Document ID: chunk:federal_register_of_legislation:F2006B09788:body:0
Version: federal_register_of_legislation:F2006B09788
Segment Type: other
Provision Reference: 
Character Range: 0–716

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

 Fokker F28 Series Aeroplanes

AD/F28/53 Cargo Door Hinges  8/87 TX

 Applicability: All models.

 Requirement: 1. Remove forward, centre and aft cargo door hinges.

2.    Remove hinge wire and disassemble hinge.

3.    Inspect hinge lugs for corrosion and cracking.

            Compliance: Unless accomplished within the pat six months within 50 hours time in service after 9 June 1987.

            Background: The Department has received reports of intergranular corrosion and cracking of the cargo door hinges. In one case nearly half of the lugs were cracked.