Document ID: chunk:federal_register_of_legislation:F2006B09869:body:0
Version: federal_register_of_legislation:F2006B09869
Segment Type: other
Provision Reference: 
Character Range: 0–860

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

 Fokker F50 (F27 Mk 50) Series Aeroplanes

 AD/F50/42
 Amdt 1

 External Power Connection Relay Fitment 5/91

 Applicability: All F 27 MK50 aircraft as listed in the requirement document.

            Requirement: Action in accordance with the technical requirements of RLD Airworthiness Directive 90-137 dated 14 December 1990.

Note: Fokker SB F50-24-015 dated 29 November 1990 also refers.

 Compliance: As specified in the requirement document.

 Background: Reports indicate that the potential exists for serious damage to occur to contactors and circuit breakers during ground power to aircraft power change-over.

            Note: Amendment 1 to this AD is issued to clarify the compliance statement.