AD/GAF-N22/74 Amdt 1 - Left Wing Aft Wing Break Electrical Connector (Cth)

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

GAF N22 and N24 Series Aeroplanes

AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/GAF-N22/74 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

AD/GAF-N22/74 Amdt 1

Left Wing Aft Wing Break Electrical Connector

11/2001

Applicability: Nomad N22 and N24 series aeroplanes, line sequence numbers as listed in Aerospace Technologies of Australia (ASTA) Nomad Service Bulletin (SB) ANMD-57-13 Revision 1 dated 14 August 2001.

Requirement: 1. Inspect the left wing aft wing break electrical connector in accordance with ASTA Nomad SB ANMD-57-13 Revision 1.

2. If any contamination is found during the Requirement 1 inspection clean the connector in accordance with ASTA Nomad SB ANMD-57-13 Revision 1.

3. If any arcing damage, deposits between contacts or looseness of contacts is found during the Requirement 1 inspection incorporate either Modification N875 (N22 aeroplanes) or Modification N876 (N24 aeroplanes) in accordance with ASTA Nomad SB ANMD-57-13 Revision 1.

Incorporation of Modification N875 or N876 is considered terminating action for the Requirement 1 repetitive inspections.