AD 62-23-02

final rule
Data completeness: 70%

Airworthiness Directives; Bell Model 47 Series Helicopters

AD Number
62-23-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: October 23,1962

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

Excessive wear and evidence of impending failure of the main rotor mast thrust bearing have occurred.

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

Required Actions

Within 25 hours' time in service after the effective date, conduct a close visual inspection of the engine oil filter every 25 hours. If metal particles are found, locate and eliminate the contaminant source, inspect and overhaul engine and transmission components as prescribed, inspect and replace the main rotor mast thrust bearing (P/N 47-130-110-1) if unserviceable, and clean the engine oil filter before reinstalling.

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

Compliance Time

Within the next 25 hours' time in service following the effective date of this AD and thereafter at periods not to exceed 25 hours

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

Affected Aircraft

Scotts-Bell 47 Inc Model 47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1 equipped with Main Rotor Mast Thrust Bearing, P/N 47-130-110-1.

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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