Powerplant; Fuel System - Tecnam P2002-JF Flight Manual

POWERPLANT

ENGINE
Manufacturer
Model
Type
Maximum rating
Max oil consumption Max: 0.1 litres/hour
PROPELLER
Manufacturer
Model
N° of blades
Diameter
Type

FUEL SYSTEM

The system is equipped with two aluminium fuel tanks integrated within the wing
leading edge and accessible for inspection through dedicated covers. Capacity of
individual tank is 50lt and the total fuel capacity is 100lt. A multi-position fuel
selector valve is located into the cabin. It is possible to select the following fuel
feeding: LEFT (means a left tank feeding), RIGHT (means a right tank feeding)
and a third OFF position which could not be accidentally operated. A strainer cup
with a drainage valve (Gascolator) is located beneath the cabin, just behind the
firewall. Fuel level indicators for each tank are located on instrument panel. Fuel
feed is through an engine-driven mechanical pump and also through an electric
pump that supplies adequate engine feed in case of main pump failure. Figure 7-3
illustrates the schematic layout of the fuel system.
st th
1 Edition – 29 March 2004
F
LIGHT MANUAL
Bombardier-Rotax GmbH
ROTAX 912 S2
4 stroke, horizontally-opposed 4 cylinder, mixed air and
water cooled, twin electronic ignition, forced lubrication.
98.6hp (73.5kW) @ 5800 rpm/min (2388 rpm/min. prop).
Gear reduction ratio - 2.4286:1
Hoffmann Propeller
HO17GHM A 174 177C
2
1740 mm (no reduction permitted)
wood, fixed pitch
P2002-JF
S E C T I O N 7
Systems
7-6