STC SA00202SE
FAA DRS lists SA00202SE as Current · Reissued, held by BLR Aerospace LLC., for Piper Aircraft PA-31-350. Recorded change: Installation of the Super Chieftain II landing weight increase kit. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of the Super Chieftain II landing weight increase kit.
SA00202SE 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: Piper Aircraft PA-31-350. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-31-350 model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Installation of a maximum payload weight reduction to 7500 lbs in accordance with STC document AMER 2004-01, Revision 0, dated June 30, 2004, or later FAA approved revision. The Airplane Flight Manual Supplement (AFMS) document number AMER 2004-01C, Revision 0, dated October 5, 2004, or later FAA approved revision is required.
FAA holder: Ameristar Jet Charter
Incorporation of change in aircraft weight and balance by supplementing the current aircraft weight and balance manual with Newport Aeronautical Development Report No. NAD 2004-101, Revsion A, dated June 16, 2004, or later FAA approved revision.
FAA holder: Newport Aeronautical Development
Installation of side-facing divan certified for take-off and landing use.
FAA holder: Gulfstream Aerospace Corporation
Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY).
FAA holder: Structural Integrity Engineering