AD 2000-26-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dornier | Model 328-100 Series | Airworthiness Directives; Dornier Model 328-100 Series Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements could adversely affect the structural integrity of these airplanes.
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Required Actions
Within 30 days after the effective date, revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness by incorporating Revision 13 of the Dornier 328 Airworthiness Limitations Document and the listed Temporary Revision (TR) documents. No alternative inspections or intervals may be approved for the specified structural elements unless approved by the FAA.
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Compliance Time
Within 30 days after the effective date of February 7, 2001.
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Affected Aircraft
All Dornier Model 328-100 series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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