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MIKRON III
A
TECHNICAL
DA'l'A
,.7
--------~--------------------------------------------------"---
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
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