AD Amdt-39-12247

final rule
Data completeness: 70%

Airworthiness Directives; Air Tractor, Inc. AT-400, AT-500, and AT-800 Series Airplanes

AD Number
Amdt-39-12247
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-CE-72-AD
FR Citation
66 FR 29900

Applicability

TypeManufacturerModelDetails
aircraft Air Tractor, Inc. AT-400, AT-500, and AT-800 Series Airworthiness Directives; Air Tractor, Inc. AT-400, AT-500, and AT-800 Series Airplanes

Unsafe Condition

Fatigue cracks in the wing lower spar cap, originating in the outboard 3/8-inch bolthole, could result in the wing separating from the airplane during flight.

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

Required Actions

Inspect the wing lower spar cap using eddy current methods for airplanes at or over the lower safe life. Replace or modify the wing lower spar cap if cracks are found. Terminate inspections when parts become available or after performing three repetitive inspections.

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

Compliance Time

Before further flight for airplanes at or over the lower safe life.

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

Affected Aircraft

Air Tractor, Inc. AT-400, AT-500, and AT-800 series airplanes, excluding those AT-800 series airplanes equipped with the factory-supplied part number 80540 computerized fire gate.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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