AD 73-26-08

final rule
Data completeness: 70%

Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes

AD Number
73-26-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 95-55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. 95-A55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. 95-B55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. 95-C55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. D55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. D55A Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. E55 Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes
aircraft Textron Aviation Inc. E55A Airworthiness Directives: BEECH Models 95-55, 95-A55, 95-B55, 95-C55, D55, D55A, E55 and E55A Airplanes

Unsafe Condition

The roll and pitch servo clamps may have slipped or insufficient torque on the clamp bolts, leading to binding or restrictions between the bridle cables and aircraft components, or improper bridle cable tension.

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

Required Actions

Inspect the roll and pitch bridle cables and clamps for slippage and binding, verify bridle cable tension matches attached control cables, and torque clamp bolts to 55 ±5 in-lbs with a minimum .005 inch gap between clamp halves.

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

Compliance Time

within 25 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 95-55, 95-A55, 95-B55 (Serial Numbers TC-1 through TC-1573 except TC-350); 95-C55, D55, D55A, E55 and E55A (Serial Numbers TE-1 through TE-919 and TC-350), equipped with the EDO-AIRE Mitchell AK-292 Autopilot.

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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