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2010-09-22
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Airworthiness Directives; Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes
Proposed Rules
D09002ee1bddaacd4
D09002ee1bddaad5b
United States
Department of Transportation
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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 Raytheon (Beech) Model 400, 400A, and 400T series airplanes. This proposed AD would require modifying the attachment fasteners on the engine cowling panels. This proposed AD results from several reports of loose attachment fasteners found on the engine cowling panels, and subsequently the panels either peeling back or separating from the airplane during flight. We are proposing this AD to prevent failure of the attachment fasteners on the engine cowling panels, which could result in separation of a panel from the airplane, and consequent damage to airplane structure. These conditions could adversely affect continued safe flight and landing of the airplane, or cause injury to people or damage to property on the ground.
72 FR 29446
https://www.govinfo.gov/app/details/FR-2007-05-29/E7-10216
E7-10216
fr29my07-8
RIN 2120-AA64
4910-13-P
Docket No. FAA-2007-28308
Directorate Identifier 2007-NM-016-AD
https://www.govinfo.gov/app/details/FR-2007-05-29/E7-10216
https://www.govinfo.gov/content/pkg/FR-2007-05-29/html/E7-10216.htm
https://www.govinfo.gov/content/pkg/FR-2007-05-29/pdf/E7-10216.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
2 p.
29446
29447
72 FR 29446
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; Federal Register Vol. 72, Issue
PRORULE
E7-10216
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2007-07-13
Docket No. FAA-2007-28308
Directorate Identifier 2007-NM-016-AD
4910-13-P
E7-10216
Notice of proposed rulemaking (NPRM).
The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon (Beech) Model 400, 400A, and 400T series airplanes. This proposed AD would require modifying the attachment fasteners on the engine cowling panels. This proposed AD results from several reports of loose attachment fasteners found on the engine cowling panels, and subsequently the panels either peeling back or separating from the airplane during flight. We are proposing this AD to prevent failure of the attachment fasteners on the engine cowling panels, which could result in separation of a panel from the airplane, and consequent damage to airplane structure. These conditions could adversely affect continued safe flight and landing of the airplane, or cause injury to people or damage to property on the ground.
We must receive comments on this proposed AD by July 13, 2007.
William Griffith, Aerospace Engineer, Airframe and Services Branch, ACE-118W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4116; fax (316) 946-4107.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Raytheon,
http://dms.dot.gov
http://www.regulations.gov
Federal Register
Vol. 72, no. 102
Office of the Federal Register, National Archives and Records Administration
2007-05-29
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420 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2007-05-29
P0b002ee180965db8
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr29my07
https://www.govinfo.gov/app/details/FR-2007-05-29
https://www.govinfo.gov/content/pkg/FR-2007-05-29/pdf/FR-2007-05-29.pdf
https://www.govinfo.gov/content/pkg/FR-2007-05-29/xml/FR-2007-05-29.xml
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29429
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2010-09-22
2023-05-02
FR-2007-05-29
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FR-2007-05-29
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