AD 67-12-06

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes

AD Number
67-12-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: April 4, 1967

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-140 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes
aircraft Piper Aircraft Inc. PA-28-150 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes
aircraft Piper Aircraft Inc. PA-28-160 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes
aircraft Piper Aircraft Inc. PA-28-180 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes
aircraft Piper Aircraft Inc. PA-28-235 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes
aircraft Piper Aircraft Inc. PA-32-260 Airworthiness Directives; Piper Models PA-28 and PA-32 Series Airplanes

Unsafe Condition

Internal corrosion resulting from inadequate corrosion protection of certain open end steel tube assemblies, including aileron balance weights, rudder horn assemblies, and stabilator balance weights.

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

Required Actions

Conduct a close visual inspection of the interior of the open end tubes for protective coating and corrosion per Piper Service Bulletin No. 240 or approved method. Remove corrosion, replace corroded parts if necessary, and apply zinc chromate primer if corrosion is present.

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

Compliance Time

Prior to but not later than July 31, 1967 (Group I), July 31, 1968 (Group II), or July 31, 1969 (Group III), extendable up to 30 days by FAA inspector to coincide with annual inspection.

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

Affected Aircraft

Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, and PA-32-260 with specified serial ranges as outlined in Groups I, II, and III.

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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