STC ST00782AT
FAA DRS lists ST00782AT as Current · Reissued, held by Structural Integrity Engineering, for Boeing 727-100 Series. Recorded change: Approval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY). Snapshot dated June 30, 2026.
FAA-listed holder
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued
Recorded modification
What the FAA record covers
ST00782AT 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 727-100 Series. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related fuel systems STCs
Increase in aircraft operating weights(maximum landing weight - 240,000 lbs., maximum zero fuel weight - 224,000 lbs.) (DC-8F-54 S/N 45637).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs).
FAA holder: Aircraft Modification Design Services
FAA record reference
- STC number
- ST00782AT
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- May 23, 1995
- Revision date
- December 29, 2003
- CFR references
- Part 21