AD 2016-11-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | AEROTECHNIK s.r.o. | Various | Airworthiness Directives; EVEKTOR, spol. s.r.o. Gliders |
| aircraft | Aviat | Various | Airworthiness Directives; EVEKTOR, spol. s.r.o. 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 021N, for damage and material hardness following the procedures in AEROTECHNIK CZ s.r.o. Mandatory Service Bulletin SEH 13-005a. Replace the fitting if it does not meet the specified hardness requirements.
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 2000-20-12)
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Affected Aircraft
EVEKTOR, spol. s.r.o. Models L 13 SEH VIVAT and L 13 SDM VIVAT 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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