Bailey Moyes 912 Dragonfly, Руководство по обслуживанию

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FIGURE 2 Knots used for Safety Links
CAUTION: Any increase in Safety Link strength or change of configuration can cause
structural damage and/or allow either or both aircraft to get into unsafe attitudes. Safety Links
must be installed in the configurations outlined within!
NOTE: Automotive GOOP can be applied over knots to help them last longer.
The Tow System, Release and Airframe have been tested in accordance with AC 43.13-2B Chapter 8
804 (d) 1, 2 & 3
NOTE: This Placard must be in the Cockpit and view of the Tow Pilot. “ Glider towline assembly
Safety Link breaking strength not to exceed 130 lbs. and tied in the manner specified in the manuals.”
and “Banner towing is excluded by the Light Sport Rule.” (AC 43.13-2B 807)
NOTE: Placard in Cockpit to indicate Release operation. “Emergency Release, Squeeze Lever to
Release Towline.”
2.4 Angles
Angles tested in accordance with AC 43.13-2B 806 and additionally to a 33 degree cone of
forces.
2.5 Forces
Forces to the Aircraft structure are limited by the Safety Links. These have been tested in both slow
application and quick application of forces.
Tested in the cone of forces to 675 lbs. in accordance with AC 43.13 – 2B 804 d (1)