Airworthiness Directives; Airbus Model A310-200 and -300 Series Airplanes
airworthiness · Rule · Final rule. · Published 2006-05-16 · Effective 2006-06-20 · 71 FR 28254
Document
Document number
06-4503
Federal Register citation
71 FR 28254
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A310-200 and -300 Series
Publication date
2006-05-16
Effective date
2006-06-20
FAA docket
Docket No. FAA-2006-24104
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A310-200 and -300 series airplanes. This AD requires repetitive inspections for cracking of the flap transmission shafts, and replacing the transmission shafts if necessary. This AD also provides an optional terminating action for the repetitive inspections. This AD results from reports of longitudinal cracks due to stress corrosion in the transmission shafts between the power control unit (PCU) and the torque limiters of the flap transmission system. We are issuing this AD to detect and correct cracking of the flap transmission shaft, which could compromise shaft structural integrity and lead to a disabled flap transmission shaft and reduced controllability of the airplane.