AD 80-21-10

final rule
Data completeness: 70%

Airworthiness Directives; Beech Model 77 Airplanes

AD Number
80-21-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 77 Airworthiness Directives; Beech Model 77 Airplanes

Unsafe Condition

Thread damage on the four bolts and nuts attaching the engine mount to the firewall could compromise the structural integrity of the engine mount attachment.

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

Required Actions

Remove and inspect the four bolts and nuts for thread damage. Replace damaged bolts and nuts with new parts per Table I. Ream attachment holes to .375/.379 inch diameter, clean parts, install bolts with specified torque, and report damaged bolts via FAA Form 8330-2 within five days.

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

Compliance Time

Prior to further flight

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

Affected Aircraft

Beech Model 77 airplanes with serial numbers WA-1 through WA-156, WA-158 through WA-161, WA-163 through WA-171, WA-173, WA-174, WA-177, and WA-178.

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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