pdf Gfa ad 221 issue 1 Popular
By Tim Shirley Tagged in SZD-36, SZD-36A, SZD-39 985 downloads
gfa ad 221 issue 1.pdf
LONGITUDINAL CRACKING OF THE LEADING EDGES OF THE WING AND HORIZONTAL TAILPLANE
Applicable to the SZD-36, SZD-36A and SZD-39 Cobra glider. PZL Bulletin BR-004/80 details the inspection for and repair of cracks found, in the leading edges. Cracking is largely caused by exposure of the glider to moisture under inadequate storage conditions.
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