AD 2006-08-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Air | Tractor, Inc. Models AT-802 and AT-802A | Airworthiness Directives; Air Tractor, Inc. Models AT-802 and AT-802A Airplanes |
Unsafe Condition
Fatigue cracking of the wing main spar lower cap at the center splice joint outboard fastener hole, which could result in failure of the spar cap and lead to wing separation and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect (using the eddy current method) the two outboard fastener holes in both of the wing main spar lower caps at the center splice joint for cracks. Repair or replace any cracked spar cap.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Air Tractor, Inc. Models AT-802 and AT-802A airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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