AD 64-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H.114 Heron Series 2A | Airworthiness Directives; deHavilland Model 114 Heron Series Aircraft |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H.114 Heron Series 2DA | Airworthiness Directives; deHavilland Model 114 Heron Series Aircraft |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H.114 Heron Series 2X | Airworthiness Directives; deHavilland Model 114 Heron Series Aircraft |
Unsafe Condition
Cracking of eye ends used in the rudder and elevator trim tab connecting rod assemblies.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove eye ends with part numbers CM2A and CM2B, conduct the crack test specified in T.N.S. Heron (114) No. CF10, and replace cracked parts before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 150 hours' time in service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
de Havilland Aircraft Co., Ltd.'s D.H.114 Heron Series 2A, 2DA, and 2X models.
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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