AD 63-23-01

final rule
Data completeness: 70%

Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft

AD Number
63-23-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC3-G102 Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3-G102A Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3-G103A Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3-G202A Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3A-S1C3G Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3A-S1CG Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3A-S4C4G Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3A-SC3G Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3A-SCG Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft
aircraft The Boeing Company DC3C-R-1830-90C Airworthiness Directives; DOUGLAS all DC-3, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, R4D Series except R4D-8 aircraft

Unsafe Condition

Cracks in the wing upper attach angles and doublers along the radius of the bent-up flange and between bolt holes could result in structural failure.

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

Required Actions

Inspect wing upper attach angles for cracks using a 4-power magnifying glass within 50 hours' time in service after the effective date. Reinspect at intervals not exceeding 450 hours' time in service. Replace cracked parts before further flight. At next wing removal, inspect doublers and angles with 6-power magnifying glass or dye penetrant, and maintain specified tolerances during replacement. Use specified jigs or FAA-approved equivalents for alignment.

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

Compliance Time

Compliance required as indicated.

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

Affected Aircraft

Douglas DC-3 series and military variants including C-41, C-47, C-48, C-49, C-50, C-51, C-52, C-53, C-68, C-117A, R4D series except R4D-8 aircraft.

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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