AD 72-19-05

final rule
Data completeness: 70%

Airworthiness Directives; Pitts Model S-2A Series Airplanes

AD Number
72-19-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Aviat Aircraft Inc S-2A Airworthiness Directives; Pitts Model S-2A Series Airplanes

Unsafe Condition

Failure of the horizontal stabilizer leading edge support tube due to cracks in the vicinity of the AN3 bolt holes.

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

Required Actions

Inspect the stabilizer leading edge support tube for cracks near AN3 bolt holes; replace if cracks are found. Cut the tube ends to specified dimensions, redrill bolt holes, apply zinc chromate, reassemble, and stencil 'No lift' on stabilizers.

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 the effective date of this AD

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

Affected Aircraft

Pitts Model S-2A series Airplanes, serial numbers 2001 through 2030.

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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