Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
airworthiness · Rule · Final rule. · Published 2007-03-15 · Effective 2007-04-19 · 72 FR 12072
Document
Document number
E7-4382
Federal Register citation
72 FR 12072
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-03-15
Effective date
2007-04-19
FAA docket
Docket No. FAA-2006-26516
Abstract
The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A318-100 and A319-100 series airplanes, Model A320-111 airplanes, and Model A320-200, A321-100, and A321-200 series airplanes. That AD currently requires repetitive inspections of the upper and lower attachments of the trimmable horizontal stabilizer actuator (THSA) to measure for proper clearance and to detect cracks, damage, and metallic particles. The existing AD also requires corrective actions, if necessary, and reports of inspection findings. This new AD shortens the repetitive interval for inspecting the upper THSA attachment. This AD results from new test results on the secondary load path, which indicated the need to shorten the repetitive interval for inspecting the upper THSA attachment. We are issuing this AD to detect and correct failure of the THSA's primary load path, which could result in latent (undetected) loading and eventual failure of the THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control of the airplane.