AD 55-25-03

final rule
Data completeness: 60%

Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft

AD Number
55-25-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 1A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 2A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 5A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 5BA Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 6A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 6BA Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7AXC Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8A Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8AXC Airworthiness Directives; de Havilland Model 104 "Dove" Aircraft

Unsafe Condition

Corrosion at the main earth connection on the fuselage nose decking near nose frame 4 reduces the efficiency of the earthing point, causing overheating of cockpit lighting cables.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the earth post on the nose floor for protective coating D.T.D. 827. If uncoated or corroded, dismantle the terminal, clean surfaces, replace washers with D.H.S. 439 G corrosion washers and cadmium-plated steel washers as needed, and repaint with D.T.D. 827 paint.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

As soon as practical but not later than February 15, 1956, unless already accomplished.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

de Havilland Aircraft Co., Ltd.'s Model 104 Dove Series 1A, 2A, 5A, and other listed series, all serial numbers.

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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