AD 2008-16-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Short | Brothers Model SD3-60 | Airworthiness Directives; Short Brothers Model SD3-60 Airplanes |
Unsafe Condition
Failure of the balance weight bracket of the elevator trim tab, which could cause loss of the balance weight, resulting in incorrect trim during takeoff and landing, and reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the welded joints of the balance weight brackets for the elevator trim tabs for cracking using dye penetrant. If no cracking is found, repeat the inspection at intervals not to exceed 4,800 flight hours. Replace any bracket that has not been replaced prior to the accumulation of 28,800 total flight hours or within 6 months after August 3, 2004, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 2 months after August 3, 2004, for the initial inspection.
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Affected Aircraft
All Short Brothers Model SD3-60 airplanes, certificated in any category.
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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