Tecnam P92 Echo MK2 - Powerplant; Engine; Propeller; Oil System

P92 LSA
Flight Manual
Rev.0
16
1.4 Powerplant
1.4.1 Engine
Manufacturer
Bombardier Rotax GmbH
Model
912 ULS2
Engine 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 power (at declared rpm)
73.5kW (98.5hp) @5800rpm (max.5’)
69.0kW (92.5hp) @5500rpm (cont.)
1.4.2 Propeller
Manufacturer
Sensenich
Model
W68T2ET-70J
Number of blades:
2
Diameter
1730 mm (no reduction allowed)
Type
Fixed pitch – wood
1.4.3 Oil System
Oil system
Forced type with external reservoir
Oil
Lubricant specifications and grade are detailed into the
“Rotax Operators Manual” and in its related documents.
Oil capacity
Max. 3 litres – min. 2.0 litres
1.4.4 Cooling
Cooling system
Mixed air and liquid pressurized closed circuit system
Coolant liquid
Coolant type and specifications are detailed into the
“Rotax Operator’s Manual” and in its related documents.
1.4.5 Fuel
Fuel tanks
Two wing tanks integrated within the wing’s leading
edge. Equipped with finger strainers outlet and with
drain fittings.
Capacity of each wing tank
45 litres
Tanks overall capacity
90 litres
Approved fuel
MOGAS ASTM D4814
MOGAS EN 228 Super/Super Plus (MIN RON 95)
AVGAS 100LL (ASTM D910)