AD 58-23-03

final rule
Data completeness: 60%

Airworthiness Directives; Mooney Model M-20 Aircraft

AD Number
58-23-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Mooney Aviation Company Inc M20 Airworthiness Directives; Mooney Model M-20 Aircraft

Unsafe Condition

Failures of the aileron counterbalance buttweld at the aileron spar have occurred.

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

Required Actions

Determine if a 3/8 inch O.D. x 0.028 inch x 3 inch steel reinforcing brace is installed. If not, remove paint from the welded joint and inspect for cracks, reweld the joint if cracks are present, and install the specified 4130 steel tubular brace trimmed to fit.

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

Compliance Time

As soon as practicable but not later than December 15, 1958.

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

Affected Aircraft

Mooney Model M-20 Aircraft Serial Numbers 1002 Through 1051.

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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