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.

FAA-listed holder

Flint Aero Inc

Aircraft configurations

FAA revision date

February 16, 2007

FAA status

Current · Amended

Recorded modification

What the FAA record covers

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.

SA02410ATFuel systemsRevised Oct 10, 2001

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.

View record

SA5811SWFuel systemsRevised Oct 8, 2001

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

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SA5981SWFuel systemsRevised Oct 8, 2001

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

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ST00976LAFuel systemsRevised Oct 3, 2001

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

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FAA record reference

STC number: SA1809WE
Product: Aircraft · Single-Engine
Country: United States
Application date: September 19, 1968
Revision date: February 16, 2007
CFR references: Part 3, Part 21

What the FAA record covers

Aircraft named in FAA DRS

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).

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.

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 record reference