AD 54-24-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Scotts-Bell 47 Inc | 47B | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47B3 | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47D | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47D1 | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47E | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
| aircraft | Scotts-Bell 47 Inc | 47G | Airworthiness Directives; Bell Model 47B, 47B3, 47D, 47D1, 47E and 47G Helicopters |
Unsafe Condition
Improper installation of the antitorque pedal assembly for dual controls could lead to loss of antitorque control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install two stop assemblies, part number 47-722-165-1, to preclude improper installation of the antitorque pedal assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
next 25-hour inspection
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bell Model 47B, 47B3, 47D, 47D1, 47E, and 47G helicopters except serial numbers 1286, 1287, 1294, 1295, and 1299 and subsequent.
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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