AD 75-14-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Allied Ag Cat Productions, Inc. | G-164 | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164A | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164B | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164B-15T | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164B-20T | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164B-34T | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
| aircraft | Allied Ag Cat Productions, Inc. | G-164B (with 73 inch wing gap) | Airworthiness Directives; Grumman Models G-164, G-164A, and G-164B |
Unsafe Condition
Rudder cables (P/N A1860-35, -36 for G-164 and G-164A; P/N A3860-1, -3 for G-164B) may fray in the cockpit floorboard and chafe strip area, leading to broken strands and potential failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect rudder cables in the cockpit floorboard and chafe strip area for fraying; replace any cables with broken strands using same part number or approved equivalents. Install pulley and bracket P/N AN220-1 and A1839-11/-12 or comply with Grumman Drawing A3371-1/-3 to meet AD requirements.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 20 hours' time in service after July 7, 1977, unless inspected within last 80 hours, and thereafter every 100 hours' time in service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Grumman Models G-164 (S/N 101-400), G-164A (S/N 401-1719), G-164B (S/N 1B-206B and 208B-277B)
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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