AD 70-25-04

final rule
Data completeness: 70%

Airworthiness Directives; BEECH Model 65-90 Airplanes

AD Number
70-25-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 65-90 Airworthiness Directives; BEECH Model 65-90 Airplanes

Unsafe Condition

Cracking of wing center section and other wing panel front spar carry through structural components.

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

Required Actions

Visually inspect lower wing skin adjacent to outer wing panel front spar attachment fittings for cracks per Beechcraft Service Instruction 0394-018 within 100 hours' time in service after December 5, 1970. Repeat inspections at intervals not exceeding 100 hours. Inspect wing attachment fittings with visual and dye penetrant methods every 500 hours' time in service. If cracks found, replace affected parts as specified in the service instruction. Perform additional inspections per paragraphs B, D, and E with specified methods and intervals. Report findings to FAA.

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 December 5, 1970

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

Affected Aircraft

BEECH Model 65-90 airplanes with serial numbers LJ-1 through LJ-67 and 5,000 or more hours' time in service.

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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