Tecnam P2002 JF - Page 57

Page 17 2
nd
Edition – Rev 0
03-00
AIRPLANE GENERAL DESCRIPTION
Engine
Manufacturer
Bombardier-Rotax GmbH
Model
912 S2
Type
4 cylinder horizontally-opposed twins with
overall displacement of 1352 c.c., mixed
cooling, (water-cooled heads and air-cooled
cylinders), twin carburetors, integrated
reduction gear with torque damper.
Maximum rating
73.5 kW (98.6 hp) @ 5800 rpm - max. 5 min.
69.0 kW (92.5 hp) @ 5500 rpm - continuous
Propeller
Manufacturer
Hoffmann propeller GmbH
Model
HO17GHM A 174 177C
Number of blades
2
Diameter
1740 mm
Type
Fixed pitch - wood
Fuel
Fuel grade
 EN 228 Super/Super Plus (min RON
95/AKI 91)
 AVGAS 100LL (ASTM D910)
Fuel tanks
2 wing tanks integrated within the wing's
leading edge with fuel strainer located in engine
cowling
Capacity of each wing tank
50 Liters
Total capacity
100 Liters
Usable fuel
99 Liters (49.5 liters each tank)
Oil System
Oil system type
Forced, with external oil reservoir
Oil
Lubricant specifications and grade are detailed
into the “Rotax Operator’s Manual” and in its
related documents.
Oil Capacity
Max. 3.0 liters, min 2.0 liters
Cooling
Cooling system:
Mixed air and liquid pressurized closed circuit
system
Coolant:
Coolant type and specifications are detailed into
the “Rotax Operator’s Manual” and in its
related documents.