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2010-09-23
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Airworthiness Directives; Schweizer Aircraft Corporation Model 269C, C-1, and D Helicopters
Rules and Regulations
D09002ee1bde3b2a1
D09002ee1bde3b847
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
This amendment adopts a new airworthiness directive (AD) for the Schweizer Aircraft Corporation (Schweizer) Model 269C, C-1, and D helicopters. This action requires inspecting, modifying, and testing the lateral control trim actuator assembly on certain serial-numbered helicopters. This amendment is prompted by three reported incidents of the inner spring tube separating from the lateral trim control housing resulting in a lateral cyclic control restriction. The actions specified in this AD are intended to prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of control of the helicopter.
70 FR 28415
https://www.govinfo.gov/app/details/FR-2005-05-18/05-9764
05-9764
fr18my05-2
RIN 2120-AA64
4910-13-P
Docket No. FAA-2005-21217
Directorate Identifier 2005-SW-06-AD
Amendment 39-14089
AD 2005-10-12
https://www.govinfo.gov/app/details/FR-2005-05-18/05-9764
https://www.govinfo.gov/content/pkg/FR-2005-05-18/html/05-9764.htm
https://www.govinfo.gov/content/pkg/FR-2005-05-18/pdf/05-9764.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
28415
28417
70 FR 28415
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Schweizer Aircraft Corporation Model 269C, C-1, and D Helicopters; Federal Register Vol. 70, Issue
RULE
05-9764
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-06-02
Docket No. FAA-2005-21217
Directorate Identifier 2005-SW-06-AD
Amendment 39-14089
AD 2005-10-12
4910-13-P
05-9764
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) for the Schweizer Aircraft Corporation (Schweizer) Model 269C, C-1, and D helicopters. This action requires inspecting, modifying, and testing the lateral control trim actuator assembly on certain serial-numbered helicopters. This amendment is prompted by three reported incidents of the inner spring tube separating from the lateral trim control housing resulting in a lateral cyclic control restriction. The actions specified in this AD are intended to prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of control of the helicopter.
Effective June 2, 2005.
Leung Lee, Aviation Safety Engineer, FAA, New York Aircraft Certification Office, Systems and Flight Test Branch, 1600 Stewart Ave., Suite 410, Westbury, New York 11590, telephone (516) 228-7309, fax (516) 794-5531.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Schweizer Aircraft Corp.,
http://dms.dot.gov
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
http://www.regulations.gov
Federal Register
Vol. 70, no. 95
Office of the Federal Register, National Archives and Records Administration
2005-05-18
continuing
daily
deposited
born digital
367 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2005-05-18
P0b002ee180992c74
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr18my05
https://www.govinfo.gov/app/details/FR-2005-05-18
https://www.govinfo.gov/content/pkg/FR-2005-05-18/pdf/FR-2005-05-18.pdf
https://www.govinfo.gov/content/pkg/FR-2005-05-18/xml/FR-2005-05-18.xml
fdlp
28415
28771
DGPO
2010-09-23
2023-05-03
FR-2005-05-18
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FR
FR-2005-05-18
70
95