AD 2003-04-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | APEX | Various | Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes |
Unsafe Condition
Structural cracking in the upper and lower wing spars 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
Install an inspection opening in the wing, repetitively inspect the upper and lower wing spars for structural cracking, and repair any cracks as required. Restrict the entry speed for flick maneuvers to a reduced value, insert a copy of the AD into the flight manual, and install a placard in the cockpit indicating the speed restriction. Temporarily reduce the load factor limits prior to the initial inspection.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
APEX Aircraft Model CAP 10B airplanes
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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