AD 2003-07-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Quality | Aerospace, Inc. S2R Series and Model 600 S2D | Airworthiness Directives; Quality Aerospace, Inc. S2R Series and Model 600 S2D Airplanes |
Unsafe Condition
Fatigue cracking in the lower spar caps could result in the wing separating from the airplane, leading to loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the 1/4-inch and 5/16-inch bolt hole areas on the lower spar caps for fatigue cracking. Replace or repair any lower spar cap where fatigue cracking is found. Report any fatigue cracking found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in AD 2000-11-16, as extended by this amendment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Quality Aerospace, Inc. S2R series and Model 600 S2D airplanes, including additional airplanes manufactured with a similar design to those previously affected by AD 2000-11-16.
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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