Aircraft model

Evektor L 13 Vivat

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

Airworthiness Directives
3
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-023 of 3 re-checked, oldest 2026-10-01
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Also known as: L 13 SDM, L 13 SEH

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What Airworthiness Directives apply to the Evektor L 13 Vivat

The FAA has published 3 Airworthiness Directives that name the Evektor L 13 Vivat (EVEKTOR, spol. s.r.o. (formerly Aerotechnik)), the earliest in 2000 and the newest on 2016-06-09.

Newest

  1. AD 2016-11-12 Airworthiness Directives; EVEKTOR, spol. s.r.o. Gliders 2016-06-09
  2. AD 2016-11-11 Airworthiness Directives; EVEKTOR, spol. S.r.o. Gliders 2016-06-07
  3. AD 2000-20-12 Airworthiness Directives; Aerotechnik s.r.o. Model L 13 SEH VIVAT Sailplanes 2000-10-17

See all 3 directives

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

3 records · 1 superseded record nested above
ADAD 2016-11-12EVEKTOR, spol. s.r.o. Gliders2016-07-14Active
AD

2016-11-12

FR doc 2016-12601 · 81 FR 37124

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

Supersedes 2000-20-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

EVEKTOR, spol. s.r.o. Gliders

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1 AD superseded by this one retired · earliest 2000-10-17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

Superseded by 2016-11-12 — see above

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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

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 · checked against the live Federal Register record on 2026-10-01

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 · checked against the live Federal Register record on 2026-10-02

ADAD 2016-11-11EVEKTOR, spol. S.r.o. Gliders2016-07-12Active
AD

2016-11-11

FR doc 2016-12606 · 81 FR 36436

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

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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 · checked against the live Federal Register record on 2026-10-02

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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