AD 76-06-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Scheibe-Flugzeugbau GmbH | SF-26A Standard | Airworthiness Directives; Scheibe Flugzeugbau Model SF 26A Gliders |
Unsafe Condition
Possible loss of lateral control due to cracks in the aileron bellcranks near the weld of the middle bearing bushing.
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Required Actions
Visually inspect the aileron bellcranks near the weld of the middle bearing bushing for cracks using a magnifying glass of at least 5 power, in accordance with Scheibe Technical Note No. 232-1/75 or FAA-approved equivalent. Inspections must be done within the next 10 hours time in service after the effective date and every 50 hours thereafter. Repair any cracked bellcrank before further flight per FAR 43.13.
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Compliance Time
Within the next 10 hours time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours time in service from the last inspection.
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Affected Aircraft
Scheibe Flugzeugbau GmbH Model SF 26A gliders certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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