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Official Tecnam Dealer Belgium

P2008 JC CS/VLA


The P2008 CS-LSA has metal wings and a metal stabilator.
Tecnam chose to keep the metal wing and stabilator structures for strength, reliability, and ability to flex in flight providing a more comfortable ride. 
To produce the desired increase in cabin width and greater aerodynamic efficiency, Tecnam chose carbon fiber. 
The decision to utilize both materials was for the optimization of aerodynamic qualities, flight characteristics, and reliability. 
Tecnam was able to utilize the expertise from its aquisition of Tecnam Spain. 
This addition allows Tecnam to make decisions to be based on design and structural integrity rather than purely the cost of production. 
The wing is based on the well known NACA63A airfoil, and through partial tapering, it is brought close to the optimal lift distribution (elliptical). 
The singleslot flaps extend along much of the wing span. 
The Frise type aileron along with the taper design provides a high rate of roll. The all movable type (stabilator) horizontal tail, traditional on all Tecnam aircraft, allows excellent controllability and excellent “hands off” longitudinal stability

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The main springleaf landing gear, including wheels, tires and fairings, are the same as all of the other non-retractable Tecnam models. 
This design has withstood the test of time and extensive use in flight training environments. 
The newly designed nose gear is free castering and consists of a tubular steel leg, connected to the lower engine mount attachments and is braced by a rubber shock absorber. 
The steerable nose wheel is also available. 
All of the landing gear is faired to minimize drag. Ground steering is by differential braking.

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The powerplant and associated cowlings are similar to all of the existing Tecnam line with few modifications. 
The P2008 CS-LSA has higher capacity than the existing line (55x2 lt - 14,5x2 GAL) and fuel tanks are installed in the wing box, behind the main spar. 
This is to preserve their integrity in case of a crash landing and to minimize fire potential. 
The instrument panel size is increased from other Tecnam models due to the increase in cabin width. 
It is modular in design and can accommodate the most complete instrumentation, analogical or digital type.

 

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FLIGHT INSTRUMENTS AND INDICATORS
G3X DUAL SCREEN
GDU370
GDU375
LRU KIT
SENSOR KIT
INSTALLATION KIT
G3X SENSOR KIT
ANTENNA GPS
 ENGINE INSTRUMENTS, GSU CONFIGURATION
AMPS (AMMETER SHUNT OR HALL EFFECT)
MONITOR CHT
AIRCRAFT BUS VOLTAGES
OIL TEMP.
OAT
OIL PRESS
FUEL PRESS.
RPM
FUEL QTY
TRIM INDICATOR
 OTHER INSTRUMENTS / WARNING
CHRONOMETER
GENERATOR WARNING LIGHT
WARNING LIGHT:
- LOW OIL PRESSURE
- LOW FUEL PRESSURE
 
FLIGHT CONTROLS
HYDRAULIC TOE BRAKES
PARKING BRAKE
ELECTRICAL FLAPS
DUAL FLIGHT CONTROLS
CASTERING NOSE WHEEL
STABILATOR TRIM (ELECTRIC ACTUATED FROM STICK)
ENGINE CONTROLS
- CENTRAL QUADRANT WITH SINGLE TROTTLE LEVEL
- THROTTLE
- CHOKE
FLIGHT TRIM CONTROLS
- STABILATOR WITH INDICATOR
FUEL CONTROL SELECTOR WITH ANDAIR
PANEL SWITCHES:
- SPLIT STARTER
- AVIONIC
STARTER KEY ACS
 ELECTRICAL SYSTEM
12 VOLT 18A AMP. BATTERY FIAMM 64
12 VOLT ALTERNATORS-20 AMP.
SWITCHES
NAV. LIGHTS
- LANDING LIGHT
- STROBE LIGHT
12 VOLT SOCKET
EXTERNAL POWER SUPPLY RECEPTABLE
AUXILIARY ALTERNATOR 40A
CIRCUIT BREAKER PANEL
 FUEL SYSTEM
TWO INTEGRAL FUEL TANKS WITH 110 LITRES, TOTAL CAPACITY
ENGINE DRIVEN FUEL PUMP
ELECTRICAL FUEL PUMPS
FUEL QUICK DRAIN
 
INTERIOR
PILOT AND COPILOT SEATS
- ADJUSTABLE FORE AND AFT
SEAT BELTS & SHOULDER HARNESS, ALL SEATS
WALL TO WALL CARPETING
MAP E STORAGE POCKETS
LUGGAGE COMPARTMENTS
FIRE EXTINGUISHER
RADIO CALL PLATE
SOUNDPROOFING
FIRST AID KIT
 EXTERIOR
EPOXY CORROSION PROOFING, ALL STRUCTURE
LH/RH FRONT DOOR PILOT/COPILOT, LOCK AND KEY
ALL WINDOWS TINTED
MAIN WHEELS, 5,00 X 5 MARC INGEGNO
NOSE WHEEL, 5,00 X 5
STALL WARNING
 EXTERIOR LIGHTS
NAV. LIGHTS WITH STROBE
TAXI LIGHT
TAIL LIGHT
 
CABIN CONFORT SYSTEM
WINDSHIELD DEFROSTER
VENTILATOR ADJUSTABLE, 2 PLACE
HEATING SYSTEM
 POWERPLANT AND PROPELLER
ENGINES - 1 ROTAX 912S2 100 HP, 4 CYLINDERS
LIQUID/AIR COOLED, INTEGRATED REDUCTION GEAR
DUAL IGNITION SYSTEM
THROTTLE CONTROL
TUBULAR STEEL ENGINE MOUNT
PROPELLER - GT PROPELLER, 2 BLADE FIX
PROPELLER SPINNER
AIR FILTER
OIL FILTER
OIL AND WATER COOLERS
CARBURETOR HEAT WITH MANUAL CONTROL
THERMOSTAT VALVE WATER AND OIL
AUXILIARY ALTERNATOR
 PRODUCT SUPPORT/DOCUMENTS
MANUFACTURERS FULL TWO YEAR LIMITED WARRANTY
PILOTS OPERATION HANDBOOK
MAINTENANCE MANUAL
PARTS CATALOG
AIRCRAFT LOG BOOK
ENGINE LOG BOOK
 
STANDARD GARMIN AVIONICS PACKAGE
GMA 340 AUDIO PANEL
GNC 255A COM/NAV
GTX 23 TDX REMOTE MOUNTED
ELT 406 MHZ
ANTENNAS:
- TRANSPONDER
- VHF
- ELT
SPEAKERS
MICROPHONE
STICK PUSH-TO-TALK SWITCH-PILOT/COPILOT
MIC& PHONE JACKS-PILOT/COPILOT
 
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