AD 94-01-01

final rule
Data completeness: 70%

Airworthiness Directives: Beech Aircraft Corporation Models B300 and B300C Airplanes

AD Number
94-01-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-CE-43-AD
FR Citation
Federal Register: January 13, 1994 (Volume 59, Number 9)

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. B300 Airworthiness Directives: Beech Aircraft Corporation Models B300 and B300C Airplanes
aircraft Textron Aviation Inc. B300C Airworthiness Directives: Beech Aircraft Corporation Models B300 and B300C Airplanes

Unsafe Condition

Cracking of cabin seat frames around the welded-in bushings could cause seat separation from its base during an accident, resulting in occupant injury.

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

Required Actions

Inspect each cabin seat frame for cracks and repair any cracks prior to further flight. Modify all cabin seat frames by incorporating Beech Kit No. 303-307 following applicable service bulletins.

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

Compliance Time

within the next 150 hours time-in-service after the effective date of this AD, unless already accomplished

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Affected Aircraft

Beech Aircraft Corporation Models B300 (serial numbers FL-1 through FL-76) and B300C (serial numbers FM-1, FM-2, and FM-3) that do not have all nine cabin seats modified with Beech Kit No. 303-307.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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