AD 91-15-20

final rule
Data completeness: 70%

Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes

AD Number
91-15-20
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-CE-08-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 58 Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. 58A Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. 95-C55 Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. 95-C55A Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. D55 Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. D55A Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. E55 Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes
aircraft Textron Aviation Inc. E55A Airworthiness Directives; Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58 and 58A Airplanes

Unsafe Condition

Cracked engine mounts may cause severe engine vibration and possible separation of the engine from the airplane.

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

Required Actions

Inspect each engine mount in accordance with Beech SB No. 2362, Revision 1. If cracks are found, remove the engine and mount, perform magnetic particle inspection, and either repair with Kit 58-9007-1S if crack length ≤0.52 inches or replace with P/N 96-910010-67 if crack length >0.52 inches. Repeat inspections every 100 hours TIS unless terminated by repair or replacement.

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

Compliance Time

Within 600 hours time-in-service (TIS) or within 100 hours TIS after the effective date of this AD (September 3, 1991), whichever occurs later.

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

Affected Aircraft

Beech Models 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, and 58A airplanes with serial numbers: TC350, TE-1 through TE-1201 (Models 95-C55, 95-C55A, D55, D55A, E55, E55A), and TH-1 through TH-1610 (Models 58 and 58A).

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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