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Aircraft performance

STC ST00671AT

FAA DRS lists ST00671AT as Current · Amended, held by Structural Integrity Engineering, for Boeing 727-200 Series. Recorded change: Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY). Snapshot dated June 30, 2026.

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Aircraft configurations
1
FAA revision date
FAA status
Current · Amended

Recorded modification

What the FAA record covers

ST00671AT 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: Boeing 727-200 Series. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

FAA record reference

STC number
ST00671AT
Product
Aircraft · Large Multi-Engine
Country
United States
Application date
January 11, 1995
Revision date
December 29, 2003
CFR references
Part 21