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2010-09-24
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Airworthiness Directives; Eurocopter Deutschland GMBH Model EC 135 P1 and EC 135 T1 Helicopters
Rules and Regulations
D09002ee1bdfb5fa6
D09002ee1bdfb600b
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) applicable to Eurocopter Deutschland GMBH (ECD) Model EC 135 P1 and EC 135 T1 helicopters. This action requires inspecting main rotor expansion bolt safety wires, bolt heads, and bolt nuts; replacing any unairworthy expansion bolt with a hexagon bolt; and, as necessary, replacing any bolt nut before further flight. This AD also requires replacing each expansion bolt, regardless of condition, no later than January 31, 2000. This amendment is prompted by reports of main rotor blade expansion bolt nuts becoming loose. This condition, if not corrected, could result in severe vibration during flight and subsequent loss of control of the helicopter.
65 FR 3796
https://www.govinfo.gov/app/details/FR-2000-01-25/00-1369
00-1369
fr25ja00-5
RIN 2120-AA64
4910-13-U
Docket No. 99-SW-74-AD
Amendment 39-11517
AD 2000-01-19
https://www.govinfo.gov/app/details/FR-2000-01-25/00-1369
https://www.govinfo.gov/content/pkg/FR-2000-01-25/html/00-1369.htm
https://www.govinfo.gov/content/pkg/FR-2000-01-25/pdf/00-1369.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
3796
3798
65 FR 3796
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Eurocopter Deutschland GMBH Model EC 135 P1 and EC 135 T1 Helicopters; Federal Register Vol. 65, Issue
RULE
00-1369
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-02-04
Docket No. 99-SW-74-AD
Amendment 39-11517
AD 2000-01-19
4910-13-U
00-1369
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) applicable to Eurocopter Deutschland GMBH (ECD) Model EC 135 P1 and EC 135 T1 helicopters. This action requires inspecting main rotor expansion bolt safety wires, bolt heads, and bolt nuts; replacing any unairworthy expansion bolt with a hexagon bolt; and, as necessary, replacing any bolt nut before further flight. This AD also requires replacing each expansion bolt, regardless of condition, no later than January 31, 2000. This amendment is prompted by reports of main rotor blade expansion bolt nuts becoming loose. This condition, if not corrected, could result in severe vibration during flight and subsequent loss of control of the helicopter.
Effective February 4, 2000.
Richard A. Monschke, Aerospace Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth, Texas 76193-0110, telephone (817) 222-5116, fax (817) 222-5961.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Federal Register
Vol. 65, no. 16
Office of the Federal Register, National Archives and Records Administration
2000-01-25
continuing
daily
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325 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-01-25
P0b002ee180a01449
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr25ja00
https://www.govinfo.gov/app/details/FR-2000-01-25
https://www.govinfo.gov/content/pkg/FR-2000-01-25/pdf/FR-2000-01-25.pdf
https://www.govinfo.gov/content/pkg/FR-2000-01-25/xml/FR-2000-01-25.xml
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DGPO
2010-09-24
2023-05-05
FR-2000-01-25
machine generated
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FR
FR-2000-01-25
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