Gfa ad 558 issue 2
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gfa ad 558 issue 2.pdf
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CRACKING OF REAR PLATE OF PROPELLER MOUNT
This AD was issued as a result of cracks found in one aircraft. Following the discovery of cracks in several other aircraft the AD has been revised. The content of the AD is unchanged except that periodically recurring inspections are now required. DG-Flugzeugbau Technical Note No 826/42 and pages 0.3, 2A and Diagram 6 of DG-400 Maintenance Manual form part of this AD.