AD Amdt-39-9184

final rule
Data completeness: 70%

Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes

AD Number
Amdt-39-9184
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-CE-15-AD
FR Citation
60 FR 16366

Applicability

TypeManufacturerModelDetails
aircraft Beech Various Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes

Unsafe Condition

In-flight separation of the elevator trim tab control cable caused by misrouting, which could result in loss of control of the airplane.

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

Required Actions

Inspect (one-time) the elevator trim tab control cables at the top of the vertical stabilizer to ensure correct routing around the pulleys and within the cable guide pins, and replace any cable that is incorrectly routed or chafed.

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

Beech Aircraft Corporation Model 1900D airplanes

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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