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FR
Regulatory Information
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2020-11-07
article
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
Proposed Rules
D09002ee1bdb33e37
D09002ee1bdb33e9e
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
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+, EC135P3, and EC135T3 helicopters. This proposed AD was prompted by a deviation from a new manufacturing process, which resulted in a reduced life limit (service life limit) for certain tail rotor blades. This proposed AD would require a reduced life limit for those tail rotor blades and require a new life limit for certain other tail rotor blades, as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.
85 FR 71286
https://www.govinfo.gov/app/details/FR-2020-11-09/2020-24766
2020-24766
fr09no20-18
RIN 2120-AA64
4910-13-P
Docket No. FAA-2020-0985
Product Identifier 2018-SW-064-AD
https://www.govinfo.gov/app/details/FR-2020-11-09/2020-24766
https://www.govinfo.gov/content/pkg/FR-2020-11-09/html/2020-24766.htm
https://www.govinfo.gov/content/pkg/FR-2020-11-09/pdf/2020-24766.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
71286
71289
85 FR 71286
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters Deutschland GmbH; Federal Register Vol. 85, Issue
PRORULE
2020-24766
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2020-12-24
Docket No. FAA-2020-0985
Product Identifier 2018-SW-064-AD
4910-13-P
2020-24766
Notice of proposed rulemaking (NPRM).
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+, EC135P3, and EC135T3 helicopters. This proposed AD was prompted by a deviation from a new manufacturing process, which resulted in a reduced life limit (service life limit) for certain tail rotor blades. This proposed AD would require a reduced life limit for those tail rotor blades and require a new life limit for certain other tail rotor blades, as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.
The FAA must receive comments on this proposed AD by December 24, 2020.
Kristin Bradley, Aviation Safety Engineer, International Validation Branch, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5485; email Kristin.Bradley@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Airbus Helicopters Deutschland GmbH,
9-ASW-FTW-AMOC-Requests@faa.gov
ADs@easa.europa.eu
Kristin.Bradley@faa.gov
https://ad.easa.europa.eu
https://www.regulations.gov
Federal Register
Vol. 85, no. 217
Office of the Federal Register, National Archives and Records Administration
2020-11-09
continuing
daily
deposited
born digital
315 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2020-11-09
P0b002ee1a93cf2c1
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr09no20
https://www.govinfo.gov/app/details/FR-2020-11-09
https://www.govinfo.gov/content/pkg/FR-2020-11-09/pdf/FR-2020-11-09.pdf
https://www.govinfo.gov/content/pkg/FR-2020-11-09/xml/FR-2020-11-09.xml
fdlp
71223
71528
DGPO
2020-11-07
2023-04-27
FR-2020-11-09
machine generated
eng
FR
FR-2020-11-09
85
217