Alsim al250 - Fuel Capacity and Limitations; Aircraft Weight Limits; Centre of Gravity Limits; Aircraft Manoeuvre Limitations

Limitations
FUEL LIMITATIONS
AL250 Flight Manual
MEP
1-6 FUEL LIMITATIONS
Total capacity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .110 U.S. Gal.
Unusable fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2 U.S. Gal.
The unusable fuel for this airplane has been determined as 1.0 gallon in each nacelle in critical
flight attitudes.
Usable fuel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 108 U.S. Gal.
The usable fuel in this airplane has been determined as 54 gallons in each nacelle or a total
of 108 gallons.
1-7 WEIGHT LIMITS
Maximum take-off weight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3800 lbs
1-8 CENTRE OF GRAVITY LIMITS
The centre of gravity of the ALSIM AL250 is variable within a range of 0% to 100% (0% is
maximum forward CG and 100% is maximum aft CG).
1-9 MANOEUVRE LIMITS
This is a normal category aircraft. No acrobatic manoeuvres (including spins) approved.
Avoid abrupt manoeuvres.
1-10 GYRO SUCTION LIMITS
The operating limits for the suction system are 4.5 to 5.2 inches of mercury for all operations
as indicated by the gyro suction gauge.
Figure 1.6: Gyro Pressure Gauge
Rev. 1.8 © 2021 ALSIM - All Rights Reserved 1-6