AD/BEECH 200/21 Amdt 12 - Fuselage Fatigue Life Limitation (Cth)

AIRWORTHINESS DIRECTIVE On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BEECH 200/21 Amdt 11 and issues the following 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.

Beechcraft 200 (Super King Air) Series Aeroplanes AD/BEECH 200/21 Amdt 12 Fuselage Fatigue Life Limitation 10/2005

Applicability: All models, all serial numbers. Requirement: (i) For serial numbers BB-2 thru BB-1157; BB-1159 thru BB-1166; BB-1168 thru BB-1192; BL-1 thru BL-72; BT-1 thru BT-30; BN-1 thru BN-4:

Retire the life limited fuselage components, in accordance with the requirements of the limitations section of the CASA approved airplane flight manual. Carry out fuselage component structural inspections in accordance with the applicable sections of Chapters 5, 53 and 57 of the Beech Super King Air 200 Series Maintenance Manual 101-590010-19, latest revision.

(ii) For S/N's BT-31 and after; BN-5 and after; BL-73 and after; BB-1193 and after; and S/N BB-1158 and BB-1167:

Retire the life limited fuselage components, in accordance with the Beechcraft Super King Air "Airworthiness Limitations Manual" - P/N: 101-590010-453, latest revision. Carry out fuselage component structural inspections in accordance with the applicable sections of Chapters 5, 53 and 57 of the Beech Super King Air 200 Series Maintenance Manual 101-590010-19, latest revision. Compliance: In accordance with the Requirement Documents above. This Amendment becomes effective on 29 September 2005. Background: The original issue of this AD became effective on 30 September 1977 and promulgated the fuselage life limitations, which were listed in the US Approved Flight Manual and made mandatory by the FAA Type Certificate Data Sheet A24CE.