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SPECIFICATIONS
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Rotax 912 UL 80
HP
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Rotax 912 ULS
100 HP
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Material
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6061-T6 aluminum
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Seating
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2, side-by-side
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Wing type
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high with 2 struts
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Wing span
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29' 5"
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Wing chord
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57"
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Wing area
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139.5 s.f.
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Aspect
ratio
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6.3:1
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Wing loading
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8.8 lbs./s.f.
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Flaps
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0 - 20 - 40
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Landing gear
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fixed, tricycle
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Wheel track
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5' 7"
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Length
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21' 4"
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Height
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9' 1"
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Cabin width
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42"
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Gross weight
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1234 lbs.
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Power
ratio
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12.3
- 10.1 lbs./hp
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Forward C of G
limit
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30%
MAC
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Rear C of G
limit
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38.5%
MAC
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Limit
load factor
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+6/-3g
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Number of
kits sold
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800+
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Empty weight
- lbs *
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598
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607
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Useful load - lbs.
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634
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625
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Fuel capacity - US gal.
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21
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21
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Payload with max. fuel
- lbs. **
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510
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501
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PERFORMANCE
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Rotax 912 UL 80
HP
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Rotax 912 ULS
100 HP
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Stall speed full flaps
(Vso) - mph
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28
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28
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Approach speed (Vref) - mph
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36
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36
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Maneuvering speed (Va) - mph
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85
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85
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Cruise speed -
mph (standard tires)
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90
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96
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Max speed - mph
(standard tires)
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100
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110
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Never exceed speed (Vne) - mph
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125
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125
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Take off run at 1000
lb. - ft
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114
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98
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Landing roll at 1000 lb. - ft.
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160
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Climb rate-
ft/min
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960
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1320
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Best rate of climb
speed - mph
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47
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53
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Best angle of climb
speed - mph
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45
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47
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Glide ratio at
60 mph
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12:1
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Fuel consumption at 75%
power - gph
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5.1
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5.3
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Range (max endurance) - miles
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425
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410
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