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Fuel systems

STC ST01363AT

FAA DRS lists ST01363AT as Current · Surrendered, held by Aircraft Modification Design Services, for McDonnell Douglas DC-8-62. Recorded change: Increase in aircraft operating weights (max landing weight - 250,000 lbs., max takeoff weight - 342,000 lbs., Max zero fuel wieth - 230,000 lbs.) (DC-8-62 s/n 45925 only). Snapshot dated June 30, 2026.

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Aircraft configurations
1
FAA revision date
FAA status
Current · Surrendered

Recorded modification

What the FAA record covers

ST01363AT 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-8-62. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

FAA record reference

STC number
ST01363AT
Product
Aircraft · Large Multi-Engine
Country
United States
Application date
September 18, 1995
Revision date
December 1, 2009
CFR references
Part 21