AD 2000-23-13

final rule
Data completeness: 70%

Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes

AD Number
2000-23-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-364-AD
FR Citation
65 FR 69439

Applicability

TypeManufacturerModelDetails
aircraft Israel Various Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes

Unsafe Condition

Incorrect installation of the tie rod through the dust shield and both jackscrew assemblies on the horizontal stabilizer trim actuator can lead to jamming or disconnection of the actuator, resulting in reduced pitch control of the airplane.

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

Required Actions

Inspect the tie rod installation through the dust shield and both jackscrew assemblies on the horizontal stabilizer trim actuator. Measure the distance between the bottom of the dust shield and the housing of the horizontal stabilizer actuator. Take corrective action if necessary to ensure proper installation.

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

Israel Aircraft Industries, Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes, 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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