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2019-05-07
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Airworthiness Directives; Airbus SAS Airplanes
Proposed Rules
D09002ee1c163c37a
D09002ee1c163dffe
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
We propose to supersede Airworthiness Directive (AD) 96-25-04, which applies to certain Airbus SAS Model A320 series airplanes. AD 96- 25-04 requires repetitive inspections to detect chafing of the wire looms (bundles) in the wing and the horizontal stabilizer and in certain areas of the main landing gear (MLG) bays; repair or replacement, protection, and realignment, if necessary; installation of protective sleeves around the wire bundles; and realignment of bundles that are not guided centrally into the conduit end fittings. Since we issued AD 96-25-04, investigations identified issues with the previously installed protective sleeves. This proposed AD would partially retain the requirements of AD 96-25-04 and would require modification of the wing electrical installation, as specified in an 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 19885
https://www.govinfo.gov/app/details/FR-2019-05-07/2019-09265
2019-09265
fr07my19-7
RIN 2120-AA64
4910-13-P
Docket No. FAA-2019-0258
Product Identifier 2018-NM-134-AD
https://www.govinfo.gov/app/details/FR-2019-05-07/2019-09265
https://www.govinfo.gov/content/pkg/FR-2019-05-07/html/2019-09265.htm
https://www.govinfo.gov/content/pkg/FR-2019-05-07/pdf/2019-09265.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
19885
19888
84 FR 19885
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
2019-09265
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2019-06-21
Docket No. FAA-2019-0258
Product Identifier 2018-NM-134-AD
4910-13-P
2019-09265
Notice of proposed rulemaking (NPRM).
We propose to supersede Airworthiness Directive (AD) 96-25-04, which applies to certain Airbus SAS Model A320 series airplanes. AD 96- 25-04 requires repetitive inspections to detect chafing of the wire looms (bundles) in the wing and the horizontal stabilizer and in certain areas of the main landing gear (MLG) bays; repair or replacement, protection, and realignment, if necessary; installation of protective sleeves around the wire bundles; and realignment of bundles that are not guided centrally into the conduit end fittings. Since we issued AD 96-25-04, investigations identified issues with the previously installed protective sleeves. This proposed AD would partially retain the requirements of AD 96-25-04 and would require modification of the wing electrical installation, as specified in an 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 June 21, 2019.
Sanjay Ralhan, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3223.
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
Federal Register
Vol. 84, no. 88
Office of the Federal Register, National Archives and Records Administration
2019-05-07
continuing
daily
deposited
born digital
161 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2019-05-07
P0b002ee1a0f5611f
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr07my19
https://www.govinfo.gov/app/details/FR-2019-05-07
https://www.govinfo.gov/content/pkg/FR-2019-05-07/pdf/FR-2019-05-07.pdf
https://www.govinfo.gov/content/pkg/FR-2019-05-07/xml/FR-2019-05-07.xml
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FR-2019-05-07
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