Document ID: chunk:federal_register_of_legislation:F2014L01088:body:0:p2
Version: federal_register_of_legislation:F2014L01088
Segment Type: other
Provision Reference: 
Character Range: 2860–3600

of sufficient magnitude to leave witness marks on the fabric covering, or otherwise obvious damage to a wing. In the case of such an event, both the top and bottom wings are to be inspected on the side of the aircraft where the impact occurred.
                3. The action in Requirement 3 must be taken in accordance with Part 4B – Defect Reporting of CAR 1988.
                The effective date of this AD is 14 August 2014.
Background:  This AD ensures the requirement to conduct visual inspections of the entire internal wooden structure of the aircraft's flying surfaces to ensure the continued airworthiness of all variants of DH 82 and DH 82A aircraft.

Nicholas Ward
Delegate of the Civil Aviation Safety Authority
11 August 2014