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2021-01-16
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Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Rules and Regulations
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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
The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Models PA-28-151, PA-28-161, PA- 28-181, PA-28-235, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA- 28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This AD was prompted by a report of a wing separation caused by fatigue cracking in a visually inaccessible area of the lower main wing spar cap. This AD requires calculating the factored service hours for each main wing spar to determine when an inspection is required, inspecting the lower main wing spar bolt holes for cracks, and replacing any cracked main wing spar. The FAA is issuing this AD to address the unsafe condition on these products.
86 FR 3769
https://www.govinfo.gov/app/details/FR-2021-01-15/2021-00044
2021-00044
fr15ja21-9
RIN 2120-AA64
4910-13-P
Docket No. FAA-2018-1046
Product Identifier 2018-CE-049-AD
Amendment 39-21371
AD 2020-26-16
https://www.govinfo.gov/app/details/FR-2021-01-15/2021-00044
https://www.govinfo.gov/content/pkg/FR-2021-01-15/html/2021-00044.htm
https://www.govinfo.gov/content/pkg/FR-2021-01-15/pdf/2021-00044.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
12 p.
3769
3780
86 FR 3769
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Piper Aircraft, Inc. Airplanes; Federal Register Vol. 86, Issue
RULE
2021-00044
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2021-02-16
Docket No. FAA-2018-1046
Product Identifier 2018-CE-049-AD
Amendment 39-21371
AD 2020-26-16
4910-13-P
2021-00044
Final rule.
The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Models PA-28-151, PA-28-161, PA- 28-181, PA-28-235, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA- 28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This AD was prompted by a report of a wing separation caused by fatigue cracking in a visually inaccessible area of the lower main wing spar cap. This AD requires calculating the factored service hours for each main wing spar to determine when an inspection is required, inspecting the lower main wing spar bolt holes for cracks, and replacing any cracked main wing spar. The FAA is issuing this AD to address the unsafe condition on these products.
This AD is effective February 16, 2021.
Dan McCully, Aviation Safety Engineer, Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474-5548; fax: (404) 474-5605; email: william.mccully@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Piper Aircraft, Inc. Airplanes,
fedreg.legal@nara.gov
william.mccully@faa.gov
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Federal Register
Vol. 86, no. 10
Office of the Federal Register, National Archives and Records Administration
2021-01-15
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Table of Contents:
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https://www.govinfo.gov/app/details/FR-2021-01-15
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