2-6
PAGE
ALPHA Trainer LSA
Pilot Operating Handbook
POH-162-00-40-001
PAGE REV. 0
SECTION 2
LIMITATIONS
2.6 WEIGHT AND CENTER OF GRAVITY LIMITS
Maximum takeo weight 550 kg / 1212 lbs
Maximum landing weight 550 kg / 1212 lbs
Design empty weight (typical) 279 kg / 615 lbs
Design useful load 271 kg / 597 lbs
Most forward CG
25 % MAC
267 mm or 10 7/16”
Most rearward CG
35 % MAC
355 mm or 13 31/32”
NOTE
: The reference datum is wing’s leading edge at root.
2.7 OCCUPANCY
Max. Occupancy Pilot and 1 Passenger
Maximum weight / per seat
110 kg / 242 lbs, 200 kg/ 440 lbs
total
Minimum weight solo pilot 55 kg / 121 lbs
Maximum baggage weight * 10 kg / 22 lbs
* only when solid baggage compartment (p/n 6023077) is installed and CG limita-
tions are respected
2.8 FUEL
Approved fuels include MOGAS or AVGAS 100LL, as per Rotax specifica-
tion, with max. 10% ethanol and the following antiknock properties: min.
RON 90 (min. AKI 87)
Total fuel capacity
50 liters / 13.2 US gal
36 kg / 79 lbs
Total usable fuel (all flight condi-
tions)
48 liters / 12.7 US gal
34.5 kg / 76 lbs
NOTE: Operation with leaded fuels (including AVGAS) results in shorter oil
filter replacement intervals of 50 hours.
NOTE: Unusable fuel is 2 liters (0.5 US gal)
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