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1998_register
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2010-09-24
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Airworthiness Directives; Airbus Model A320-111 Series Airplanes
Rules and Regulations
D09002ee1be002ac8
D09002ee1be002b8b
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A320-111 series airplanes. This amendment requires repetitive inspections to detect cracking around the attachment holes for the access panels in the lower skin of the wing; and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect and correct such cracking, which could result in reduced structural integrity of the airplane.
63 FR 13508
https://www.govinfo.gov/app/details/FR-1998-03-20/98-6947
98-6947
fr20mr98-15
RIN 2120-AA64
4910-13-U
Docket No. 98-NM-22-AD
Amendment 39-10410
https://www.govinfo.gov/app/details/FR-1998-03-20/98-6947
https://www.govinfo.gov/content/pkg/FR-1998-03-20/html/98-6947.htm
https://www.govinfo.gov/content/pkg/FR-1998-03-20/pdf/98-6947.pdf
3 p.
13508
13510
63 FR 13508
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Model A320-111 Series Airplanes; Federal Register Vol. 63, Issue
RULE
98-6947
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1998-06-18
Docket No. 98-NM-22-AD
Amendment 39-10410
4910-13-U
98-6947
Direct final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A320-111 series airplanes. This amendment requires repetitive inspections to detect cracking around the attachment holes for the access panels in the lower skin of the wing; and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect and correct such cracking, which could result in reduced structural integrity of the airplane.
Effective June 18, 1998.
Norman B. Martenson, Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2110; fax (425) 227-1149.
Federal Register
Vol. 63, no. 54
Office of the Federal Register, National Archives and Records Administration
1998-03-20
continuing
daily
deposited
born digital
301 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
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https://www.govinfo.gov/app/details/FR-1998-03-20
P0b002ee180a67856
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr20mr98
https://www.govinfo.gov/app/details/FR-1998-03-20
https://www.govinfo.gov/content/pkg/FR-1998-03-20/pdf/FR-1998-03-20.pdf
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DGPO
2010-09-24
2023-05-06
FR-1998-03-20
machine generated
eng
FR
FR-1998-03-20
63
54