AD 2000-06-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-200 | Airworthiness Directives; Boeing Model 737-200, -200C, -300, and -400 Series Airplanes |
Unsafe Condition
Fatigue cracking of the corners of the door frame and the cross beams of the aft cargo door, which could result in rapid depressurization of the airplane.
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Required Actions
Conduct repetitive high frequency eddy current (HFEC) inspections to detect cracking of the corners of the door frame and the cross beams of the aft cargo door. Perform corrective actions if necessary. Mandate accomplishment of the previously optional terminating action.
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Compliance Time
Within 12,000 total flight cycles after installation of the door.
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Affected Aircraft
Boeing Model 737-200, -200C, -300, and -400 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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