AD 62-27-02

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 47 Series Helicopters

AD Number
62-27-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: December 28, 1962

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47B Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47D Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47E Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2 Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2A Airworthiness Directives; Bell Model 47 Series Helicopters
aircraft Scotts-Bell 47 Inc 47G-2A-1 Airworthiness Directives; Bell Model 47 Series Helicopters

Unsafe Condition

Failures of wood tail rotor blades resulting from wood deterioration, including elongated bolt holes exceeding 0.260 inch diameter, decay of wood with discoloration, and cracks in stainless steel leading edge strips and grip plates.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within 50 hours' time in service after the effective date, remove wood tail rotor blades, remove fiberglass wrapping and blade covering, inspect root end for bolt hole diameter, decay, and cracks using a 5-power magnifying glass. Blades with defects must be removed from service. Blades without defects must be recovered, rewrapped with MIL-P-8013 No. 181 fiberglass cloth, and retired after 200 hours' time in service since reinstallation.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 50 hours' time in service after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All Model 47 Series Helicopters equipped with P/N 47-642-020-1 Wood Tail Rotor Blades.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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