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2010-09-24
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Airworthiness Directives; Eurocopter France Model SA-360C, SA- 365C, C1, C2, SA-365N, N1, AS-365N2, and SA-366G1 Helicopters
Rules and Regulations
D09002ee1bdfbc32f
D09002ee1bdfbc425
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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United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD), applicable to Eurocopter France Model SA-360C, SA-365C, C1, C2, SA- 365N, N1, AS-365N2, and SA-366G1 helicopters, that requires inspecting and, if necessary, replacing certain circuit breakers. This amendment is prompted by the manufacturer discovering the loss of electrical continuity between the terminals of a circuit breaker. The actions specified by this AD are intended to prevent loss of electrical power, loss of instrumentation, and subsequent loss of control of the helicopter.
64 FR 54769
https://www.govinfo.gov/app/details/FR-1999-10-08/99-25917
99-25917
fr08oc99-5
RIN 2120-AA64
4910-13-P
Docket No. 98-SW-26-AD
Amendment 39-11359
AD 99-21-14
https://www.govinfo.gov/app/details/FR-1999-10-08/99-25917
https://www.govinfo.gov/content/pkg/FR-1999-10-08/html/99-25917.htm
https://www.govinfo.gov/content/pkg/FR-1999-10-08/pdf/99-25917.pdf
2 p.
54769
54770
64 FR 54769
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 SA-360C, SA- 365C, C1, C2, SA-365N, N1, AS-365N2, and SA-366G1 Helicopters; Federal Register Vol. 64, Issue
RULE
99-25917
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1999-11-12
Docket No. 98-SW-26-AD
Amendment 39-11359
AD 99-21-14
4910-13-P
99-25917
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to Eurocopter France Model SA-360C, SA-365C, C1, C2, SA- 365N, N1, AS-365N2, and SA-366G1 helicopters, that requires inspecting and, if necessary, replacing certain circuit breakers. This amendment is prompted by the manufacturer discovering the loss of electrical continuity between the terminals of a circuit breaker. The actions specified by this AD are intended to prevent loss of electrical power, loss of instrumentation, and subsequent loss of control of the helicopter.
Effective November 12, 1999.
Carroll Wright, Aerospace Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, 2601 Meacham Blvd., Fort Worth, Texas 76137, telephone (817) 222-5120, fax (817) 222-5961.
Federal Register
Vol. 64, no. 195
Office of the Federal Register, National Archives and Records Administration
1999-10-08
continuing
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367 p.
Table of Contents:
AE 2.7:
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AE 2.106:
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https://www.govinfo.gov/app/details/FR-1999-10-08
P0b002ee180a5599f
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr08oc99
https://www.govinfo.gov/app/details/FR-1999-10-08
https://www.govinfo.gov/content/pkg/FR-1999-10-08/pdf/FR-1999-10-08.pdf
fdlp
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DGPO
2010-09-24
2023-05-05
FR-1999-10-08
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eng
FR
FR-1999-10-08
64
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