AD 74-13-03

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft

AD Number
74-13-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-23-235 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-23-250 (Navy UO-1) Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-24-260 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-24-400 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-30 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft
aircraft Piper Aircraft Inc. PA-39 Airworthiness Directives; Piper Models PA-23-235, PA-23-250, PA-24, PA-24-250. PA-24-260, PA-24-400, PA-30 and PA-39 Aircraft

Unsafe Condition

Corrosion of the stabilator attachment bolts may cause possible hazards in flight.

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

Required Actions

Within the next 100 hours in service, remove and inspect the four stabilator attachment bolts for corrosion. If corrosion is found, replace the bolt, nut, and washer with unused parts of the same part numbers or equivalent corrosion-resistant AN bolts before further flight. Equivalent parts must be FAA approved.

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

Compliance Time

Within the next 100 hours in service, unless previously accomplished, and at intervals not to exceed three years or five hundred hours in service from the last inspection, whichever occurs first.

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

Affected Aircraft

Piper Aircraft Inc. Models PA-23-235 (Serial Nos. 27-1 through 27-4654), PA-23-250 (Navy UO-1), PA-24 (Serial Nos. 24-1 through 24-5047), PA-24-250, PA-24-260, PA-24-400 (Serial Nos. 26-2 through 26-148), PA-30 (Serial Nos. 30-1 through 30-2000), and PA-39 (Serial Numbers 39-1 through 39-155) certificated in all categories.

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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