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Gfa ad 305 issue 1

MODIFICATIONS, INCLUDING RUDDER SYSTEM DAMPER, RUDDER HINGE STIFFENING, AND AILERON MASS BALANCE

GFA AD 296 restricted the Grob G 109B to a VNE of 100 knots as a temporary flutter limitation. Grob TM 817-20 (which forms part of this AD) has been issued outlining rudder and aileron system modifications which, when fully incorporated, will allow AD 296 restriction to be lifted returning the G 109B to its normal operational speed limits.