Maximum Cylinder Head Temperature: . . . . . . .
150 deg.C
Maximum Oil temperature
. . . . . . . . . . . . . . . . . . . 140 deg. C
Oil Pressure, Minimum
. . . . . . . . . . . . . . . . . . . . .
1.5 bar
Maximum . . . . . . .. . . . . . . . . . . . . 5 bar
Fuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . .
0
. 15 - 0.4 bar
Fuel grade.. . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . .
Premium grade leaded gas, according to
DlN1600, O N O R M C1103 E U R O
SUPER ROZ 95 unleaded, according to
DIN51603, ONORM C 1101
Oil grade . . . . . .
. . . . . . . .
. . . . . . . . . . . . . . . . . . . .
SAE 20 W
50 or SAE
30 High
performance automotive oil API, S6,
Mobil 1, 15 W50, NO AVIATION OIL
Propeller manufacturer
Propeller model
Propeller Blade angle - see propeller manual
Powerplant instrument markings:
Powerplant instrument markings and their colour code are shown below:
Instrument
Red line
Minimum
limit
Green Arc
Yellow Arc
Red line
Normal operating Caution range Maximum limit
Tachmeter
2 500 -5 500
5 500 - 5 800
5 800
Oil TemDerature deg.C
50
90-
110
110- 140
140
Cyl. head temp. deg.C
150
Fuel
(bar)
pressure
0.15
0.4
Oil
(bar)
pressure
1.5
4 - 5
5
Weight:
Basic Empty weight.....................................................
760
kg
.
Maximum take-off weight .......................................... 450 kg
Maximum landing weight.. ......................................... 450 kg
Maximum cockpit weight .......................................... .190 kg
Minimum cockpit weight........................................... .55 kg
Maximum weight in Baggage compartment.. ............ .I8 kg
Centre of gravity:
Standard entre of gravity position for empty aircraft is 21.6 % MAC ( 3 10 mm from
reference datum - leading edge of slats)
Allowable Range: 20 - 35 % (286 mm to 500 mm)
See section 6 Weight & Balance for details
