# Airworthiness Directives; LET Aeronautical Works Model L-13 “Blanik” Sailplanes
> **Rule** · Final rule. · Published 2000-10-13 · Effective 2000-11-27 · 65 FR 60845
## Document
- **Document number:** 00-25548
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 60845
- **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
- [Federal Register document](https://www.federalregister.gov/documents/2000/10/13/00-25548/airworthiness-directives-let-aeronautical-works-model-l-13-blanik-sailplanes)
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