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2019-06-14
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Airworthiness Directives; Airbus SAS Airplanes
Proposed Rules
D09002ee1bdb73e4c
D09002ee1bdb73efc
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
We propose to supersede Airworthiness Directive (AD) 2000-03- 20 R1, which applies to all Airbus SAS Model A300 B4-601, B4-603, and B4-620, Model A300 B4-600R series, and Model A300 F4-605R airplanes. AD 2000-03-20 R1 requires repetitive ultrasonic inspections to detect cracks on the forward fittings in the radius of a certain frame, adjacent to the tension bolts in the center section of the wings, and various follow-on actions. Since we issued AD 2000-03-20 R1, we have determined that the existing compliance times must be reduced. This proposed AD would retain the requirements of AD 2000-03-20 R1, add new airplanes to the applicability, and introduce new compliance times for the required inspections as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.
84 FR 27990
https://www.govinfo.gov/app/details/FR-2019-06-17/2019-12664
2019-12664
fr17jn19-25
RIN 2120-AA64
4910-13-P
Docket No. FAA-2019-0441
Product Identifier 2019-NM-036-AD
https://www.govinfo.gov/app/details/FR-2019-06-17/2019-12664
https://www.govinfo.gov/content/pkg/FR-2019-06-17/html/2019-12664.htm
https://www.govinfo.gov/content/pkg/FR-2019-06-17/pdf/2019-12664.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
5 p.
27990
27994
84 FR 27990
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes; Federal Register Vol. 84, Issue
PRORULE
2019-12664
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2019-08-01
Docket No. FAA-2019-0441
Product Identifier 2019-NM-036-AD
4910-13-P
2019-12664
Notice of proposed rulemaking (NPRM).
We propose to supersede Airworthiness Directive (AD) 2000-03- 20 R1, which applies to all Airbus SAS Model A300 B4-601, B4-603, and B4-620, Model A300 B4-600R series, and Model A300 F4-605R airplanes. AD 2000-03-20 R1 requires repetitive ultrasonic inspections to detect cracks on the forward fittings in the radius of a certain frame, adjacent to the tension bolts in the center section of the wings, and various follow-on actions. Since we issued AD 2000-03-20 R1, we have determined that the existing compliance times must be reduced. This proposed AD would retain the requirements of AD 2000-03-20 R1, add new airplanes to the applicability, and introduce new compliance times for the required inspections as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.
We must receive comments on this proposed AD by August 1, 2019.
Dan Rodina, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3225.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Airbus SAS Airplanes
,
9-ANM-116-AMOC-REQUESTS@faa.gov
ADs@easa.europa.eu
http://www.regulations.gov
https://ad.easa.europa.eu
https://w3.airbus.com/
Federal Register
Vol. 84, no. 116
Office of the Federal Register, National Archives and Records Administration
2019-06-17
continuing
daily
deposited
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273 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2019-06-17
P0b002ee1a163ce2e
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr17jn19
https://www.govinfo.gov/app/details/FR-2019-06-17
https://www.govinfo.gov/content/pkg/FR-2019-06-17/pdf/FR-2019-06-17.pdf
https://www.govinfo.gov/content/pkg/FR-2019-06-17/xml/FR-2019-06-17.xml
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DGPO
2019-06-14
2023-04-28
FR-2019-06-17
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FR-2019-06-17
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