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Aircraft performance

STC SA568SW

FAA DRS lists SA568SW as Current · Reissued, held by Air Repair Inc, for Cessna Aircraft 305A (USAF 0-1A). Recorded change: Increase gross weight to 2,300 pounds, oil system mod per Option One Installation Instructions.. Snapshot dated June 30, 2026.

FAA-listed holder
Air Repair Inc
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

Increase gross weight to 2,300 pounds, oil system mod per Option One Installation Instructions..

SA568SW 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: Cessna Aircraft 305A (USAF 0-1A). Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Cessna Aircraft 305A (USAF 0-1A)5A5

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Cessna Aircraft 305A (USAF 0-1A) model, serial range, and configuration?
  2. 02Which limits, loading assumptions, performance data, and supplements 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?

Related aircraft performance STCs

SA02208SEAircraft performance

Fabrication of AeroAcoustics Aircraft Systems (AASI) Aircraft Payload Extender short field landing performance (APE STOL) system in accordance with AASI Master Drawing List No. AA2230, Revision NC, dated March 15, 2011, or later Federal Aviation Administration (FAA) approved revision; and installation of APE STOL system in accordance with AASI Installation Manual No. AA2231, Revision B, dated December 27, 2011, or later FAA-approved revision.

FAA holder: AeroAcoustics Aircraft Systems Inc.

View record