AD 91-12-11

final rule
Data completeness: 70%

Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes

AD Number
91-12-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-CE-44-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 200 Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. 200C Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. 200CT Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. 200T Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. 300 Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. B200 Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. B200C Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. B200CT Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. B200T Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes
aircraft Textron Aviation Inc. F90 Airworthiness Directives: Beech Model F90, 200, B200, 200C, B200C, 200CT, B200CT, 200T, B200T and 300 Airplanes

Unsafe Condition

Cracking and possible blowout of cast acrylic cockpit 'D' side windows could result in decompression injuries.

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

Required Actions

Within 150 hours time-in-service after the effective date, inspect the 'D' side window for cracks, chips, stress crazes, fissure scratches, or other damage. If damage exceeds limits, replace with stretched acrylic window. If no damage, replace cast acrylic window within 12 calendar months. If stretched acrylic windows are unavailable but ordered, operate unpressurized with specified placards until installed.

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

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

Affected Aircraft

Beech Model F90 (S/N LA-2 through LA-236); Models 200 and B200 (S/N BB-2 through BB-1212); Models 200C and B200C (S/N BL-1 through BL-72); Models 200CT and B200CT (S/N BN-1 through BN-4); Models 200T and B200T (S/N BT-1 through BT-30); and Model 300 (S/N FA-2 through FA-56)

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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