AD/SD3-60/36 Amdt 1 - MLG Rear Pintle Pin Bush (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/SD3-60/36 and issues the following AD under subregulation 39.1 (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.

Short SD3-60 Series Aeroplanes

AD/SD3-60/36 Amdt 1

MLG Rear Pintle Pin Bush 12/2004

Applicability: Model SD3-60 aircraft.

Requirement: 1. Inspect the main landing gear rear pintle pin assemblies for correctly applied sealant in accordance with Shorts Service Bulletin SD360-32-37 original issue, or later EASA approved revision (refer to Accomplishment Instructions, paragraph 2A of Messier-Dowty Service Bulletin 32-70SD Revision 1).

2. If the sealant is incorrectly applied, perform a magnetic flaw detection inspection of the rear pintle pin fork ends in accordance with Shorts Service Bulletin SD360-32-37 original issue, or later EASA approved revision (refer to Accomplishment Instructions, paragraph 2B of Messier-Dowty Service Bulletin 32-70SD Revision 1).

If pintle pin fork ends are found cracked, before further flight, replace with a serviceable part that has been inspected in accordance with this Directive.

Note: UK CAA AD G-2004-0022 refers.

Compliance: 1. At the next "B" check after 25 November 2004, but no later than 3 months after the effective date of this Directive.