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Fuel systems

STC SA09897AC

FAA DRS lists SA09897AC as Current · Issued, held by T-34 Spar Corporation, for Textron Aviation D45 (Military T-34B). Recorded change: Modification of fuel return system to bypass the header tank. Snapshot dated June 30, 2026.

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FAA-listed holder
T-34 Spar Corporation
Aircraft configurations
1
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

SA09897AC 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: Textron Aviation D45 (Military T-34B). Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Textron Aviation D45 (Military T-34B)5A3

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SA1-368Fuel systems

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SA144EAFuel systems

Approval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20, 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15, 1964 is required.

FAA holder: D'Shannon Products Ltd.

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FAA record reference

STC number
SA09897AC
Product
Aircraft · Single-Engine
Country
United States
Application date
September 24, 2018
Revision date
February 7, 2019
CFR references
Part 3, Part 21