Summary
The FAA is revising the applicability of the function and reliability flight testing requirements to include all part 23 turbine- powered airplanes weighing 6,000 pounds or less. Revising the applicability is necessary because advancements in aviation technology have invalidated the reasons for excluding these airplanes. This revision is intended to improve aviation safety for these airplanes.
Directive Details
AD Number
FAA-2010-0218
Document Number
2011-26955
Type
Rule
Publication Date
October 18, 2011
Effective Date
December 19, 2011
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2010-0218
Topics
Official Documents
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