AD 2003-16-51

Emergency airworthiness directive · Spar cap · Schempp-Hirth Flugzeugbau Duo-Discus

Effective
August 20, 2003
Published
August 20, 2003 · 68 FR 50055–50056
Issued
August 7, 2003
Model
Duo-Discus
Data sheet
TCDSG85EU
Registered aircraft
29 matched by model
Product
Aircraft · Glider
Amendment
39-13282
Docket
2003-CE-33-AD
Issued as
Final rule; request for comments

Unofficial copy from the Federal Register XML, document 03-21152. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.

On this page

Summary

This document makes a correction to Airworthiness Directive (AD) 2003-16-51, which was published in the Federal Register on August 20, 2003 (68 FR 50055), and applies to certain Schempp-Hirth (SCHEMPP-HIRTH) Flugzeugbau GmbH Model Duo-Discus gliders. We inadvertently omitted certain regulatory text in 14 CFR part 39. This action corrects the regulatory text.

The airworthiness directive

On page 50056, in § 39.13 [Amended], in the third column, add the words “Amendment 39-13282; “ after “GmbH:”

Action is taken herein to correct this reference in AD 2003-16-51 and to add this AD correction to § 39.13 of the Federal Aviation Regulations (14 CFR 39.13).

The effective date remains August 20, 2003.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

Effective datePage 1

The effective date of this AD remains August 20, 2003.

For further information contactPage 1

Gregory Davidson, Aerospace Engineer, FAA, Small Airplane Directorate, Room 301, 901 Locust, Kansas City, Missouri 64106; telephone: (816) 329-4130; facsimile: (816) 329-4090.

DiscussionPage 1

On August 12, 2003, FAA issued AD 2003-16-51, Amendment 39-13282 (68 FR 50055, August 20, 2003), which applies to certain SCHEMPP-HIRTH Model Duo-Discus gliders. This AD requires you to accomplish a one-time inspection of the bonding of the spar cap and spar web, and repair any defective bonding of the spar cap and spar web.

Need for the CorrectionPage 1

The FAA inadvertently omitted Amendment 39-13282 in the regulatory portion of the AD (in 14 CFR part 39).

The information is included in the preamble of the AD. The amendment number is needed for appropriate logbook entry for the affected airplane owners/operators if the preamble of the AD is not available.

Correction of PublicationPage 1

Accordingly, the publication of August 20, 2003 (68 FR 50055), of Amendment 39-13282; AD 2003-16-51, is corrected as follows:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 29

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Schempp-Hirth Flugzeugbau29 aircraft
By year built
19962025
Registered aircraft by year built: 23 aircraft
19961
19983
19993
20001
20011
20021
20034
20041
20052
20072
20151
20161
20252

6 with no year recorded

By model

Aircraft

See all 29 aircraft

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 2003-16-51, often to say whether the aircraft complied with it.