pdf Gfa ad 517 issue 1 Popular
By Tim Shirley Tagged in ASW27, ASW27-18, ASW27-18E 992 downloads
gfa ad 517 issue 1.pdf
CHECK OF CONTROL CIRCUIT CLEARANCE INSIDE THE TAIL BOOM TO FIN INTERSECTION
Check of control circuit clearance inside the fuselage tail boom to fin intersection. One ASW 27 owner reported slight jamming in one flight and abandoned the take-off. Rubbing of the 90º lever with its attached mass balance lead weights and connecting bolt against the cut-out of the lower fin rib has been determined as the only likely cause. Alexander Schleicher Technical Note ASW 27 No. 5 which herewith becomes part of this AD.
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