AD 70-07-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 1A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 2A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 5A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 5BA | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 6A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 6BA | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 7A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 7AXC | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 8A | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
| aircraft | de Havilland Aircraft Co., Ltd., The | D.H. 104 Dove Series 8AXC | Airworthiness Directives; Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" Series Airplanes |
Unsafe Condition
Internal corrosion of the tailplane rear spar to rear fuselage bulkhead support struts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct an x-ray inspection of the two tailplane rear spar to rear fuselage bulkhead support struts for internal corrosion. If corrosion is found, replace each corroded strut with a serviceable strut of the same part number. Report inspection results within 30 days.
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
Hawker Siddeley Models DH-104 "Dove" and DH-114 "Heron" series airplanes.
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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