PARMA-TECHNIK MIKRON III A User Manual

MIKRON III A
TECHNICAL DA'l'A
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Propeller Mount:
Drawing No. 73 47 03 for
variable pitch Ho V 62R or
MTV-l-A propellers
Drawing No. 662 110 for the
fixed pitch V 218 wooden pro-
peller and its modifications
3.3. Performance
Take-off Power
48 kW / 65 hp / 2 600 rpm
Maximum Continuous Power ':
48 kW / 65 hp / 2 600 rpm
Cruising Power
35 kW / 48 hp / 2 350 rpm
3.4. Engine Speed
Maximum Speed
2 860 rpm for 3 sec.
Maximum Continuous Speed
2 600 rpm
Cruising Engine Speed:
2 350 rpm
Idling Speed:
550 rpm
3.5. Fuels and Lubricants
Fuel:
Aviation gasoline, unleaded
72 6ct. MM minimum
Unleaded motor car gasoline,
72 oct. MMminimum
Fuel Pressure: 10 - 25 kPa
Oil:
Motor car engine
oil API pf:.'r-
formance rating
SF minimum.
For viscosity
grades s';e
table on page 25.
Consult use of other oil
grades with the engine man".l-
facturer.'
Engine'oil Quantity:
5.2 litres
4.5 litres - minimum qllantity
of oil in oil tank
6.5 litres - m1n1mum oil tank
capacity
Oil Pressure:
500 kPa maximum
" 3,00' - 400 kPa recommended
oper'ation pressure
150 kPa minimum at idling
speed
Issued 5/92

PARMA-TECHNIK MIKRON III A Specifications

General

Brand	PARMA-TECHNIK
Model	MIKRON III A
Category	Engine
Language	English