AD 92-08-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-8-61 | Airworthiness Directives; McDONNELL DOUGLAS DC-8-61, -62, -63, and -73 Series Airplanes |
| aircraft | The Boeing Company | DC-8-62 | Airworthiness Directives; McDONNELL DOUGLAS DC-8-61, -62, -63, and -73 Series Airplanes |
| aircraft | The Boeing Company | DC-8-63 | Airworthiness Directives; McDONNELL DOUGLAS DC-8-61, -62, -63, and -73 Series Airplanes |
| aircraft | The Boeing Company | DC-8-73 | Airworthiness Directives; McDONNELL DOUGLAS DC-8-61, -62, -63, and -73 Series Airplanes |
Unsafe Condition
Reduced structural integrity of the cargo compartment and possible loss of cargo restraint capability during emergency landing conditions.
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Required Actions
Modify the cargo area subfloor structure and install fuselage overhead external doubler straps per Rosenbalm Aviation Service Bulletin DC-8 51-01. Install transverse cusp membranes and re-attach the longitudinal cusp membrane to the seat track outboard flange per Rosenbalm Aviation Service Bulletin DC-8 51-02.
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Compliance Time
within 180 days after the effective date of this AD, unless accomplished previously
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Affected Aircraft
McDONNELL DOUGLAS DC-8-61, -62, -63, and -73 series airplanes equipped with cargo conversion modification installed per STC SA1802SO
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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