CTHIn ForceLegislation
AD/750XL/11 - Rudder Trim Tab Pivot
Pacific Aerospace 750XL Series AeroplanePacific Aerospace 750XL Series Aeroplanes
Start here
Get a plain-English read of Pacific Aerospace 750XL Series Aeroplane
Turn the raw legal text into a practical explanation grounded in AD/750XL/11 - Rudder Trim Tab Pivot.
Pacific Aerospace 750XL Series Aeroplanes
| AD/750XL/11 | Rudder Trim Tab Pivot | 6/2007 |
|---|
| Applicability: | Model 750XL aircraft without modification PAC/XL/0267 incorporated. |
|---|---|
| Requirement: | 1. Inspect the rudder trim tab upper pivot in accordance with the instructions in Pacific Aerospace Limited Mandatory Service Bulletin (MSB) PACSB/XL/023.If there is any lateral movement of the bush, incorporate modification PAC/XL/0267 in accordance with MSB PACSB/XL/023 and PAC Drawing No. 11-03131.Note 1: Modification PAC/XL/0267 comprises removing the upper bush part number 11-33119-1 and installing upper bearing part number 11-33121-1 in accordance with PAC Drawing No. 11-03131. This modification constitutes terminating action to the requirements of this Directive.2. Modify the rudder trim tab upper pivot in accordance with MSB PACSB/XL/023 and PAC Drawing No. 11-03131.Note 2: NZ CAA AD DCA/750XL/11 refers. |
| Compliance: | 1. Within 150 hours time in service after 7 June 2007. Thereafter at intervals not to exceed 150 hours time in service; until Requirement 2 is accomplished.2. Within 450 hours time in service or 24 months after 7 June 2007, whichever occurs first. |
| This Airworthiness Directive becomes effective on 7 June 2007. | |
| Background: | Wear has been detected in the rudder trim tab upper pivot hole in the rudder rib. This Directive requires inspections until eventual replacement of the trim tab upper pivot bush with a bearing. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
24 April 2007