AD/BAe 146/121 - Lift Spoiler Actuator Life Limits (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.

British Aerospace BAe 146 Series Aeroplanes AD/BAe 146/121 Lift Spoiler Actuator Life Limits 8/2006

Applicability: BAe 146 and AVRO 146-RJ aeroplanes. Requirement: 1. Determine the life of each lift spoiler actuator/jack, part number P308-45-0002, P308-45-0102 or P308-45-0202, in accordance with Paragraph 1.D of Service Bulletin 27-178 Revision 0 or later approved revision.

2. Replace each lift spoiler actuator/jack part number P308-45-0002, P308-45-0102 or P308-45-0202, in accordance with Paragraph 2.A of Service Bulletin 27-178 Revision 0 or later approved revision.

Note: EASA AD 2006-0138 dated 23 May 2006 refers. Compliance: 1. Within 30 days after the effective date of this AD.

2. Prior to the part accumulating 55,000 flight cycles or before 1 September 2007, whichever occurs later after the effective date of this AD. This Airworthiness Directive becomes effective on 3 August 2006. Background: The life limitation relating to the P308-45 series of lift spoiler jacks was originally qualified to 55000 flight cycles and there is no new data to support an increase to this figure.