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Fuel systems

STC ST02032AT

FAA DRS lists ST02032AT as Current · Surrendered, held by Aircraft Modification Design Services, for McDonnell Douglas DC-8-62F. Recorded change: Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs). Snapshot dated June 30, 2026.

FAA-listed holder
Aircraft Modification Design Services
Aircraft configurations
1
FAA revision date
FAA status
Current · Surrendered

Recorded modification

What the FAA record covers

Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs).

ST02032AT 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-8-62F. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas DC-8-62F4A25

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact McDonnell Douglas DC-8-62F model, serial range, and configuration?
  2. 02Which tanks, plumbing, usable-fuel assumptions, and inspections apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

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