AD 97-15-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aeromot-Industria Mecanico Metalurgica Ltda. | AMT-200 (Super Ximango) | Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Sailplanes |
| aircraft | Aeromot-Industria Mecanico Metalurgica Ltda. | AMT-200S (Super Ximango) | Airworthiness Directives; Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 Powered Sailplanes |
Unsafe Condition
Failure of the forward horizontal stabilizer bolt, part number 53451, caused by a low cycle fatigue crack induced by over torquing the bolt.
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Required Actions
Immediately inspect the forward horizontal stabilizer front bolt using non-destructive testing (NDT) methods for defects (scratches, damaged threads, or surface cracks). Replace the bolt immediately if defective or at a certain time period if not defective. Alternatively, replace the bolt immediately instead of performing the NDT inspection.
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Compliance Time
Required as indicated after the effective date of this AD (August 15, 1997), except for those receiving it by priority letter on July 11, 1997, which made the actions effective immediately upon receipt.
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Affected Aircraft
Aeromot-Industria Mecanico Metalurgica Ltda. Model AMT-200 powered sailplanes, serial numbers 200.057, 200.058, 200.059, 200.063, 200.065, 200.066, 200.071, and 200.072.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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