Weight And Center Of Gravity Limits; Occupancy; Fuel - Pipistrel ALPHA Trainer LSA Pilot Operating Handbook

SECTION 2
LIMITATIONS

2.6 WEIGHT AND CENTER OF GRAVITY LIMITS

Maximum takeoff weight
Maximum landing weight
Design empty weight (typical)
Design useful load
Most forward CG
Most rearward CG
NOTE The reference datum is wing's leading edge at root.
:

2.7 OCCUPANCY

Max. Occupancy
Maximum weight / per seat
Minimum weight solo pilot
Maximum baggage weight *
* 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
Total usable fuel (all flight condi-
tions)
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)
PAGE
2-6
ALPHA Trainer LSA
Pilot Operating Handbook
550 kg / 1212 lbs
550 kg / 1212 lbs
279 kg / 615 lbs
271 kg / 597 lbs
25 % MAC
267 mm or 10 7/16"
35 % MAC
355 mm or 13 31/32"
Pilot and 1 Passenger
110 kg / 242 lbs, 200 kg/ 440 lbs
total
55 kg / 121 lbs
10 kg / 22 lbs
50 liters / 13.2 US gal
36 kg / 79 lbs
48 liters / 12.7 US gal
34.5 kg / 76 lbs
POH-162-00-40-001
PAGE REV. 0