AircraftDirectives
Aircraft model

Evektor L 13 Vivat

EVEKTOR, spol. s.r.o. (formerly Aerotechnik)

Airworthiness Directives
3
Service Bulletins
0
Last live check
2026-08-173 of 3 re-verified
What this page is: a restatement of what the official Federal Register and manufacturer records show as of the date listed below each item. It is not a determination that any specific aircraft or engine is, or is not, in compliance. Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible for maintaining airworthiness and required records. Always verify against the official FAA and manufacturer sources linked below before making a maintenance or airworthiness decision.

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Airworthiness Directives

3 records · 1 superseded record nested above
AD

2016-11-12

FR doc 2016-12601 · 81 FR 37124

AD 2016-11-12Published 2016-06-09Effective 2016-07-14

EVEKTOR, spol. s.r.o. Gliders

Supersedes 2000-20-12 — see below

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2000-10-17
AD

2000-20-12

FR doc 00-25553 · 65 FR 61262

AD 2000-20-12Published 2000-10-17Effective 2000-11-27

Aerotechnik s.r.o. Model L 13 SEH VIVAT Sailplanes

Superseded by 2016-11-12 — see above

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.

Full official abstract

Airworthiness Directives; Aerotechnik s.r.o. Model L 13 SEH VIVAT Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Aerotechnik s.r.o. (Aerotechnik) Model L 13 SEH VIVAT 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 00-25553, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

View on Federal Register (opens in a new tab) Search DRS manually for AD 2000-20-12 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
Full official abstract

Airworthiness Directives; EVEKTOR, spol. s.r.o. Gliders

We are superseding airworthiness directive (AD) 2000-20-12 for EVEKTOR, spol. s.r.o. Models L 13 SEH VIVAT and L 13 SDM VIVAT gliders (type certificate previously held by AEROTECHNIK s.r.o.). 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 insufficient material strength of the tail- fuselage attachment fitting. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2016-12601, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

View on Federal Register (opens in a new tab) Search DRS manually for AD 2016-11-12 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)
AD

2016-11-11

FR doc 2016-12606 · 81 FR 36436

AD 2016-11-11Published 2016-06-07Effective 2016-07-12

EVEKTOR, spol. S.r.o. Gliders

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; EVEKTOR, spol. S.r.o. Gliders

We are adopting a new airworthiness directive (AD) for EVEKTOR, spol. s.r.o. Models L 13 SEH VIVAT and L 13 SDM VIVAT gliders (type certificate previously held by AEROTECHNIK s.r.o.). 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 lack of distinct color marking of the elevator drive. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2016-12606, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

View on Federal Register (opens in a new tab) Search DRS manually for AD 2016-11-11 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 3 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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