STC ST00617AT
FAA DRS lists ST00617AT as Current · Surrendered, held by Aircraft Modification Design Services, for McDonnell Douglas DC-8-51. Recorded change: Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
ST00617AT identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: McDonnell Douglas DC-8-51. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
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Installation of an 18 gallon auxiliary fuel system in the aft baggage compartment.
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