AEROPRAKT-32 Pilot Operating Handbook
A32-240-POH
10
min.
0.15 bar (2.2 psi)
Fuel
antiknock properties
min. RON 90 (min. AKI 91
1
) min. RON 95 (min. AKI 91)
European standard
EN 228 normal, EN 228
super, EN 228 super plus
EN 228 super,
EN 228 super plus
Aviation standard
AVGAS 100 LL
(ASTM D910)
AVGAS 100 LL
(ASTM D910)
Oil:
with RON 424 classification
NOTE: On all issues of engine operation refer to Rotax engine Operator's Manual.
Follow its instructions to ensure safe and efficient operation of the engine.
2.8 Kinds of operation limits
This aircraft is approved for flying day and night, VFR, simple meteorological conditions.
Flight into icing conditions is prohibited.
2.9 Crosswind limitation
Maximum crosswind component for A-32 airplane is 7 m/s (14 kts).
It is highly recommended to choose upwind direction for takeoff and landing with the least
crosswind. It will significantly shorten takeoff and landing distances and increase degree of
safety.
2.10 Markings and placards
The markings and placards are made using pieces of sticking film with inscriptions.
All switches for electrical systems are switched ON when moved UP, and switched OFF
when moved DOWN.
The respective switches' positions are marked with:
and
labels.
Apart from the individual markings of the instruments, controls and switches there are
placards and markings with the following information:
•
Prohibited aerobatic maneuvers:
•
Limit aircraft loading data:
•
Maximum luggage weight:
•
Settings of fuel shut-off valves:
1
Anti Knock Index (RON+MON)/2
ANY AEROBATIC MANOEUVRES
AND INTENTIONAL SPINNING
ARE PROHIBITED
MAXIMUM WEIGHT 450 KG (992 LB)
MINIMUM LOAD IN COCKPIT
–
60 KG (132 LB)
MAXIMUM LOAD IN COCKPIT
WITH FULL FUEL TANKS
–
100 KG (220 LB)
