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2018-08-28
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Airworthiness Directives; General Electric Company Turbofan Engines
Rules and Regulations
D09002ee1bdb8966e
D09002ee1bdb896de
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6- 80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6- 80C2B7F, CF6-80C2D1F, CF6-80C2L1F, and CF6-80C2K1F turbofan engines. This AD was prompted by an uncontained failure of a high-pressure turbine (HPT) stage 2 disk that resulted in a fire. This AD requires ultrasonic inspection (UI) of HPT stage 1 and 2 disks. We are issuing this AD to address the unsafe condition on these products.
83 FR 43739
https://www.govinfo.gov/app/details/FR-2018-08-28/2018-18576
2018-18576
fr28au18-2
RIN 2120-AA64
4910-13-P
Docket No. FAA-2017-0792
Product Identifier 2017-NE-28-AD
Amendment 39-19336
AD 2018-15-04
https://www.govinfo.gov/app/details/FR-2018-08-28/2018-18576
https://www.govinfo.gov/content/pkg/FR-2018-08-28/html/2018-18576.htm
https://www.govinfo.gov/content/pkg/FR-2018-08-28/pdf/2018-18576.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
43739
43742
83 FR 43739
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; General Electric Company Turbofan Engines; Federal Register Vol. 83, Issue
RULE
2018-18576
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2018-10-02
Docket No. FAA-2017-0792
Product Identifier 2017-NE-28-AD
Amendment 39-19336
AD 2018-15-04
4910-13-P
2018-18576
Final rule.
We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6- 80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6- 80C2B7F, CF6-80C2D1F, CF6-80C2L1F, and CF6-80C2K1F turbofan engines. This AD was prompted by an uncontained failure of a high-pressure turbine (HPT) stage 2 disk that resulted in a fire. This AD requires ultrasonic inspection (UI) of HPT stage 1 and 2 disks. We are issuing this AD to address the unsafe condition on these products.
This AD is effective October 2, 2018.
Matthew Smith, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA, 01803; phone: 781- 238-7735; fax: 781-238-7199; email: matthew.c.smith@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
General Electric Company Turbofan Engines
,
ANE-AD-AMOC-@faa.gov
aviation.fleetsupport@ge.com
matthew.c.smith@faa.gov
http://www.archives.gov/federal-register/cfr/ibr-locations.html
http://www.regulations.gov
Federal Register
Vol. 83, no. 167
Office of the Federal Register, National Archives and Records Administration
2018-08-28
continuing
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231 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2018-08-28
P0b002ee19c1b09ee
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr28au18
https://www.govinfo.gov/app/details/FR-2018-08-28
https://www.govinfo.gov/content/pkg/FR-2018-08-28/pdf/FR-2018-08-28.pdf
https://www.govinfo.gov/content/pkg/FR-2018-08-28/xml/FR-2018-08-28.xml
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FR-2018-08-28
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FR-2018-08-28
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