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2010-11-09
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Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Model Duo-Discus Gliders
Rules and Regulations
D09002ee1bdebab27
D09002ee1bdebabbb
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD) that applies to certain Schempp-Hirth (SCHEMPP-HIRTH) Flugzeugbau GmbH 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. 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 detect and correct failure of the bonding of the spar cap and spar web, which if not detected and corrected, could result in an in-flight failure of the wing.
68 FR 50055
https://www.govinfo.gov/app/details/FR-2003-08-20/03-21152
03-21152
fr20au03-5
RIN 2120-AA64
4910-13-P
Docket No. 2003-CE-33-AD
Amendment 39-13282
AD 2003-16-51
https://www.govinfo.gov/app/details/FR-2003-08-20/03-21152
https://www.govinfo.gov/content/pkg/FR-2003-08-20/html/03-21152.htm
https://www.govinfo.gov/content/pkg/FR-2003-08-20/pdf/03-21152.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
2 p.
50055
50056
68 FR 50055
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Model Duo-Discus Gliders; Federal Register Vol. 68, Issue
RULE
03-21152
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2003-08-20
Docket No. 2003-CE-33-AD
Amendment 39-13282
AD 2003-16-51
4910-13-P
03-21152
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that applies to certain Schempp-Hirth (SCHEMPP-HIRTH) Flugzeugbau GmbH 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. 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 detect and correct failure of the bonding of the spar cap and spar web, which if not detected and corrected, could result in an in-flight failure of the wing.
The AD becomes effective August 20, 2003, to all affected persons who did not receive emergency AD 2003-16-51, issued August 7, 2003. Emergency AD 2003-16-51 contained the requirements of this amendment, and became effective immediately upon receipt and required the actions prior to further flight.
Gregory Davidson, Aerospace Engineer, FAA, Small Airplane Directorate, Room 301, 901 Locust, Kansas City, Missouri 64106; telephone: (816) 329-4130; facsimile: (816) 329-4090.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Schempp-Hirth Flugzeugbau GmbH,
9-ACE-7-Docket@faa.gov
Federal Register
Vol. 68, no. 161
Office of the Federal Register, National Archives and Records Administration
2003-08-20
continuing
daily
deposited
born digital
429 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2003-08-20
P0b002ee180b3f6a7
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr20au03
https://www.govinfo.gov/app/details/FR-2003-08-20
https://www.govinfo.gov/content/pkg/FR-2003-08-20/pdf/FR-2003-08-20.pdf
https://www.govinfo.gov/content/pkg/FR-2003-08-20/xml/FR-2003-08-20.xml
fdlp
50039
50455
DGPO
2010-11-09
2023-05-04
FR-2003-08-20
machine generated
eng
FR
FR-2003-08-20
68
161