Bombardier (Boeing Canada/De Havilland)
Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes
Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes
| AD/DHC-8/131 | Spring Tab Mechanism Bolts | 8/2007 |
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| Applicability: | Bombardier Inc. Models DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201,DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-314 and DHC-8-315, Serial Numbers 003 through 611. |
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| Requirement: | 1. Carry out a one-time inspection of the LH and RH elevator spring tab mechanism clamp bolts for correct installation, according to the Accomplishment Instructions of initial issue of Bombardier Service Bulletin (SB) 8-27-106, dated 7 Feb 2006, or later NAA approved revisions.2. If the inspection discovered any bolt that is incorrectly installed, re-install bolt according to the Accomplishment Instructions of the above-noted SB.Note: Transport Canada AD CF-2007-08 dated 4 June 2007 refers. |
| Compliance: | 1. Within 12 months after the effective date of this AD unless already accomplished.2. Prior to further flight after the effective date of this AD. |
| This Airworthiness Directive becomes effective on 2 August 2007. | |
| Background: | It has been discovered in several cases that clamp bolts of the elevator spring tab mechanism were not installed in the correct orientation. Bolts have been found installed with bolt heads on the lower position and in two cases, some bolts, nuts and washers were found to be loose or missing. Detachment of an elevator spring tab mechanism clamp bolt could lead to jamming of the elevator control system and reduced controllability of the aircraft. |
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David Punshon
Delegate of the Civil Aviation Safety Authority
21 June 2007