AD 60-01-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Maryland Air Industries, Inc. | F-27 | Airworthiness Directives; Fairchild Models F-27, F-27A, and -27B aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27A | Airworthiness Directives; Fairchild Models F-27, F-27A, and -27B aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27B | Airworthiness Directives; Fairchild Models F-27, F-27A, and -27B aircraft |
Unsafe Condition
Rudder oscillation (rudder walk) creates a flight hazard.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Add a beaded angle to the rudder balance tab trailing edge in accordance with Fairchild Service Bulletin 27-14.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
January 15, 1960
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fairchild Models F-27, F-27A, and F-27B aircraft
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.