Document ID: chunk:federal_register_of_legislation:F2009L03771:body:0:p1
Version: federal_register_of_legislation:F2009L03771
Segment Type: other
Provision Reference: 
Character Range: 0–3083

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/AT 800/9 Amdt 3 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.

Airtractor 800 Series Aeroplanes
AD/AT 800/9 Amdt 4  Engine Mount  11/2009

Applicability:  Model AT-802 and AT-802A aircraft, serial numbers 0001 through 0227.
Requirement:       1. For engine mounts without gussets installed, inspect the engine mount in accordance with Snow Engineering Co. SL No. 253 Revision C, dated
                   17 April 2008:

                     a. For aircraft with less than 5,000 hours time in service; at the initial and repetitive times specified in the Compliance section.

                     b. For aircraft with 5,000 hours time in service or more; at the initial and repetitive times specified in the Compliance section.

                   2. For engine mounts with gussets installed, inspect the engine mount in accordance with Snow Engineering Co. SL No. 253 Revision C, dated
                   17 April 2008:

                     a. For aircraft with less than 5,000 hours time in service; at the initial and repetitive times specified in the Compliance section.

                     b. For aircraft with 5,000 hours time in service or more; at the initial and repetitive times specified in the Compliance section.

                Note:  FAA AD 2009-11-05 Amdt 39-15915 refers.
Compliance:          1. a. Initially, upon accumulating 1,300 hours time in service or within the next 100 hours time in service after 30 August 2007, whichever occurs later.  Repetitively thereafter at intervals not to exceed 300 hours time in service.

                     1. b. Initially, upon accumulating 5,000 hours time in service or within the next
                     10 hours time in service after 30 July 2009, or within the next 100 hours time in service from the last inspection performed, whichever occurs later.  Repetitively thereafter at intervals not to exceed 100 hours time in service.

                     2. a. Initially, upon accumulating 1,300 hours time in service or within the next 100 hours time in service after 30 July 2009, whichever occurs later.  Repetitively thereafter at intervals not to exceed 300 hours time in service.

                  2. b. Initially, upon accumulating 5,000 hours time in service or within the next
                  10 hours time in service after 30 July 2009, or within the next 100 hours time in service from the last inspection