Document ID: chunk:federal_register_of_legislation:F2006B03622:body:0
Version: federal_register_of_legislation:F2006B03622
Segment Type: other
Provision Reference: 
Character Range: 0–1090

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 18 Series Aeroplanes

AD/BEECH 18/23 Pilot Seats - Reinforcement 1/84

 Applicability: All model 18 aircraft equipped with A.M.I. seats model 716-1,-2,-11, -12, -21 and -22
            and Model 865-1 to -9 and-11.

            Requirement: Reinforce pilot seat frame assembly P/N 865J10005-1 by installation of A.M.I. Industries, Inc., seat frame brace kit P/N 865K90000-1 I.A.W. A.M.I. Industries, Inc., service bulletin No 25-10-865-01, dated 31 January, 1983.

            Note: FAA AD 83-21-06 refers.

 Compliance: Unless previously accomplished, before 30 April 1984.

            Background: A case occurred where failure of the pilots seats during a survivable emergency landing contributed to occupant injury. Subsequent T.S.O. tests verified failure of the seat frame at loads below the 9g. forward requirement.

                   Federal Register of Legislative Instruments F2006B03622