AD 57-12-04

final rule
Data completeness: 60%

Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters

AD Number
57-12-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Scotts-Bell 47 Inc 47B Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47B3 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47D Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47D1 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47G Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47G-2 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47H-1 Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters
aircraft Scotts-Bell 47 Inc 47J Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J Helicopters

Unsafe Condition

Excessive play in the metal tail rotor blade and hub assembly and the pitch control mechanism can result in blade flutter.

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

Required Actions

Inspect the metal tail rotor blade and hub assembly and pitch control mechanism as required in Part A of Bell Mandatory Service Bulletin No. 121SB. Inspect metal tail rotor blades P/N 47-642-102-5 for minimum 0.750 inch thickness at blade station 14.00; replace blades below this thickness.

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

Compliance Time

as soon as possible but not later than August 1, 1957

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

Affected Aircraft

Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, 47H1, and 47J helicopters with metal tail rotor blades (Part A); Bell Model 47B, 47B3, 47D, 47D1, 47G, 47G2, and 47H1 helicopters with metal tail rotor blades P/N 47-642-102-5 (Part B)

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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