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2010-09-22
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Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, B, L, L-1, L-3, and L-4 Helicopters
Rules and Regulations
D09002ee1bddeddfd
D09002ee1bddee79d
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
This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters. The existing AD currently requires certain inspections and checks of the tail rotor blade (blade) for a deformation, a crack, and a bent or deformed tail rotor weight (weight). Also, that AD requires, before further flight, replacing each blade with an airworthy blade if a deformation, a crack, or a bent or deformed weight is found. This action contains the same actions as the existing AD and also adds to the applicability certain serial-numbered blades inadvertently omitted from the current AD. This action also requires replacing each affected blade, which is a terminating action. This amendment is prompted by three reports of skin cracks originating near the blade trailing edge balance weight. The actions specified by this AD are intended to prevent blade failure and subsequent loss of control of the helicopter.
72 FR 889
https://www.govinfo.gov/app/details/FR-2007-01-09/E7-39
E7-39
fr09ja07-3
RIN 2120-AA64
4910-13-P
Docket No. FAA-2005-22696
Directorate Identifier 2005-SW-22-AD
Amendment 39-14877
AD 2007-01-06
https://www.govinfo.gov/app/details/FR-2007-01-09/E7-39
https://www.govinfo.gov/content/pkg/FR-2007-01-09/html/E7-39.htm
https://www.govinfo.gov/content/pkg/FR-2007-01-09/pdf/E7-39.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
4 p.
889
892
72 FR 889
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, B, L, L-1, L-3, and L-4 Helicopters; Federal Register Vol. 72, Issue
RULE
E7-39
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2007-02-13
Docket No. FAA-2005-22696
Directorate Identifier 2005-SW-22-AD
Amendment 39-14877
AD 2007-01-06
4910-13-P
E7-39
Final rule.
This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters. The existing AD currently requires certain inspections and checks of the tail rotor blade (blade) for a deformation, a crack, and a bent or deformed tail rotor weight (weight). Also, that AD requires, before further flight, replacing each blade with an airworthy blade if a deformation, a crack, or a bent or deformed weight is found. This action contains the same actions as the existing AD and also adds to the applicability certain serial-numbered blades inadvertently omitted from the current AD. This action also requires replacing each affected blade, which is a terminating action. This amendment is prompted by three reports of skin cracks originating near the blade trailing edge balance weight. The actions specified by this AD are intended to prevent blade failure and subsequent loss of control of the helicopter.
Effective February 13, 2007.
Sharon Miles, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Regulations and Guidance Group, Fort Worth, Texas 76193-0111, telephone (817) 222-5122, fax (817) 222- 5961.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Bell Helicopter Textron Canada,
http://dms.dot.gov
Federal Register
Vol. 72, no. 5
Office of the Federal Register, National Archives and Records Administration
2007-01-09
continuing
daily
deposited
born digital
266 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2007-01-09
P0b002ee180947cbb
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr09ja07
https://www.govinfo.gov/app/details/FR-2007-01-09
https://www.govinfo.gov/content/pkg/FR-2007-01-09/pdf/FR-2007-01-09.pdf
https://www.govinfo.gov/content/pkg/FR-2007-01-09/xml/FR-2007-01-09.xml
fdlp
875
1133
DGPO
2010-09-22
2023-05-02
FR-2007-01-09
machine generated
eng
FR
FR-2007-01-09
72
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