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Aircraft structures

STC SA01130SE

FAA DRS lists SA01130SE as Current · Issued, held by Sterling Paul M, for Piper Aircraft PA-38-112. Recorded change: Sterling Aviation Technologies, Inc. Kit No. SA500 Piper PA-38-112 Tomahawk Fatigue Life Extension Wing Spar Modification. Snapshot dated June 30, 2026.

FAA-listed holder
Sterling Paul M
Aircraft configurations
1
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

Sterling Aviation Technologies, Inc. Kit No. SA500 Piper PA-38-112 Tomahawk Fatigue Life Extension Wing Spar Modification.

SA01130SE 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-38-112. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Piper Aircraft PA-38-112A18SO

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Piper Aircraft PA-38-112 model, serial range, and configuration?
  2. 02Which configuration, loads, materials, inspections, and damage limits 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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