AD 2013-02-13

final rule
Data completeness: 70%

Airworthiness Directives; Piper Aircraft, Inc.

AD Number
2013-02-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-0731
FR Citation
78 FR 7642

Applicability

TypeManufacturerModelDetails
aircraft The New Piper Aircraft Inc. PA-28 Airworthiness Directives; Piper Aircraft, Inc.
aircraft Piper Aircraft Airworthiness Directives; Piper Aircraft, Inc.

Unsafe Condition

Reports of control cable assembly failures that may lead to failure of the horizontal stabilator control system and could result in loss of pitch control.

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

Required Actions

Inspect the stabilator control system and replace parts as necessary.

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

Compliance Time

Before further flight

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

Affected Aircraft

Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 airplanes, all serial numbers, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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