AirBorne WindSports FUN 160, Руководство владельца и по обслуживанию

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A irBorne WindSports
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Fun MANUAL
Issue Date: 1 October 2001 Page 22
Fun 190
GLIDER MODEL: Fun 190
MANUFACTURED BY: AIRBORNE WINDSPORTS Pty Ltd
NOTE: These specifications are intended only as a guideline for determining whether a given glider is a
certified model and whether it is in the certified configuration.
Be aware, however, that no set of specifications, however detailed, can guarantee the ability to determine
whether a glider is the same model, or is in the same configuration as was certified, or has those
performance, stability, and structural characteristics required by the certification standards. An owner’s
manual is required to be delivered with each HGMA certified glider, and it is required that it contain additional
airworthiness information.
Metric Imperial
Weight of glider with all essential parts and without cover bags and non essential
parts.
23.0 kg 51 lbs
Leading Edge Dimensions
Nose Plate anchor hole to crossbar plate attachment hole 3530 mm 138.98”
Nose Plate anchor hole to rear sail attachment point 5810 mm 228.74”
Outside diameter at nose 50 mm 1.97”
Outside diameter at cross bar 52 mm 2.05”
Outside diameter at rear sail attachment point 50 mm 1.97”
Crossbar Dimensions
Overall pin to pin length from leading edge attachment point to hinge
bolt at glider centre line
3100 mm 122.05”
Largest outside diameter 62 mm 2.44”
Keel dimensions
2
The cross bar centre load bearing pin 1455 mm 57.28”
The pilot hang loop Fwd
Rear
1600 mm
1650 mm
62.00”
64.96”
Sail Dimensions
Chord length at 3 ft outboard of centre line 2280 mm 89.76”
Chord length at 3 ft inboard of tip 1225 mm 48.23”
Span (extreme tip to tip) 10100 mm 397.63”
Location of Information Placard Cross Bar
Location of Test Fly Sticker Front Keel
Recommended Pilot Hook in Weight Range 70-120 kg 154-265 lbs
Minimum Recommended Pilot Proficiency Novice Novice
NB: Conversions * 0.4536 kg/pound * 25.4 mm/inch
2
least and greatest allowable distances, whether variable through tuning or through in-flight variable geometry, from the line
joining the leading edge nose bolts to: