AD 75-13-02

final rule
Data completeness: 70%

Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes

AD Number
75-13-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 95 Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes
aircraft Textron Aviation Inc. B95 Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes
aircraft Textron Aviation Inc. B95A Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes
aircraft Textron Aviation Inc. D95A Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes
aircraft Textron Aviation Inc. E95 Airworthiness Directives; BEECH Models 95, B95, B95A, D95A, E95 Airplanes

Unsafe Condition

Propeller blade vibration stresses may exceed safe limits due to improper manifold pressure and RPM settings, risking structural failure.

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

Required Actions

Install Beech P/N 95-324079-1 placard and P/N 95-590014-69 flight manual supplement, calibrate tachometers and manifold pressure indicators to specified tolerances, replace non-compliant instruments, and obtain approval for alternate compliance methods.

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

Compliance Time

within the next 100 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 Models 95, B95, B95A, D95A, E95 (Serial Numbers TD-2 through TD-721)

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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