AD 64-21-05

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-30 and PA-23-250 Aircraft

AD Number
64-21-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: September 15, 1964

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-23-250 (Navy UO-1) Airworthiness Directives; Piper Model PA-30 and PA-23-250 Aircraft
aircraft Piper Aircraft Inc. PA-30 Airworthiness Directives; Piper Model PA-30 and PA-23-250 Aircraft

Unsafe Condition

Propeller failure due to insufficient replacement of governor relief valve springs as per Hartzell Service Bulletin No. 88, leading to continued operational risks.

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

Required Actions

Service propeller governors in accordance with Hartzell Service Bulletin No. 88A dated August 4, 1964, within 10 hours' time in service after the effective date of this AD. Additionally, comply with prior Service Bulletin No. 88 if not already done.

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

Compliance Time

within 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

Piper Model PA-30 and PA-23-250 aircraft equipped with specific Hartzell propellers: PA-30 with HC-E2YL-2B/7663-4 and PA-23-250 with HC-E2YK-2RB/8465-7R propellers.

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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