AD 72-10-03

final rule
Data completeness: 70%

Airworthiness Directives; Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC Airplanes

AD Number
72-10-03
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 7A Airworthiness Directives; Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7AXC Airworthiness Directives; Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8A Airworthiness Directives; Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8AXC Airworthiness Directives; Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC Airplanes

Unsafe Condition

Fatigue failure of a wing main spar lower attach fitting or of a wing center section lower spar boom

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

Required Actions

Replace each wing lower spar attach fitting P/N CPD 2004 installed under STC SA1747WE at or before 1800 hours' time in service, and at intervals thereafter not to exceed 1800 hours' time in service. Replace the wing center section lower spar boom under specified drawings or approved modification. Discontinue replacements if modified with STC SA2438WE or approved alternative.

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

Compliance Time

prior to further flight after the effective date of this AD

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

Affected Aircraft

Hawker Siddeley de Havilland Model D.H. 104 Series 7A, 7AXC, 8A, 8AXC airplanes modified per STC SA1747WE

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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