Summary
This action supersedes emergency airworthiness directive (AD) 2011-05-51 that was sent previously to all known U.S. owners and operators of the products listed above. That AD requires inspecting the fuel ejector in the body of the fuel ejector assembly for proper installation by checking that the circlip is properly seated in its groove. That AD was prompted by three reports of incorrectly assembled low-pressure fuel system ejectors; with one of them resulting in an uncommanded engine in-flight shutdown. This AD requires the same actions and compliance times as the emergency AD, after receipt of the emergency AD, and expands the AD applicability by including helicopters having one or two affected engines and experiencing no starting difficulties. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Directive Details
AD Number
FAA-2011-0141
Document Number
2011-4832
Type
Rule
Publication Date
March 4, 2011
Effective Date
March 9, 2011
Affected Manufacturer
Turbomeca Model Arriel 1E2, 1S, and 1S1 Turboshaft
Criticality
critical
Emergency
Yes
Docket ID
Docket No. FAA-2011-0141
Topics
Official Documents
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