STC SA448GL
FAA DRS lists SA448GL as Current · Reissued, held by Shadin Avionics, for Cessna Aircraft 411, Cessna Aircraft 401B, and Cessna Aircraft 401, and 6 more aircraft configurations. Recorded change: Installation of a Shadin Co. 910502, 910504, or 910514 fuel flow indicating system. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of a Shadin Co. 910502, 910504, or 910514 fuel flow indicating system.
SA448GL 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 411, Cessna Aircraft 401B, and Cessna Aircraft 401, and 6 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft 411 and Cessna Aircraft 401B, and 7 more aircraft configurations model, serial range, and configuration?
- 02Which tanks, plumbing, usable-fuel assumptions, 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 fuel systems STCs
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Increase maximum ramp weight to 7610 pounds; maximum takeoff weight to7560 pounds; maximum landing weight is 7200 pounds; decrease zero fuel weight to 6533 pounds; install winglets.
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Increase maximum ramp weight to 7610 pounds, maximum takeoff weight to 7560 pounds, maximum landing weight is 7200 pounds, maximum zero fuel weight is 6533 pounds.
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