AD 2000-02-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | DHC-7-100 | Airworthiness Directives; Bombardier Model DHC-7-100 Series Airplanes |
Unsafe Condition
Fatigue cracking of the baggage door fittings and the support structure, which could result in structural failure and consequent rapid decompression of the airplane during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive high frequency eddy current inspections to detect cracks on the locking pin fittings of the baggage door and locking pin housings of the fuselage. Perform repetitive detailed visual inspections to detect cracks of the inner door structure on all four door locking attachment fittings. Take corrective actions if necessary. Alternatively, revise the Airplane Flight Manual (AFM) and install a placard as a temporary option in certain cases.
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Compliance Time
Not specified in the provided text.
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Affected Aircraft
All Bombardier Model DHC-7-100 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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