FAA STC category

Fuel systems STCs

Fuel tanks, cells, plumbing, transfer, measurement, and refueling changes. This directory contains 1,199 selected records listed with status Current in the June 30, 2026 FAA DRS snapshot and links every entry to its source.

Showing 1,081–1,199 of 1,199Page 10 of 10

SA00172BOFuel systemsRevised Jul 11, 2003

Installation of Piper PA-18 right wing fuel tank. Limited to installation on PA-16, serial number 16-403 ONLY.

FAA holder: Lagace Donald O.

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SA02055ATFuel systemsRevised Jul 3, 2003

Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions, Revision D, dated January 13, 2000, or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII, Revision C, dated August 17, 1999, or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs.

FAA holder: Aviation Enterprises

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SH408NE-DFuel systemsRevised Jun 30, 2003

Replacement of auxiliary fuel boost pumps with Parker Hannifin-Airborne centrifugal boost pumps.

FAA holder: American Eurocopter Corporation

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SH6022SW-DFuel systemsRevised Jun 30, 2003

Installation of a Michigan Dynamic airframe fuel filter.

FAA holder: American Eurocopter Corporation

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SH7695SW-DFuel systemsRevised Jun 30, 2003

Installation of a Shaw Aero Devices fuel filler.

FAA holder: American Eurocopter Corporation

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SH7697SW-DFuel systemsRevised Jun 30, 2003

Installation of visible fuel quantity indicator to indicate 80% or more fuel quantity.

FAA holder: American Eurocopter Corporation

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SH82NE-DFuel systemsRevised Jun 30, 2003

Installation of differential fuel pressure switch. Also compatible with BO-105C as modified by Carson Helicopters' STC SH1025EA.

FAA holder: American Eurocopter Corporation

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SH920NE-DFuel systemsRevised Jun 30, 2003

Installation of Main Fuel Tank Pump Switch off Advisory Light System.

FAA holder: American Eurocopter Corporation

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SA561WEFuel systemsRevised Jun 20, 2003

12.7-gallon auxiliary fuel tank.

FAA holder: Robertson Lorene E

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SB01836CHFuel systemsRevised May 23, 2003

Replace basket/burner and fuel tanks with a Cameron Balloons basket. Limited to installation on model Colt 240A, serial number 2285 ONLY.

FAA holder: Cameron Balloons US

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SA01214SEFuel systemsRevised May 12, 2003

Fabrication of Steve's Aircraft Fuel Vent System.

FAA holder: Steve's Aircraft

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SH4134SWFuel systemsRevised Apr 28, 2003

Installation of fuel extender.

FAA holder: Hunt Carter A.

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SA1511SOFuel systemsRevised Apr 21, 2003

Remove the 12 gallon fuselage fuel tank and install an 18 gallon fuel tank in the right wing.

FAA holder: Swallows of Atlanta Inc

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ST00181DEFuel systemsRevised Apr 16, 2003

Installation of a Fuel Jettison System for the de Havilland Model DHC-7-102 and -103. (DHC-7-103 3 and Subs).

FAA holder: Northrop Grumman Corporation California Microwave Systems

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ST00167BOFuel systemsRevised Apr 9, 2003

Installation of a refuel/defuel power switching system. Installation of this STC is dependent upon a previously FAA-approved installation of an electrical pressure feed-thru or electrical disconnect at approximately fuselage station 521 between STGR23R and STGR24R under right wing root fairing.

FAA holder: Learjet Inc.

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SR01817ATFuel systemsRevised Apr 1, 2003

Installation of forward and aft replacement fuel tanks.

FAA holder: Ryan Aerospace Inc

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SA02644ATFuel systemsRevised Mar 28, 2003

Installation of modified fuel system. Limited to installation on model HST-550, serial number 001 ONLY.

FAA holder: Mojoe LLC

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SA1484GLFuel systemsRevised Mar 19, 2003

Installation of 30 gallon fuel system.

FAA holder: Busch Ron

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SB01775CHFuel systemsRevised Feb 21, 2003

Replace Cameron Balloons basket/burner system and fuel tanks with Aerostar International basket model RB6 (P/N 52428), the Aerostar International Burner Model H.P.III Dual (P/N 52350), and the Aerostar International fuel tank model V-23 (P/N 52427). Approved for installation on serial number 6046 ONLY.

FAA holder: Cameron Balloons US

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SA00859ATFuel systemsRevised Feb 18, 2003

Installation of an additional fuel filler opening and cap, outboard of the standard filler cap to allow the carriage of 10 additional gallons per side.

FAA holder: 2 Days' Wings Inc.

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SA1492GLFuel systemsRevised Feb 18, 2003

Installation of 30 gallon fuel system. (415-CD S/N 813 AND UP).

FAA holder: Busch Ron

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SR01618NYFuel systemsRevised Jan 24, 2003

Installation of a Fuel Drain Collector System.

FAA holder: Airworthiness Resources Corporation

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SA5450SWFuel systemsRevised Jan 8, 2003

Installation of Foxboro fuel flow system.

FAA holder: BAE Systems Regional Aircraft Inc.

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SA1527NMFuel systemsRevised Dec 13, 2002

Installation of Foxboro fuel management indication system.

FAA holder: Northrop Grumman Corporation California Microwave Systems

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SB01734CHFuel systemsRevised Nov 8, 2002

Replace Cameron Balloons Basket/Burner system and fuel tanks. Approved for installation on serial number 715 ONLY.

FAA holder: Thunder & Colt America

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SA02579ATFuel systemsRevised Nov 1, 2002

Installation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware.

FAA holder: PMA Products, Inc.

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SA00786SEFuel systemsRevised Oct 10, 2002

Installation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30, Revision G, dated August 1, 2002, or later FAA approved revision.

FAA holder: Aviation Innovations LLC

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SB01707CHFuel systemsRevised Oct 1, 2002

Replace existing Cameron Balloons US Basket, Burner, and fuel tanks with Lindstrand Balloons Basket, p/n BU-006-A-001, S/N BA333. Approved for installation on N-90, serial number 6012 ONLY.

FAA holder: Rainbow Ryders, Inc.

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SB01703CHFuel systemsRevised Sep 30, 2002

Replace Cameron Balloons US Basket/Burner system and fuel tanks with Aerostar International Bank model RSW. Approved for instalation on model N-77, serial number 5468 ONLY.

FAA holder: Cameron Balloons US

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SA09655SCFuel systemsRevised Sep 20, 2002

Installation of RAM Induction Equalized Fuel Nozzle Set.

FAA holder: RAM Aircraft Limited Partnership

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SB01692CHFuel systemsRevised Aug 14, 2002

Replace the Cameron Balloons US basket/burner system and fuel tanks with the Aerostar International Basket model RWSW (p/n 53030), the Aerostar International burner model HP III Dual (p/n 52350), and the Aerostar International fuel tank model V-15 (p/n 51977). For installation on N-77, serial number 6063 ONLY.

FAA holder: Cameron Balloons US

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SA01205ATFuel systemsRevised Jul 31, 2002

Installation of left hand side and right hand side main tank fuel cell assemblies. (H-395 (USAF L-28A or U-10B) ALL S/N'S).

FAA holder: Floats & Fuel Cells

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SA01258ATFuel systemsRevised Jul 31, 2002

Installation of left hand and right hand box section fuel cell assemblies.

FAA holder: Floats & Fuel Cells

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SA01259ATFuel systemsRevised Jul 31, 2002

Installation of left hand and right hand box section fuel cell assemblies.

FAA holder: Floats & Fuel Cells

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SA09046SCFuel systemsRevised Jul 31, 2002

Installation of replacement wing fuel cell bladders, P/N DF308-1 & -2.

FAA holder: Floats & Fuel Cells

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SA09047SCFuel systemsRevised Jul 31, 2002

Installation of replacement wing fuel cell bladders.

FAA holder: Floats & Fuel Cells

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SA09048SCFuel systemsRevised Jul 31, 2002

Installation of replacement wing fuel cell bladders.

FAA holder: Floats & Fuel Cells

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SA2357CEFuel systemsRevised Jul 31, 2002

Installation of LH and RH main fuel tank bladder cells, P/N's DF054-320 and DF054-321, as replacements for original bladders.

FAA holder: Floats & Fuel Cells

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SA2577CEFuel systemsRevised Jul 31, 2002

Installation of main fuel cell bladders as replacements for original bladders. (T210 SERIES SPECIFIC SERIAL NUMBERS AFFECTED).

FAA holder: Floats & Fuel Cells

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SA2584CEFuel systemsRevised Jul 31, 2002

Installation of LH and RH main fuel cell bladders, P/N's DF054-324 and DF054-325, as replacements for original bladders.

FAA holder: Floats & Fuel Cells

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SA2652CEFuel systemsRevised Jul 31, 2002

Installation of main fuel cell bladders as replacements for original bladders.

FAA holder: Floats & Fuel Cells

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SA8596SWFuel systemsRevised Jul 31, 2002

Installation of left (right) hand forward inboard fuel tank bladder cells, P/N DF304-1 (2) as a replacement for original bladders, P/N 5630304-1 (-2).

FAA holder: Floats & Fuel Cells

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SA8597SWFuel systemsRevised Jul 31, 2002

Installation of P/N DF062-507, upper center fuel tank bladder cells as a replacement for original bladder P/N 5630062-507.

FAA holder: Floats & Fuel Cells

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SA8598SWFuel systemsRevised Jul 31, 2002

Installation of P/N GL204-501, lower center fuel tank bladder cells, as a replacement for original bladder P/N 5630204-501.

FAA holder: Floats & Fuel Cells

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SA8599SWFuel systemsRevised Jul 31, 2002

Installation of left (right) hand forward inboard fuel tank bladder cells, P/N DF060-507 (LH) and 508(RH) as a replacement for original bladders P/N 5630060-507 (508).

FAA holder: Floats & Fuel Cells

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SA00801ATFuel systemsRevised Jul 29, 2002

Installation of left hand and right hand fuel cell assemblies.

FAA holder: A/C Fuel Cells Worldwide

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SA3437NMFuel systemsRevised Jul 16, 2002

Modification to permit an increase in maximum allowable zero fuel weight of DC-8-62 airplanes, (1) which are certified to a 335,000 lbs. maximum takeoff gross weight or (2) which are certified to a 350,000 lbs. maximum takeoff gross weight.

FAA holder: Leth & Associates

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SA1072NWFuel systemsRevised Jul 2, 2002

Increase of zero fuel weight to131,000 pounds for aircraft complying complying with GD Convair strength and operating restrictions report ZS-22-300, Rev 3. This STC is limited to aircraft modified per STC Number SA1071NW.

FAA holder: Lost Birds Aviation Historical Society & Museum

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ST09999SCFuel systemsRevised Jun 24, 2002

Reduction in aircraft Maximum Zero Fuel Weight (MZFW).

FAA holder: Elite Aviation Inc.

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SA1480WEFuel systemsRevised Jun 14, 2002

Installation of an integral 24 gallon auxiliary fuel tank in each wing tip.

FAA holder: Met-Co Aire

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SA01652CHFuel systemsRevised Jun 10, 2002

Installation of Shadin fuel flow transducer. Installation with STC SE1688GL required.

FAA holder: Shadin Company Inc

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SA00148BOFuel systemsRevised May 29, 2002

Wing rib spacing modification per Scootair Modification to Clipped Wing Piper J3C-65 for Fuel Tank Installation Instructions of 11/10/01.

FAA holder: Scootair LLC

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SB01638CHFuel systemsRevised May 10, 2002

Replace Cameron Balloons US basket/burner system, fuel tanks, and instruments. Approved for installation on serial number 6312 ONLY.

FAA holder: Cameron Balloons US

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SB01632CHFuel systemsRevised Apr 26, 2002

Replace existing fuel tanks with Sky model V40 and/or Thunder & Colt model V40 fuel tanks. Approved for installing on serial number 6258 ONLY.

FAA holder: Cameron Balloons US

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SA29SWFuel systemsRevised Apr 23, 2002

Auxiliary outboard fuel tank.

FAA holder: AAR Oklahoma Inc

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SA01078SEFuel systemsRevised Apr 17, 2002

Installation of externally mounted fuel pump manufactured in accordance with Master Drawing List AEA105-90, Revision A, dated April 5, 2002, or later FAA approved revision, and installed in accordance with Installation Instructions VT-AEA105-12, Revision IR, dated April 5, 2002, or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness AEA-105-13, Revision IR, dated April 5, 2002, or later FAA approved revision.

FAA holder: Aero Air, LLC

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SR153CHFuel systemsRevised Mar 25, 2002

Installation of airborne division centrifugal fuel boost pump with canister.

FAA holder: Parker Hannifin Corp

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SA1620SWFuel systemsRevised Mar 22, 2002

Cessna 180 fuel cells.

FAA holder: Air Repair Inc

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SB01624CHFuel systemsRevised Feb 21, 2002

Replace Cameron Balloons Ltd bakset/burner/fuel tanks with a Cameron Balloons US basket/burner/fuel tanks. Approved for installation on serial number 5863 ONLY.

FAA holder: Cameron Balloons US

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SB01618CHFuel systemsRevised Jan 31, 2002

Replace Cameron Balloons US basket/burner system, fuel tanks, and instruments with Aerostar International Basket Model RWSW. Approved for installation on serial number 4202 ONLY.

FAA holder: Cameron Balloons US

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SR09044RCFuel systemsRevised Jan 17, 2002

Installation of an external water tank.

FAA holder: Dart Aerospace USA Inc.

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SB01568CHFuel systemsRevised Nov 13, 2001

Replace the Cameron Balloons Ltd. (Colt) Basket/Burner and fuel tanks with the Cameron Ballons US Basket part number CBUS301-5/MK IV Standard Double Burner part number CB392, and Cameron Balloons US fuel tanks, part number CB250. The Cameron Balloons US Basket/Double Burner is installed via the stand Cameron Carabiner (snaplin) attachments. (Colt 210A, S/N 2475USA).

FAA holder: Cameron Balloons US

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SA4632NMFuel systemsRevised Nov 7, 2001

Installation of extended range wing fuel tanks.

FAA holder: Del-Air

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SE09963SCFuel systemsRevised Nov 6, 2001

Installation of modified fuel injector nozzles.

FAA holder: General Aviation Modifications, Inc.

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SB01562CHFuel systemsRevised Oct 24, 2001

Replace Cameron Balloons basket/burner and fuel tanks with Cameron Balloons Basket part number CBUS301-5/MK IV super double burner part number CB579. Approved for serial number 2475USA ONLY.

FAA holder: Cameron Balloons US

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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.

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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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SB01546CHFuel systemsRevised Sep 28, 2001

Replace Cameron Balloons US basket/burner system and fuel tanks with Thunder model 40x48 basket/thunder C3 Magnum Double Burner, and Thunder fuel tanks, Model V30. Approved for serial number 6140 ONLY.

FAA holder: Cameron Balloons US

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SB01538CHFuel systemsRevised Sep 17, 2001

Replace Cameron Balloons US basket and fuel tanks with Sky Balloons basket size 2.87m X 1.57m type AO/BT14150/A and fuel tanks model V40. Approval limited to serial number 6258 ONLY.

FAA holder: Cameron Balloons US

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SB01530CHFuel systemsRevised Sep 4, 2001

Replace Cameron Balloons Ltd (Thunder) basket/burner and fuel tanks with Cameron Balloons part number CB860/ultra triple burner part number CB2081-2, and Cameron Balloons US fuel tanks, part number CBUS1050 and CBUS2060. Approved for serial number 4795 ONLY.

FAA holder: Cameron Balloons US

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SB01525CHFuel systemsRevised Aug 20, 2001

Replace Cameron Balloons basket/burner system and fuel tanks with Colt Model 40x60 basket/Colt III (C3) double burner, and Colt fuel tanks Model V30. Approved for serial number 6279 ONLY. Maximum gross weight is 2400 lbs.

FAA holder: Cameron Balloons US

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SA00348NYFuel systemsRevised Jul 17, 2001

Replacement of fuel filter element Aero-Flow Dynamics P/N 52-01103-1 (10 micron) with AAE P/N 740556.

FAA holder: PMA Design and Manufacturing, Inc.

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ST00117SEFuel systemsRevised Jun 6, 2001

For operation up to 197,700 lb maximum taxi weight, Increase in the maximum zero fuel weight to 155,000 lbs and increase in the maximum landing weight up to 164,000 lbs.

FAA holder: Altair Holdings Limited

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SA2537WEFuel systemsRevised Apr 25, 2001

Installation of modified fuel system.

FAA holder: Aviation Research Corporation

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SA1781SWFuel systemsRevised Jan 19, 2001

Revised ground and air starting procedures with bleed air heat to orifice in fuel control.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA1990SWFuel systemsRevised Jan 19, 2001

Installation of pressure relief overboard vent line and restrictor fitting to EPA fuel purge system.

FAA holder: Mitsubishi Heavy Industries America Inc.

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SA2238SWFuel systemsRevised Jan 19, 2001

Installation of tip tank taxi lights.

FAA holder: Mitsubishi Heavy Industries America Inc.

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ST00846SEFuel systemsRevised Oct 6, 2000

Installation of Model 840037-108, 840037-112, and 840037-113 Transient Suppression Devices on Boeing 747 Classic Airplanes fitted with Honeywell Analog Fuel Quantity Indication Systems.

FAA holder: Butler National Corporation

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ST01072LAFuel systemsRevised Sep 21, 2000

Installation of a red cover fuel shut-off handle assembly.

FAA holder: Federal Express Corp

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SA151SWFuel systemsRevised Aug 31, 2000