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FR
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2021-07-07
article
Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters
Rules and Regulations
D09002ee1aef21f26
D09002ee1aef21fa1
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 is adopting a new airworthiness directive (AD) for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters. This AD requires modifying the tail rotor (T/R) control installation, a functional test, and corrective actions as necessary. This AD was prompted by cases of insufficient clearance between a certain T/R control bearing connection and the helicopter structure, which were detected on the production line. The FAA is issuing this AD to address the unsafe condition on these products.
86 FR 35599
https://www.govinfo.gov/app/details/FR-2021-07-07/2021-14343
2021-14343
fr07jy21-2
RIN 2120-AA64
4910-13-P
Docket No. FAA-2019-0293
Product Identifier 2017-SW-052-AD
Amendment 39-21610
AD 2021-13-05
https://www.govinfo.gov/app/details/FR-2021-07-07/2021-14343
https://www.govinfo.gov/content/pkg/FR-2021-07-07/html/2021-14343.htm
https://www.govinfo.gov/content/pkg/FR-2021-07-07/pdf/2021-14343.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
35599
35601
86 FR 35599
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 Helicopters; Federal Register Vol. 86, Issue
RULE
2021-14343
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2021-08-11
Docket No. FAA-2019-0293
Product Identifier 2017-SW-052-AD
Amendment 39-21610
AD 2021-13-05
4910-13-P
2021-14343
Final rule.
The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters. This AD requires modifying the tail rotor (T/R) control installation, a functional test, and corrective actions as necessary. This AD was prompted by cases of insufficient clearance between a certain T/R control bearing connection and the helicopter structure, which were detected on the production line. The FAA is issuing this AD to address the unsafe condition on these products.
This AD is effective August 11, 2021.
David Hatfield, Aviation Safety Engineer, Aircraft Systems Section, Technical Innovation Policy Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222- 5110; email david.hatfield@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Airbus Helicopters Deutschland GmbH Helicopters,
9-AVS-AIR-730-AMOC@faa.gov
david.hatfield@faa.gov
fedreg.legal@nara.gov
https://www.airbus.com/helicopters/services/technical-support.html
https://www.archives.gov/federal-register/cfr/ibr-locations.html
https://www.regulations.gov
Federal Register
Vol. 86, no. 127
Office of the Federal Register, National Archives and Records Administration
2021-07-07
continuing
daily
deposited
born digital
476 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2021-07-07
P0b002ee1aef1e9c7
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr07jy21
https://www.govinfo.gov/app/details/FR-2021-07-07
https://www.govinfo.gov/content/pkg/FR-2021-07-07/pdf/FR-2021-07-07.pdf
https://www.govinfo.gov/content/pkg/FR-2021-07-07/xml/FR-2021-07-07.xml
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2021-07-07
FR-2021-07-07
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FR
FR-2021-07-07
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