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AD 80-17-09 SUPERSEDED

Main Rotor Straps
WARNING: This AD has been superseded and is no longer active. Replaced by: 2002-22-14. Refer to the superseding AD(s) for current requirements.
Key Information
AD Number 80-17-09 Status Superseded
Effective Date September 15, 1980 Issue Date Not specified
Docket Number Unknown Amendment 39-3876
Product Type ["Aircraft"] Product Subtype ["Rotorcraft"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Bell Helicopter Textron, Inc. California Department of Forestry Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation Rotorcraft Development Corporation San Joaquin Helicopters International Helicopters, Inc. US Helicopter, Inc. Richards Heavylift Helo, Inc.
Model(s) 204B 205A-1 212 214B 214B-1 UH-1F UH-1B UH-1E UH-1F UH-1H UH-1L UH-1P UH-1B UH-1B UH-1A UH-1B UH-1E UH-1H UH-1L
Related Airworthiness Directives
Superseded By 2002-22-14
Regulatory Text

80-17-09 BELL: Amendment 39-3876. Applies to Models 204B, 205A-1, 212, 214B, and 214B-1 helicopters and military UH-1 series helicopters certified in all categories.

Compliance required as indicated for helicopters equipped with main rotor straps, P/N 204-012-122-1, -5, or 214-010-179-1.

To preclude possible separation of a main rotor blade tension-torsion strap and loss of a main rotor blade, accomplish the following:

a. Within the next 100 hours' time in service after the effective date of this airworthiness directive (AD), remove and replace main rotor straps having:

(1) 1,100 or more hours of total time in service on the effective date of this AD, or

(2) 24 or more months elapsed calendar time in service as of the effective date of this AD, whichever comes first.

b. Remove and replace main rotor straps having less than 1,100 hours' total time in service or having less than 24 months elapsed time in service on the effective date of this AD:(1) Prior to attaining 1,200 hours' total time in service, or

(2) Prior to exceeding 24 months elapsed time in service, whichever comes first.

c. The helicopter may be flown in accordance with FAR's 21.197 and 21.199 to a base where this AD may be accomplished.

(Bell Helicopter Textron Alert Service Bulletin No. 212-80-17 pertains to this subject.)

This amendment becomes effective September 15, 1980.