AD 70-23-02

final rule
Data completeness: 70%

Airworthiness Directives; de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC Airplanes

AD Number
70-23-02
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; de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 7AXC Airworthiness Directives; de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8A Airworthiness Directives; de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC Airplanes
aircraft de Havilland Aircraft Co., Ltd., The D.H. 104 Dove Series 8AXC Airworthiness Directives; de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC Airplanes

Unsafe Condition

Cracks in the wing lower main spar cap in the region of rib 4 and loosened tank door attachment bolts at Wing Sta. 0-40.

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

Required Actions

Within specified timeframes, visually inspect the lower main spar cap using a 4 power glass and/or dye penetrant methods, check tank door bolts for tightness, repair cracks prior to further flight, replace out-of-tolerance nut plates, and perform periodic inspections at intervals not exceeding specified hours time in service. Inspections must follow Strato Engineering Service Bulletin APA-3 or equivalent procedures.

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

Compliance Time

Within the next 10 hours time in service after receipt of telegram dated October 23, 1970, and thereafter at intervals not to exceed twenty hours time in service. For certain modifications, inspections must be repeated at intervals not exceeding 500 and 250 hours time in service.

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

Affected Aircraft

de Havilland Aircraft Company Ltd Model D.H. 104 Dove Series 7A, 8A, 7AXC, 8AXC airplanes modified per STC SA1554WE or 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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