AD 64-28-03

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-30 Aircraft

AD Number
64-28-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: December 24, 1964

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-30 Airworthiness Directives; Piper Model PA-30 Aircraft

Unsafe Condition

Progressively stronger stabilator vibration due to the original stabilator torque tube design.

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

Required Actions

Install a new design stabilator torque tube (Piper P/N 22655-07) in accordance with Piper Service Bulletin No. 222A, and remove the 'Do not exceed 205 m.p.h. IAS' placard. Destroy the original torque tube to prevent reinstallation.

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Compliance Time

within 30 hours' time in service after the effective date of this AD

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Affected Aircraft

Piper Model PA-30 Aircraft, Serial Numbers 30-1 through 30-565

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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