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Airworthiness Directives; LET Aeronautical Works Model L-13 “Blanik” Sailplanes

airworthiness · Rule · Final rule. · Published 2000-10-13 · Effective 2000-11-27 · 65 FR 60845

Document

Document number
00-25548
Federal Register citation
65 FR 60845
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-10-13
Effective date
2000-11-27
FAA docket
Docket No. 99-CE-91-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all LET Aeronautical Works (LET) Model L-13 "Blanik" sailplanes. This AD requires you to inspect the tail-fuselage hinge for strength requirements and damage, and also requires you to replace any hinge with damage or that does not meet strength requirements. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Czech Republic. The actions specified by this AD are intended to detect and correct any tail-fuselage hinge that is damaged or has inadequate material characteristics. Any tail-fuselage hinge with damage or inadequate material characteristics could fail and result in loss of controlled flight.

Source

Authoritative
Federal Register document
Machine
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