AD/SF340/111 - State of Design Airworthiness Directives (Cth)

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 39.001(1) of CASR 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.

SAAB SF340 Series Aeroplanes AD/SF340/111 State of Design Airworthiness Directives 16/2010

Applicability: SAAB 340 aircraft. Requirement: 1. Determine the applicability of the Swedish Airworthiness Directives (SAD) listed in Table 1.

2. If it is determined that an SAD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that SAD or later EASA-approved revision.

Service Bulletins approved by EASA as Alternative Methods of Compliance (AMOC) to the SADs listed in Table 1 are considered acceptable for compliance with the equivalent requirements of this Airworthiness Directive. Table 1 SAD Issue Date Title 1-038 1990-06-29 Yaw oscillations 1-016 1987-06-18 Inspection of cabin fluorescent lighting system 1-013 1986-01-31 Cabin fluorescent lighting system 1-009 1985-08-15 Engine controls - replacement and sealing 1-002 1984-09-27 Engine and engine-performance monitoring 1-001 1984-09-12 Inspection and replacement of certain parts Note 1: Swedish Airworthiness Directives may be accessed via the internet at the following URL: http://ad.easa.europa.eu/