AD/ROTAX/8 - Ignition Unit Stator Assembly (Cth)

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES

Rotax Piston Engines

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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/ROTAX/8 Ignition Unit Stator Assembly 5/2000 TX

Applicability: Rotax 912 and 914 series engines as follows:

Engine Series Serial Number Range

912 A 3 792.541 up to 4 410.366

912 F 4 412.502 up to 4 412.791

914 F 4 420.002 up to 4 420.157

Requirement: 1. Inspect the ignition stator assembly and if necessary repair any discrepancies detected during the inspection, in accordance with Section 3.1 of Rotax Aircraft Service Bulletin SB-912-026 Revision 3 or SB-914-014 Revision 3 both dated December 1999, as appropriate.

2. Replace the stator assembly in accordance with Section 3.2 of SB-912-026 Revision 3 or SB-914-014 Revision 3, as appropriate.

Replacement of the stator assembly in accordance with previous issues of the service bulletins is considered terminating action for this directive.

Note: Austro Control (Austria) AD No 98 refers. COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES