AD 62-11-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Schweizer Aircraft Corporation | 269A | Airworthiness Directives; Hughes Model 269A Helicopters |
Unsafe Condition
Reduction in maximum horsepower due to changes in engine camshafts necessitates revised operating limitations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the FAA approved Flight Manual to incorporate new operating limitations as set forth in Hughes Model 269A Flight Manual revised page 24A. Compliance required within 50 hours' time in service after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 50 hours' time in service after the effective date of this directive
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Schweizer Aircraft Corporation Model 269A Helicopters equipped with Lycoming Model 0-360-C2D engines of serial numbers L-3816-36 through L-4599-36 and L-4601-36 through L-4640-36
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.