2.1 Aircraft Performance Limits & Design Requirements (§ 61.316)
Key Takeaways
- Since October 22, 2025, sport pilots operate aircraft meeting § 61.316—not the historical § 1.1 aircraft definition as the PIC eligibility test.
- There is no maximum takeoff weight and no absolute VH limit in § 61.316; VH training still splits at 87 KCAS under § 61.327.
- For airplanes, VS1 may not exceed 59 knots CAS at max certificated takeoff weight and most critical CG; other categories generally remain at 45 knots CAS VS1.
- Airplanes may have up to four seats, but § 61.315 still limits the sport pilot to one passenger.
- Retractable landing gear and manual controllable-pitch propellers need § 61.331 endorsements; cabins must be non-pressurized.
Aircraft Performance Limits & Design Requirements (§ 61.316)
Quick Summary: The MOSAIC rule moved sport-pilot aircraft limits out of the old § 1.1 aircraft meeting § 61.316 definition and into § 61.316. Effective for pilot certification/privileges on October 22, 2025, you may act as PIC only of an aircraft that has met these performance and design requirements since its original certification. Memorize the current numbers—especially airplane VS1 ≤ 59 KCAS and up to four seats—and do not answer with obsolete 1,320 lb / VH 120 (or mistaken 138) KCAS limits as if they were still the operational rule.
Why § 1.1 aircraft Numbers Are Exam Traps
Pre-MOSAIC materials drilled:
- MTOW 1,320 lb land / 1,430 lb sea
- VH ≤ 120 KCAS (not 138)
- VS1 ≤ 45 KCAS
- Two occupants, single reciprocating engine, fixed gear, fixed/ground-adjustable prop
Those figures described the old § 1.1 aircraft definition. Under current Subpart J, § 61.315(a) points you to § 61.316. Use historical aircraft numbers only if a question explicitly asks about the former definition.
Current § 61.316 Limits (Sport Pilot PIC Eligibility)
An aircraft must, since original certification, meet all applicable items below:
Stall Speed (VS1)
- General rule: maximum stalling speed / minimum steady flight speed without lift-enhancing devices (VS1) not more than 45 knots CAS.
- Airplane exception: VS1 not more than 59 knots CAS at maximum certificated takeoff weight and most critical center of gravity.
Seating Capacity
- General: maximum seating capacity of two persons.
- Airplane exception: maximum seating capacity of four persons.
- Passenger privilege reminder: § 61.315 still allows only one passenger, even in a four-seat airplane.
Cabin
Non-pressurized cabin if equipped with a cabin.
Powerplant / Controllability Design
For powered aircraft other than balloons or airships:
- Loss of partial power must not adversely affect directional control; and
- The design must allow a controlled descent after partial or total powerplant failure.
Helicopters operated by sport pilots must be certificated with the simplified flight controls designation.
Landing Gear
- Gliders: fixed or retractable.
- Other powered aircraft: fixed landing gear, unless you meet § 61.331 for retractable gear.
Propellers (powered aircraft other than gliders)
Fixed, ground-adjustable, or automated controllable-pitch propellers are contemplated in § 61.316(a)(9). A manual controllable-pitch propeller on an airplane requires the § 61.331(b) endorsement pathway via § 61.316(b).
What Was Removed
- No maximum takeoff weight in § 61.316.
- No absolute VH ceiling in § 61.316 (endorsements at 87 KCAS remain under § 61.327).
- Multi-engine and non-reciprocating powerplants are no longer barred the way the old single-reciprocating aircraft rule barred them—subject to the controllability and other § 61.316 design rules (turbo-jet powered aircraft remain outside the sport-pilot concept as implemented in MOSAIC guidance).
Comparison Table (Historical aircraft vs Current § 61.316)
| Topic | Historical § 1.1 aircraft (legacy) | Current § 61.316 (PIC rule) |
|---|---|---|
| Weight | 1,320 / 1,430 lb MTOW | No MTOW limit |
| VH | ≤ 120 KCAS | No VH ceiling (87 KCAS endorsement split remains) |
| VS1 (airplane) | ≤ 45 KCAS | ≤ 59 KCAS |
| Seats (airplane) | 2 | Up to 4 (still 1 passenger) |
| Gear | Fixed (with seaplane/glider nuances) | Fixed, or retractable with § 61.331 |
| Prop | Fixed / ground-adjustable | Fixed / ground-adjustable / automated CPP; manual CPP with § 61.331 |
Gyroplane / Category Nuances
Gyroplanes retain a fixed-pitch, semi-rigid, teetering, two-blade rotor system requirement in § 61.316(a)(4). Always apply the category-specific paragraphs, not airplane exceptions, when the question names a non-airplane category.
How Examiners and Knowledge Tests Probe § 61.316
Expect scenario stems such as:
- “May a sport pilot fly Airplane X with VS1 of 55 KCAS and four seats?” → Check airplane VS1 ≤ 59 and seats ≤ 4, then apply the one-passenger rule.
- “Is a 1,400 lb airplane automatically illegal?” → Weight alone is no longer disqualifying under § 61.316.
- “The airplane has a manual controllable-pitch propeller—legal?” → Only with § 61.331 training/endorsement (and otherwise meeting § 61.316).
Interaction with Higher Certificates
A Private Pilot exercising sport-pilot privileges must still obey sport-pilot limits while doing so. Holding a higher certificate does not erase § 61.315 altitude, visibility, passenger, or endorsement constraints for that operation. Conversely, a sport pilot who later upgrades to Private Pilot gains night/passenger/airspace privileges under Private rules—not by stretching sport-pilot limits.
Design Philosophy Behind MOSAIC
The FAA shifted from a rigid weight-and-speed box to performance-based stall-speed and design constraints so newer trainers and personal airplanes could enter the sport-pilot ecosystem without pretending every eligible airplane is a 1,320 lb LSA. Your job on the knowledge test is to apply the current regulation text, not the 2004 study-guide flashcards.
Under current 14 CFR § 61.316, what is the maximum VS1 for an airplane a sport pilot may operate?
Which statement about sport-pilot aircraft weight and speed limits is correct after MOSAIC?
An airplane meeting § 61.316 has four seats. How many passengers may a sport pilot carry?