AD 2016-11-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | LET Aeronautical Works | Various | Airworthiness Directives; BLANIK LIMITED Gliders |
| aircraft | Aviat | Various | Airworthiness Directives; BLANIK LIMITED Gliders |
Unsafe Condition
Insufficient material strength of the tail-fuselage attachment fitting, which could lead to detachment of the tail from the fuselage and consequent loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the tail-fuselage attachment fitting, part number A 102 021 N, for insufficient material strength. If necessary, replace the fitting with a new one.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 60 days after November 27, 2000 (effective date retained from AD 2000-20-11).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BLANIK LIMITED Models L-13 Blanik and L-13 AC Blanik gliders, all serial numbers, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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