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Fuel systems

STC SA5510NM

FAA DRS lists SA5510NM as Current · Amended, held by Structural Integrity Engineering, for McDonnell Douglas DC-8-61. Recorded change: Modification in accordance with FAA approved SIE Drawing List 9000 N/C,, dated August 7, 1991, or later FAA approved revisions, to permit an increased maximum zero fuel weight (MZFW), and maximum landing weight (MLW) of DC-8-61 airplanes. Snapshot dated June 30, 2026.

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FAA-listed holder
Structural Integrity Engineering
Aircraft configurations
1
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

SA5510NM 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-8-61. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas DC-8-614A25

Related fuel systems STCs

FAA record reference

STC number
SA5510NM
Product
Aircraft · Large Multi-Engine
Country
United States
Application date
January 22, 1990
Revision date
December 29, 2003
CFR references
Part 21, Part 36