AD Amdt-39-10197
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | de Havilland | DHC-6 | Airworthiness Directives; de Havilland DHC-6 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; de Havilland DHC-6 Series Airplanes |
Unsafe Condition
Failure of the fuselage because of cracks in the fuselage side frames at Fuselage Station (FS) 218.125 and FS 219.525.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the fuselage side frames at the referenced FS areas to terminate repetitive inspections. Replace or repair any cracked parts identified during current inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
de Havilland DHC-6 series airplanes subject to AD 78-26-02 requiring repetitive inspections on fuselage side frames at FS 218.125 and FS 219.525.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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