Document ID: chunk:federal_register_of_legislation:F2006B10436:body:0
Version: federal_register_of_legislation:F2006B10436
Segment Type: other
Provision Reference: 
Character Range: 0–1006

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

 British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/155 Fuselage Fluid Drainage 10/96

 Applicability: BAe 125 series 800A, series 800B, and Hawker 800 aircraft.

            Requirement: Action in accordance with Hawker Mandatory Service Bulletin 53-82-3566G Revision 3.

            Note: FAA AD 96-12-16 Amdt 39-9659 refers.

            Compliance: Unless Modification 253566G is already installed in accordance with a previous issue of the Requirement document, including a functional test to determine if a bolt fouls the flap control system (in accordance with para. 2.A.(18) of the SB Accomplishment Instructions); before 31 December 1996.

            Background: Reports were received of restricted control of the ailerons due to water accumulation that froze at an aileron pulley in the lower area of the fuselage, aft of the wing rear spar.