MOSAIC Brief

Aircraft & Certification · Explainer

What counts as an ultralight vehicle under FAA Part 103

Section 103.1 defines an ultralight vehicle: one occupant, recreation or sport only, no airworthiness certificate, plus weight limits and, if powered, fuel, speed and stall limits. Here is what that means, including fuel capacity versus fuel carried.

By MOSAIC BriefPublished Last human review Sources checked
On this page

Suppose you are looking at a single-seat flying machine and wondering whether it counts as an “ultralight.” The label matters, because the FAA treats an ultralight vehicle very differently from an aircraft. The test is in 14 CFR 103.1, and a vehicle must meet every element that applies to it. That section is only the definition: Part 103 also has operating rules for flying an ultralight vehicle, which this article does not cover.

Why ultralights sit outside aircraft certification

The FAA's advisory circular on the subject, AC 103-7, explains the trade-off. It says an ultralight vehicle is not subject to federal aircraft certification and maintenance standards, and that the regulations on aircraft certification, pilot certification and aircraft registration are not applicable to ultralight vehicles or their operators. The flip side is that there is no assurance a particular ultralight will have consistent performance, controllability, structural integrity or maintenance, and the operator is responsible for assessing the risks. The circular is guidance, not a regulation, and is dated January 30, 1984, so read it as the FAA's explanation, not the rule's current text.

The definition, piece by piece

Section 103.1 describes an ultralight vehicle as one that is used or intended for manned operation by a single occupant, used or intended for recreation or sport only, and without any U.S. or foreign airworthiness certificate. It then splits by power. An unpowered vehicle must weigh less than 155 pounds. A powered vehicle must meet all four of these:

  • an empty weight under 254 pounds, excluding floats and safety devices intended for deployment in a potentially catastrophic situation;
  • a fuel capacity not exceeding 5 U.S. gallons;
  • no capability of more than 55 knots calibrated airspeed at full power in level flight; and
  • a power-off stall speed not exceeding 24 knots calibrated airspeed.

The circular adds that missing any one element means you may not operate under Part 103, and that calling a machine a “powered ultralight” is no assurance it qualifies. It puts responsibility for meeting the definition on the operator, on each flight, and says a vehicle that does not meet it must be operated under the applicable aircraft regulations.

Where light-sport aircraft fit

An aircraft with any U.S. or foreign airworthiness certificate fails the “no certificate” element, so a certificated light-sport aircraft is not an ultralight vehicle. For new light-sport category certification under the current § 21.190, eligibility includes the applicable § 22.100 requirements. Aircraft certificated in the light-sport category before July 24, 2026 have separate legacy conditions under § 21.181(a)(3); this article does not recertify them. Sport pilot aircraft limits in § 61.316 are written in different terms (for example VS1 rather than power-off stall speed), so do not compare those numbers directly with the § 103.1 figures.

A hypothetical: tank size versus fuel on board

Imagine a builder who plans a tank larger than the limit and reasons that they will only ever fill it partway. This illustrates why the wording matters: § 103.1(e)(2) speaks of fuel capacity and does not mention the amount carried. AC 103-7 reads it the same way, calling a powered ultralight with tanks above the limit ineligible. It counts the total volume of the tanks, usable and unusable fuel included, but not fuel in the lines, pump, strainer or carburetor. A permanent standpipe or venting arrangement that controls capacity is permitted, though you may be asked to demonstrate it, while a temporary, detachable or voluntarily observed method such as a “fill-to” line is not acceptable. An inspector may ask you to show compliance by measuring the tank's capacity.

Still to verify: the circular dates from 1984, and the example cannot tell you whether a particular tank design would be accepted. Advice, not a requirement: confirm with the FAA before building a larger tank.

What MOSAIC did with Part 103

The MOSAIC final rule lists the parts it amends as 1, 21, 22, 36, 43, 45, 61, 65, 91, 119 and 147. Part 103 is not among them. Two examples of ultralight-related provisions in its text: an existing cross-reference to § 103.1 in § 21.191(i)(1), a provision for aircraft that do not meet § 103.1 under which experimental certificates stopped being issued after January 31, 2008; and the retained exception in § 91.327(a)(1) that lets a light-sport category aircraft tow a glider or an unpowered ultralight vehicle for compensation or hire in accordance with § 91.309. These are examples, not a full list. This article does not say MOSAIC changed, or did not change, any other ultralight-related rule.

The takeaway

Check your vehicle against each element, measure tank capacity rather than fuel carried, and remember that the circular puts the responsibility for qualifying on the operator. When in doubt, ask the FAA before you build or fly. This article cannot say whether any real vehicle qualifies.

Sources and claims checked

Where each claim was checked (24 references)

Each claim below was checked against the source shown. A source’s displayed update date does not show which paragraph changed.

ClaimSourceWhereChecked
Part 103 prescribes rules governing the operation of ultralight vehicles in the United States, and § 103.1 defines an ultralight vehicle by a list of criteria; § 103.1 is that definition, not the operating rules themselves.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1 lead-in
To be an ultralight vehicle, a vehicle must be used or intended to be used for manned operation in the air by a single occupant.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(a)
It must be used or intended to be used for recreation or sport purposes only.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(b)
It must not have any U.S. or foreign airworthiness certificate.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(c)
If unpowered, it must weigh less than 155 pounds.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(d)
If powered, paragraph (e) applies instead: weight is less than 254 pounds empty weight, excluding floats and safety devices intended for deployment in a potentially catastrophic situation.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(e)(1)
If powered, the vehicle must have a fuel capacity not exceeding 5 U.S. gallons; the text speaks of capacity and does not mention the amount of fuel carried.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(e)(2)
If powered, the vehicle must not be capable of more than 55 knots calibrated airspeed at full power in level flight.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(e)(3)
If powered, the vehicle must have a power-off stall speed that does not exceed 24 knots calibrated airspeed.14 CFR 103.1 - Applicability (ultralight vehicles)14 CFR 103.1(e)(4)
AC 103-7, The Ultralight Vehicle, is an FAA advisory circular dated January 30, 1984 (shown as 1/30/84) that provides guidance to operators of ultralights and discusses the elements of the definition for operating under Part 103.AC 103-7 The Ultralight VehicleAC 103-7 p.1
The circular says the Federal Aviation Regulations on aircraft certification, pilot certification and aircraft registration are not applicable to ultralight vehicles or their operators.AC 103-7 The Ultralight VehicleAC 103-7 para 2.b
The circular says an ultralight vehicle is not subject to federal aircraft certification and maintenance standards, that there is no assurance a particular ultralight will have consistent performance, controllability, structural integrity or maintenance, and that the operator is responsible for assessing the risks and assuring personal safety.AC 103-7 The Ultralight VehicleAC 103-7 paras 2.c, 4.a
The circular says that failing to meet any one element of § 103.1 means a vehicle may not be operated under Part 103, that calling a vehicle a powered ultralight is not an assurance it can be operated as one, and that operations without meeting all elements are subject to the aircraft certification, pilot certification, equipment and operating rules applicable to the operation.AC 103-7 The Ultralight VehicleAC 103-7 para 11.a
The circular says operators are responsible for meeting § 103.1 during each flight, and that a vehicle that does not meet § 103.1 must be operated in accordance with applicable aircraft regulations.AC 103-7 The Ultralight VehicleAC 103-7 para 11.b, 11.c
The circular says the maximum fuel capacity for a powered ultralight vehicle is 5 U.S. gallons and that any powered ultralight with fuel tanks exceeding that capacity is ineligible for operation as an ultralight vehicle.AC 103-7 The Ultralight VehicleAC 103-7 para 19
The circular says fuel capacity is the total volume, including all available space for usable and unusable fuel in the tank or tanks, and that fuel in the lines, pump, strainer and carburetor is not counted.AC 103-7 The Ultralight VehicleAC 103-7 para 19.a
The circular says tanks with a permanent standpipe or venting arrangement to control capacity are permitted but may be subject to demonstration of the capacity if there is reason to doubt the arrangement is effective, while a temporary, detachable or voluntarily observed method of restricting fuel capacity, such as a “fill-to” line, is not acceptable.AC 103-7 The Ultralight VehicleAC 103-7 para 19.b
The circular says an FAA inspector may ask the operator to show compliance with § 103.1 by measuring the capacity of the fuel tank, among other checks.AC 103-7 The Ultralight VehicleAC 103-7 para 23
For new light-sport category certification, § 21.190 provides that the FAA issues the special airworthiness certificate, and eligibility includes meeting the applicable requirements of § 22.100.14 CFR 21.190 - Issue of a special airworthiness certificate for a light-sport category aircraft14 CFR 21.190(a), (b)
Light-sport category aircraft originally certificated before July 24, 2026 are covered by separate legacy conditions in § 21.181(a)(3)(iv): their light-sport airworthiness certificate stays effective while the listed conditions continue to be met.14 CFR 21.181 - Duration14 CFR 21.181(a)(3), (a)(3)(iv)
Section 61.316 sets performance limits and design requirements for aircraft a sport pilot may operate, in different terms from § 103.1 (for example a maximum VS1 of 45 knots CAS, or 59 for airplanes, and seating for two, or four for airplanes).14 CFR 61.316 - Performance limits and design requirements for the aircraft that a sport pilot may operate14 CFR 61.316(a)(1), (a)(2)
The MOSAIC final rule lists the parts it amends as 14 CFR Parts 1, 21, 22, 36, 43, 45, 61, 65, 91, 119 and 147. Part 103 is not among them.Modernization of Special Airworthiness CertificationFederal Register 2025-13972, “List of Subjects”
The final rule's regulatory text contains an existing cross-reference to § 103.1 within § 21.191(i)(1), a provision for aircraft that do not meet § 103.1 for which experimental certificates stopped being issued after January 31, 2008.Modernization of Special Airworthiness CertificationFederal Register 2025-13972, amended § 21.191(i)(1)
The final rule keeps the existing exception that lets a light-sport category aircraft tow a glider or an unpowered ultralight vehicle for compensation or hire in accordance with § 91.309.Modernization of Special Airworthiness CertificationFederal Register 2025-13972, discussion of § 91.327(a)(1)
Source documents (6)

More in Aircraft & Certification