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Since July 2007, Tecnam Hellas is the exclusive Distributor-Promoter for TECNAM Aircrafts for Greece, Cyprus and the Balkans.
| ENGINE |
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PERFORMANCE MTOW |
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| Manufacturer |
Rotax |
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Speed |
Kts |
Km |
| Model |
912 S3 |
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Maximum at Sea Level, Gross Weight |
136 |
252 |
| Power |
100 hp |
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Cruise, 75% power |
125 |
232 |
| Number of Cylinders |
4 |
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Vne |
156 |
290 |
| PROPELLER |
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Stall Speed |
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| Manufacturer |
Hoffmann |
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Flaps up, power off |
45 |
83 |
| Model |
HO-V352 |
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Flaps Down, power off |
39 |
72 |
| Number of Blades |
2 |
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Rate of Climb at Sea Level |
1050 ft/m |
| Type |
V.P. |
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Service Ceiling |
13,110 ft |
4300 m |
| DIMENSION |
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Takeoff Performance |
ft |
m |
| Wing |
ft |
m |
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Ground roll |
750 |
250 |
| Wing Span |
28,2 |
8,6 |
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Total over 50 fr obstacle |
1220 |
400 |
| Wing Area |
124 sq/ft |
11,5 |
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Landing Performance |
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| Fuselage |
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Ground roll |
915 |
300 |
| Length |
21,7 |
6,6 |
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Total over 50 fr obstacle |
1067 |
350 |
| Height |
8 |
2,43 |
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| WEIGHTS |
lb |
kg |
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All estimated performance data are based on
- airplane weights at 1280 lb,
- standard atmospheric condition level,
- hard surface,
- dry runways and no wind.
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| Maximum Take-off weight |
1320 |
600 |
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| Maximum Ramp Weight |
1320 |
600 |
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| Standard Equipped weight |
771 |
350 |
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| Standard Useful Load |
549 |
250 |
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| Ultimate Loads |
+6 – 3 |
+6 – 3 |
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| Baggage Allowance |
44 |
20 |
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P2002-JR STANDARD EQUIPMENT
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FLIGHT INSTRUMENTS and INDICATORS
- MAGNETIC COMPASS
- AIRSPEED IND., Kts
- ALTIMETER (IN)
- VERTICAL SPEED
- ATTITUDE ELECTRIC
- DIRECTIONAL ELECTRIC
- TURN AND BANK INDICATOR
- FLAPS INDICATOR
- PITOT SYSTEM
- STATIC SYSTEM
- STABILATOR TRIM POSITION INDICATOR
ENGINE INSTRUMENTS
- RPM INDICATOR
- HOUR RECORDER
- OIL PRESS
- OIL TEMP.
- HEAD TEMP.
- FUEL PRESS.
- VOLTMETER
- AMMETER
- MANIFOLD PRESSURE
- LH + RH FUEL QTY
OTHER INSTRUMENTS / WARNING
- CHRONOMETER
- O.A.T. INDICATOR
- GENERATOR WARNING LIGHT
FLIGHT CONTROLS
- HYDRAULIC BRAKES
- PARKING BRAKE
- ELECTRICAL FLAPS
- DUAL FLIGHT CONTROLS
- STEERABLE NOSE WHEEL
- STABILATOR TRIM (Electric actuated from Stick)
- ENGINE CONTROLS
_ THROTTLE, TWO
_ CARBURETOR HEAT
_ CHOKE
- LANDING GEAR, RETRACTABLE ELECTROHYDRAULIC
- LANDING GEAR SELECTOR SWITCH
- LANDING GEAR WARNING HORN
- LANDING GEAR EMERGENCY EXTENSION
- FLIGHT TRIM CONTROLS
_ STABILATOR with INDICATOR
- 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
Nav. Lights
_Landing Light
_Strobe Light
- EXTERNAL POWER SUPPLY RECEPTABLE
- CIRCUIT BREAKER PANEL
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FUEL SYSTEM
- TWO INTEGRAL FUEL TANKS WITH 100 LITRES
TOTAL CAPACITY
- ENGINE DRIVEN FUEL PUMP
- AUXILIARY FUEL PUMPS, ELECTRIC
- FUEL QUICK DRAIN
INTERIOR
- PILOT and COPILOT SEATS
_ Adjustable Fore and Aft
- SEAT BELTS & Shoulder Harness, All Seats
- WALL TO WALL CARPETING
- LUGGAGE COMPARTMENTS
- FIRE EXTINGUISHER
- RADIO CALL PLATE
- SOUNDPROOFING
- FIRST AID KIT
EXTERIOR
- EPOXY CORROSION PROOFING, All structure
- SLIDING CANOPY with lock and key
- REAR WINDOW
- TIE DOWN RINGS
- MAIN WHEELS, 5,00 X 5
- NOSE WHEEL, 4,00 X 6
EXTERIOR LIGHTS
- NAV. LIGHTS
- VERTICAL TAIL STROBE
- TAXI LIGHT
CABIN CONFORT SYSTEM
- WINDSHIELD DEFROSTER
- VENTILATOR ADJUSTABLE, 2 place
- HEATING SYSTEM
VENTILATOR ADJUSTABLE, 2 place
POWERPLANT AND PROPELLER
- ENGINES - 1 ROTAX 912S2 100 HP, 4 Cylinders
liquid/air cooled, integrated reduction gear
- DUAL IGNITION SYSTEM
- THROTTLE CONTROL LH/RH
- TUBULAR STEEL ENGINE MOUNT
- PROPELLER - Hoffmann, 2 Blade Variable Pitch
- PROPELLER CONTROL LH/RH
- PROPELLER SPINNER
- PROPELLER GOVERNOR
- AIR FILTER
- OIL FILTER
- OIL AND WATER COOLERS
- CARBURETOR HEAT with Manual Control
PRODUCT SUPPORT/DOCUMENTS
- MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
- PILOTS OPERATION HANDBOOK
- MAINTENANCE MANUAL
- PARTS CATALOG
- AIRCRAFT LOG BOOK
- ENGINE LOG BOOK
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Tecnam Hellas 
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