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 Code of Federal Regulations (Last Updated: April 5, 2024)
 Title 46 - Shipping
 Chapter I - Coast Guard, Department of Homeland Security
 SubChapter F - Marine Engineering
 Part 58 - Main and Auxiliary Machinery and Related Systems
 Subpart 58.50 - Independent Fuel Tanks

  § 58.50-5 - Gasoline fuel tanks.  

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  • § 58.50-5 Gasoline fuel tanks.

    (a) Construction - —

    (1) Shape. Tanks may be of either cylindrical or rectangular form, except that tanks for emergency electrical systems shall be of cylindrical form.

    (2) Materials and construction. The material used and the minimum thickness allowed shall be as indicated in Table 1 to § 58.50-5–5(a) except that consideration will be given to other materials which provide equivalent safety as indicated in § 58.50-15–15.

    (3) Prohibited types. Tanks with flanged-up top edges that may trap and hold moisture shall not be used.

    (4) Openings. Openings for fill, vent and fuel pipes, and openings for fuel level gages where used, shall be on the topmost surface of tanks. Tanks shall have no openings in bottoms, sides, or ends, except that an opening fitted with threaded plug or cap may be used for tank cleaning purposes.

    Table 1 to § 58.50-5–5(a)

    Material ASTM specification
    (all incorporated by reference; see 46 CFR 58.03-1–1)     		Thickness in inches and gage numbers1 vs. tank capacities for - for—
    1- through 80-gallon tanks More than 80- and not more than 150-gallon tanks Over 150-gallon tanks2
    Aluminum5 B 209, Alloy 50866 0.250 (USSG 3)0.250 (USSG 3)0.250 (USSG 3).
    Nickel-copperB 127, Hot rolled sheet or plate0.037 (USSG 20).3 0.050 (USSG 18)0.107 (USSG 12).
    Copper-nickelB 122, Alloy No. 50.045 (AWG 17)0.057 (AWG 15)0.128 (AWG 8).
    CopperB 152, Type ETP0.057 (AWG 15)0.080 (AWG 12)0.182 (AWG 5).
    Copper-siliconB 96, alloys C65100 and C655000.050 (AWG 16)0.064 (AWG 14)0.144 (AWG 7).
    Steel or iron4 0.0747 (MfgStd 14)0.1046 (MfgStd 12)0.179 (MfgStd 7).

    Notes:

    1 Gauges used are U.S. standard “USSG” for aluminum and nickel-copper; “AWG” for copper, copper-nickel and copper-silicon; and “MfgStd” for steel.

    2 Tanks over 400 gallons shall will be designed with a factor of safety of four on the ultimate strength of the material used with a design head of not less than 4 feet of liquid above the top of the tank.

    3 Nickel-copper not less than 0.031 inch (USSG 22) may be used for tanks up to a 30-gallon capacity.

    4 Fuel tanks constructed of iron or steel, which is less than 3⁄16-inch thick shall must be galvanized inside and outside by the hot dip process.

    5 Anodic to most common metals. Avoid dissimilar metal contact with tank body.

    6 And other alloys acceptable to the Commandant.

    (5) Joints. All metallic tank joints shall be welded or brazed.

    (6) Fittings. Nozzles, flanges, or other fittings for pipe connections shall be welded or brazed to the tank. The tank openings in way of pipe connections shall be properly reinforced where necessary. Where fuel level gages are used, the flange to which gage fittings are attached shall be welded or brazed to the tank. No tubular gage glasses or trycocks shall be fitted to the tanks.

    (7) Baffle plates. All tanks exceeding 30 inches in any horizontal dimension shall be fitted with vertical baffle plates where necessary for strength or for control of excessive surge. In general, baffle plates installed at intervals not exceeding 30 inches will be considered as meeting this requirement.

    (8) Baffle plate details. Baffle plates, where required, shall be of the same material and not less than the minimum thickness required in the tank walls and shall be connected to the tank walls by welding or brazing. Limber holes at the bottom and air holes at the top of all baffles shall be provided.

    (b) Installation.

    (1) Gasoline fuel tanks used for propulsion shall be located in water-tight compartments separate from, but adjacent to the engineroom or machinery space. Fuel tanks for auxiliaries shall be located on or above the weather deck outside of the engine housing or compartment and as close to the engine as practicable. All tanks shall be so installed as to provide a free circulation of air around the tanks.

    (2) Cylindrical tanks with longitudinal seams shall be arranged horizontally where practicable so that such seams are located as near the top as possible.

    (3) Fuel tanks shall be so installed as to permit examination, testing, or removal for cleaning.

    (4) Fuel tanks shall be adequately supported and braced to prevent movement. Portable fuel tanks are not permitted.

    (5) All fuel tanks shall be electrically bonded to the common ground.

    (c) Testing.

    (1) Prior to installation, tanks vented to atmosphere shall be tested to, and must withstand, a pressure of 5 pounds per square inch or 11⁄2 times the maximum head to which they may be subjected in service, whichever is greater. A standpipe of 111⁄2 feet in height attached to the tank may be filled with water to accomplish the 5 pounds per square inch test. Permanent deformation of the tank will not be cause for rejection unless accompanied by leakage.

    (2) After installation of the fuel tank on a vessel the complete installation shall be tested in the presence of a marine inspector to a head not less than that to which the tank may be subjected in service. Fuel may be used as a testing medium.

    (3) All tanks not vented to atmosphere shall be constructed and tested in accordance with part 54 of this subchapter.

    [CGFR 68-8268–82, 33 FR 18878, Dec. 18, 1968, as amended by CGFR 72-59R72–59R, 37 FR 6190, Mar. 25, 1972; USCG-1999-5151USCG–1999–5151, 64 FR 67180, Dec. 1, 1999; USCG-2003-16630USCG–2003–16630, 73 FR 65187, Oct. 31, 2008; USCG–2016–0498, 82 FR 35089, July 28, 2017]