AD 61-14-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Scotts-Bell 47 Inc | 47G-2A | Airworthiness Directives; Bell Model 47J, 47J-2, 47G-3, and 47G-2A Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47G-3 | Airworthiness Directives; Bell Model 47J, 47J-2, 47G-3, and 47G-2A Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47J | Airworthiness Directives; Bell Model 47J, 47J-2, 47G-3, and 47G-2A Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47J-2 | Airworthiness Directives; Bell Model 47J, 47J-2, 47G-3, and 47G-2A Helicopters |
Unsafe Condition
Failure of the forward cross tube near the left attaching point (cross tube to centerframe) due to welded closed and filed smooth drilled holes.
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Required Actions
Within 10 hours' time in service after the effective date, inspect the cross tube P/N 47-512-111-9 for welded holes near the stop plates P/N 47-500-024-1. If welds exist, replace the cross tube with an FAA approved part within 5 hours' time in service following inspection.
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Compliance Time
Within the next 10 hours' time in service after the effective date (July 12, 1961) for inspection, and within 5 hours' time in service following inspection if welds are found.
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Affected Aircraft
Bell Model 47J, 47J-2, 47G-3, and 47G-2A helicopters with Float Gear Kit No. 47-706-661 installed.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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