AD 62-02-06

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-25 Aircraft

AD Number
62-02-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: January 18, 1962

Applicability

TypeManufacturerModelDetails
aircraft Lavia Argentina S.A. (Laviasa) PA-25 Airworthiness Directives; Piper Model PA-25 Aircraft

Unsafe Condition

Aluminum front spar wing-to-fuselage attachment fittings (Piper P/N's 61111-00 and 61111-01) may fail due to stress corrosion cracking.

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

Required Actions

Replace aluminum fittings with steel forgings (Piper P/N's 60113-00 and 60113-01) or equivalent parts approved by FAA. Compliance must follow Piper Service Bulletin No. 206.

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

Compliance Time

Within the next 25 hours' time in service after the effective date of this AD, but not later than February 15, 1962

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

Affected Aircraft

Lavia Argentina S.A. (Laviasa) Model PA-25 Aircraft, Serial Numbers 25-1 to 25-619 Inclusive, 25-622, 25-623, 25-625, and 25-626.

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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