AD 76-10-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Schweizer Aircraft Corporation | 269A | Airworthiness Directives; Hughes Model 269 series helicopters |
| aircraft | Schweizer Aircraft Corporation | 269A-1 | Airworthiness Directives; Hughes Model 269 series helicopters |
| aircraft | Schweizer Aircraft Corporation | 269B | Airworthiness Directives; Hughes Model 269 series helicopters |
| aircraft | Schweizer Aircraft Corporation | 269C | Airworthiness Directives; Hughes Model 269 series helicopters |
Unsafe Condition
Restriction of right lateral cyclic control which will result in the loss of right lateral control of the helicopter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the structural bond between the 269A7142 tube and the 269A7318-1 housing of the lateral cyclic trim control assembly by applying a 75 to 80 pound load. Repair or replace assemblies with slippage prior to further flight. Inspect and repair spare assemblies before installation.
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 after the effective date of this AD
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Affected Aircraft
Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C helicopters equipped with P/N 269A7316-3, -5, -7, -9, or -11 cyclic trim control assembly.
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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