STC SA1809WE
FAA DRS lists SA1809WE as Current · Amended, held by Flint Aero Inc, for Cessna Aircraft 150D, Cessna Aircraft 150E, and Cessna Aircraft 150F, and 21 more aircraft configurations. Recorded change: Installation of one twelve-gallon auxiliary fuel tank in each outboard wing panel. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of one twelve-gallon auxiliary fuel tank in each outboard wing panel.
SA1809WE 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 150D, Cessna Aircraft 150E, and Cessna Aircraft 150F, and 21 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 150D and Cessna Aircraft 150E, and 22 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
Replace existing Auxiliary Electric Standby Fuel Pump with PMA Products, Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v), 1A15-s/n 24-3642, 24-4000 through 24-4782, 24-4784 through 24-4803, 2A13-s/n 28-7690001 through 28-7990626, 28-8090001 and up(14v).
FAA holder: PMA Products, Inc.
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.
FAA holder: RAM Aircraft Limited Partnership
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.
FAA holder: RAM Aircraft Limited Partnership
Installation of a 2100 US Gallon Retardant Tank system. Approval applies to basic aircraft of specified models modified with STC SA4-1100, installation of Allison turboprop engines; STC SA3574WE, installation of gross weight increase kit; and STC SA3294WE, installation of max zero fuel weight increase kit.
FAA holder: Conair Aviation Ltd