Document ID: chunk:federal_register_of_legislation:F2006B09082:body:0
Version: federal_register_of_legislation:F2006B09082
Segment Type: other
Provision Reference: 
Character Range: 0–1266

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

 DHC-3 (Otter) Series Aeroplanes

 AD/DHC-3/32
 Amdt 1

 Utility Seat Forward Leg Positive Lock Installation 11/88

 Applicability: All models with side folding cabin utility seats.

 Requirement: Action in accordance with De Havilland Canada SB 3/42 Rev A.

             Compliance: 1. Prior to the issue of the next Maintenance Release after 31 December 1987 and thereafter at each inspection for Maintenance Release issue until modified as detailed in SB 3/42 Rev A.

             2. After each time the seats are moved from stowed to deployed position, until modified as above.

            Note 1. This Compliance Para 2 inspection may be accomplished by the Pilot-In- Command, in which case the precise AD reference shall be entered in a certification made on the Maintenance Release.

            Note 2. Canadian AD CF-85-03 R1 and FAA AD 88-15-08 refer.

            Background: A sideways force applied to a utility seat forward leg could result in the leg being disengaged from the keyhole slot in the seat rail. Amendment 1 requires repeat inspection each time seats are deployed. SB 3/42 Rev A refers.