STC SA02204AK
FAA DRS lists SA02204AK as Current · Issued, held by Wagner Dane, for New Piper Aircraft PA-18, New Piper Aircraft PA-18-105 (Special), and New Piper Aircraft PA-18-125 (Army L-21A), and 15 more aircraft configurations. Recorded change: Fabrication of replacement engine exhaust system assembly. Limited to airplanes equipped with FAA approved installations of Textron Lycoming O-320 model series engines having a compression ratio of 8.5:1 and a rated power of 160 hp for all operations. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Fabrication of replacement engine exhaust system assembly. Limited to airplanes equipped with FAA approved installations of Textron Lycoming O-320 model series engines having a compression ratio of 8.5:1 and a rated power of 160 hp for all operations.
SA02204AK 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: New Piper Aircraft PA-18, New Piper Aircraft PA-18-105 (Special), and New Piper Aircraft PA-18-125 (Army L-21A), and 15 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact New Piper Aircraft PA-18 and New Piper Aircraft PA-18-105 (Special), and 16 more aircraft configurations model, serial range, and configuration?
- 02Which powerplant configuration, limits, instruments, and maintenance data apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
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