AD Amdt-39-9449
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 of the main deck cargo door may cause in-flight separation of the door from the airplane.
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Required Actions
Perform a visual inspection to detect cracking in the radii on the support angles on the lower jamb of the main deck cargo door within 50 flight hours or cycles after installation of STC SA2969SO. Replace cracked parts with new parts. Submit requests for alternative methods of compliance to the Atlanta Aircraft Certification Office.
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Compliance Time
Within 50 flight hours 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 per STC SA2969SO.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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