STC SA8334SW
FAA DRS lists SA8334SW as Current · Reissued, held by Peter C. Morrison, for Piper Aircraft PA-22, Piper Aircraft PA-22-108, and Piper Aircraft PA-22-135, and 2 more aircraft configurations. Recorded change: Installation of dual toe brakes including rudder pedals, linkages and torque tubes. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of dual toe brakes including rudder pedals, linkages and torque tubes.
SA8334SW 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-22, Piper Aircraft PA-22-108, and Piper Aircraft PA-22-135, and 2 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Piper Aircraft PA-22 and Piper Aircraft PA-22-108, and 3 more aircraft configurations model, serial range, and configuration?
- 02Which control configuration, rigging, limitations, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related flight controls STCs
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Modification in the leading edge slat and flap configurations.
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Installation of Elevator Replacement Trailing Edge.
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Installation of a swept vertical stabilizer and rudder assembly.
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