Aircraft model

Valentin Taifun 17E

Valentin GmbH

Airworthiness Directives
2
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-022 of 2 re-checked
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: Valentin 17E

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What Airworthiness Directives apply to the Valentin Taifun 17E

The FAA has published 2 Airworthiness Directives that name the Valentin Taifun 17E (Valentin GmbH), the earliest in 2001 and the newest on 2004-10-14.

Newest

  1. AD 2004-20-10 Airworthiness Directives; Valentin GmbH & Co. Taifun 17E Sailplanes 2004-10-14
  2. AD 2001-05-08 Airworthiness Directives; VALENTIN GmbH Model 17E Sailplanes 2001-03-23

See all 2 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

2 records
ADAD 2004-20-10Valentin GmbH & Co. Taifun 17E Sailplanes2004-11-24Active
AD

2004-20-10

FR doc 04-22715 · 69 FR 60949

AD 2004-20-10Published 2004-10-14Effective 2004-11-24

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.

Valentin GmbH & Co. Taifun 17E Sailplanes

Requires you to do an operational check of the front wing-locking mechanism left and right, inspect stop key movement, inspect wing and fuselage side root ribs, inspect the wing side shear force fittings, and take any corrective…

Full official abstract

Airworthiness Directives; Valentin GmbH & Co. Taifun 17E Sailplanes

The FAA adopts a new airworthiness directive (AD) for all Valentin GmbH & Co. Taifun 17E sailplanes. This AD requires you to do an operational check of the front wing-locking mechanism left and right, inspect stop key movement, inspect wing and fuselage side root ribs, inspect the wing side shear force fittings, and take any corrective actions that may be required. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct malfunction of wing-locking mechanism, which could result in failure of the wing-locking mechanism disengagement. This failure could lead to unlocking of wing in flight and consequent loss of control of the sailplane.

Source: Federal Register document 04-22715, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2001-05-08VALENTIN GmbH Model 17E Sailplanes2001-04-13Active
AD

2001-05-08

FR doc 01-6283 · 66 FR 16103

AD 2001-05-08Published 2001-03-23Effective 2001-04-13

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.

VALENTIN GmbH Model 17E Sailplanes

Requires you to inspect for, and correct, cracked or improperly installed central wing bolts; install a stronger central bolt if not already installed; and inspect for, and replace, problem telescopic rods.

Full official abstract

Airworthiness Directives; VALENTIN GmbH Model 17E Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to all VALENTIN GmbH (Valentin) Model 17E sailplanes. This AD requires you to inspect for, and correct, cracked or improperly installed central wing bolts; install a stronger central bolt if not already installed; and inspect for, and replace, problem telescopic rods. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to correct improperly installed or cracked central bolts and damaged, deformed, or loose telescopic rods. This condition, if not corrected, could cause the wing to separate from the sailplane, which could cause result in control of the sailplane.

Source: Federal Register document 01-6283, 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 2 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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