | 230 | | Number of Cylinders | 4 | | | Vne | 151 | 280 | | 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 | 28,5 | 8,7 | | Total over 50 fr obstacle | 1067 | 380 | | Wing Area | 129 sq/ft | 12 | | Landing Performance | | | | Fuselage | | | | Ground roll | 488 | 160 | | Length | 21 | 6,4 | | Total over 50 fr obstacle | 915 | 300 | | Height | 8,2 | 2,5 | | | | | | 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 ECHO 2000 RG STANDARD EQUIPMENT | | FLIGHT INSTRUMENTS and INDICATORS - MAGNETIC COMPASS - AIRSPEED IND., Km - ALTIMETER DUAL MODE (IN) - VERTICAL SPEED - BANK INDICATOR - FLPA 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 - LANDING GEAR, RETRACTABLE ELECTROHYDRAULIC - LANDING GEAR SELECTOR SWITCH - LANDING GEAR WARNING HORN - LANDING GEAR EMERGENCY EXTENSION - FUEL CONTROL SELECTOR WITH ON/OFF - PANEL SWITCHES: _ STARTER _ FUEL PUMP _ ENGINE LH and RH IGNITION SWITCHES | | ELECTRICAL SYSTEM - 12 VOLT 18A AMP. BATTERY - 12 VOLT ALTERNATORS-20 AMP. - SWITCHES - CIRCUIT FUSES PANEL FUEL SYSTEM - TWO INTEGRAL FUEL TANKS WITH 92 LITRES TOTAL CAPACITY - ENGINE DRIVEN FUEL PUMP - AUXILIARY FUEL PUMPS, ELECTRIC - FUEL QUICK DRAIN INTERIOR - 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 EXTERIOR - LH/RH FRONT DOOR Pilot/Copilot, Lock and Key - REAR WINDOW - ALL WINDOWS TINTED - RETRACTABLE LANDING GEAR - TIE DOWN RINGS - MAIN WHEELS, 5,00 X 5 - NOSE WHEEL, 4,00 X 6 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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