AD 2014-02-03

final rule
Data completeness: 80%

Airworthiness Directives; Beechcraft Corporation Airplanes

AD Number
2014-02-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0611
FR Citation
79 FR 5254

Applicability

TypeManufacturerModelDetails
aircraft Beechcraft Corporation Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition

Elevator bob-weight (stabilizer weight) traveling past its stop bolt may allow the attaching linkage to move over-center and lead to reduced nose down elevator control.

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

Required Actions

Inspect the elevator bob-weight and attaching linkage for correct installation and for damage or deformation to the weight and/or weight bracket with corrective action as necessary. Install the secondary elevator bob-weight stop bolt, Kit 114-5060.

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

Compliance Time

Within 600 flight hours time-in-service (TIS) from the effective date of this AD.

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

Affected Aircraft

Beechcraft Corporation Models 1900, 1900C, and 1900D airplanes, as listed in Table 1 of the AD.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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