AD 2000-24-04

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company Beech Models A36, B36TC, and 58 Airplanes

AD Number
2000-24-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-CE-06-AD
FR Citation
65 FR 75597

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company Beech Models A36 Airworthiness Directives; Raytheon Aircraft Company Beech Models A36, B36TC, and 58 Airplanes

Unsafe Condition

Misrouted rudder control cables, leading to guard pin wear or fraying of the cables with loss of rudder control.

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

Required Actions

Inspect rudder control cables for proper routing; replace worn or damaged guard pins; inspect and replace worn or damaged pulley brackets; replace misrouted rudder control cables.

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

Compliance Time

Within 50 flight hours after January 5, 2001, for inspection; before further flight after inspection for replacements.

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

Affected Aircraft

Raytheon Aircraft Company Beech Models A36 (serial numbers E-2519 through E-3140), B36TC (serial numbers EA-501 through EA-608), and 58 (serial numbers TH-1576 through TH-1838).

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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