AD 2001-09-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-200 and -300 | Airworthiness Directives; Boeing Model 737-200 and -300 Series Airplanes Equipped with Cargo Doors Installed in Accordance With Supplemental Type Certificate (STC) SA2969SO |
Unsafe Condition
Fatigue cracking on the support angles on the lower door jamb could lead to in-flight separation of the main deck cargo door from the airplane.
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Required Actions
Install redesigned lower jamb latch support angles in the main cargo door surround structure. Terminate repetitive inspections for cracking in the radii on the support angles on the lower jamb of the main deck cargo door.
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Compliance Time
Within 50 flight cycles after January 24, 1995, or within 50 flight cycles after installation of STC SA2969SO, whichever occurs later.
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Affected Aircraft
Boeing Model 737-200 and -300 series airplanes equipped with main deck cargo doors installed in accordance with Supplemental Type Certificate (STC) SA2969SO.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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