AD 91-23-01

final rule
Data completeness: 70%

Airworthiness Directives; Beech Models 77 Airplanes

AD Number
91-23-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-CE-10-AD
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Failure of the nose landing gear fork and airplane damage that could result.

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

Required Actions

Fluorescent penetrant inspect the nose landing gear fork for cracks within 50 hours time-in-service after the effective date. If cracks are found, replace the fork and axle assembly with part number 108-820010-653 before further flight. If no cracks, perform subsequent fluorescent penetrant inspections every 500 hours TIS and visual inspections every 100 hours TIS between. Replace if cracks are detected during any inspection.

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

Compliance Time

Within the next 50 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 77 (Skipper) airplanes with serial numbers WA-1 through WA-312 without part number 108-820010-653 nose landing gear fork and axle assembly.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.