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2010-09-23
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Airworthiness Directives; Eurocopter France Model AS332C, AS332L, AS332L1, and AS332L2 Helicopters
Rules and Regulations
D09002ee1bdeb6378
D09002ee1bdeb641a
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 adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires inspecting certain main rotor blades for disbonds, which may be indicated by cracking, and repairing or replacing each main rotor blade (MRB) as necessary. This amendment is prompted by the discovery of disbonded leading edge protective strips. The actions specified by this AD are intended to detect disbonding between the stainless steel protective strip and the MRB skin, which could cause loss of the protective strip, an out-of-balance condition, and subsequent loss of control of the helicopter.
68 FR 60845
https://www.govinfo.gov/app/details/FR-2003-10-24/03-26466
03-26466
fr24oc03-2
RIN 2120-AA64
4910-13-P
Docket No. 2002-SW-58-AD
Amendment 39-13343
AD 2003-21-08
https://www.govinfo.gov/app/details/FR-2003-10-24/03-26466
https://www.govinfo.gov/content/pkg/FR-2003-10-24/html/03-26466.htm
https://www.govinfo.gov/content/pkg/FR-2003-10-24/pdf/03-26466.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
60845
60847
68 FR 60845
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Eurocopter France Model AS332C, AS332L, AS332L1, and AS332L2 Helicopters; Federal Register Vol. 68, Issue
RULE
03-26466
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2003-11-28
Docket No. 2002-SW-58-AD
Amendment 39-13343
AD 2003-21-08
4910-13-P
03-26466
Final rule.
This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires inspecting certain main rotor blades for disbonds, which may be indicated by cracking, and repairing or replacing each main rotor blade (MRB) as necessary. This amendment is prompted by the discovery of disbonded leading edge protective strips. The actions specified by this AD are intended to detect disbonding between the stainless steel protective strip and the MRB skin, which could cause loss of the protective strip, an out-of-balance condition, and subsequent loss of control of the helicopter.
Effective November 28, 2003.
Gary Roach, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Regulations and Guidance Group, Fort Worth, Texas 76193-0111, telephone (817) 222-5130, fax (817) 222-5961.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Eurocopter France,
Federal Register
Vol. 68, no. 206
Office of the Federal Register, National Archives and Records Administration
2003-10-24
continuing
daily
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born digital
267 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2003-10-24
P0b002ee1809e6040
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr24oc03
https://www.govinfo.gov/app/details/FR-2003-10-24
https://www.govinfo.gov/content/pkg/FR-2003-10-24/pdf/FR-2003-10-24.pdf
https://www.govinfo.gov/content/pkg/FR-2003-10-24/xml/FR-2003-10-24.xml
fdlp
60841
61096
DGPO
2010-09-23
2023-05-04
FR-2003-10-24
machine generated
eng
FR
FR-2003-10-24
68
206