AD 74-10-01

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-23-250 Airplanes

AD Number
74-10-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Cracks developing in the outboard flap hinges (part numbers 17103-04 and 17103-05) could cause asymmetric flap conditions.

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

Required Actions

Inspect outboard flap hinges (part numbers 17103-04 and 17103-05) using a 10-power magnifying glass or equivalent method approved by the FAA. Clean hinges before inspection. Replace cracked hinges with unused parts of the same part numbers or FAA-approved equivalents before further flight. Compliance is not required if Piper Kits 760 861 (right) and 760 817 (left) are installed.

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

Compliance Time

Within the next 25 hours in service after December 31, 1975, and every 100 hours thereafter. Compliance time may be increased upon FAA approval with substantiating data.

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

Affected Aircraft

Piper Model PA-23-250 (Navy UO-1) airplanes with serial numbers 27-3050, 27-3154 to 27-7405330.

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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