pdf Gfa ad 305 issue 1 Popular
By Tim Shirley Tagged in G109B 263 downloads
gfa ad 305 issue 1.pdf
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.