Light-sport aircraft
A light-sport aircraft, or light sport aircraft, is a fairly new category of small, lightweight aircraft that are simple to fly. LSAs tend to be heavier and more sophisticated than ultralight aircraft, but LSA restrictions on weight and performance separates the category from established GA aircraft. There is no standard worldwide description of an LSA.
LSAs in different countries
in different countries have their own particular specifications and regulations which define the LSA category.For example, in Australia the Civil Aviation Safety Authority defines a light-sport aircraft as a heavier-than-air or lighter-than-air craft, other than a helicopter, with a maximum gross takeoff weight of not more than for lighter-than-air craft; for heavier-than-air craft not intended for operation on water; or for aircraft intended for operation on water. It must have a maximum stall speed of in landing configuration; a maximum of two seats; there is no limit on maximum speed unless it is a glider, which is limited to Vne 135 kn CAS; fixed undercarriage ; an unpressurized cabin; and a single non-turbine engine driving a propeller if it is a powered aircraft.
In the United States, several distinct groups of aircraft may be flown as light-sport. Existing certificated aircraft and experimental, amateur-built aircraft that fall within the definition listed in 14CFR1.1 are acceptable, as are aircraft built to an industry consensus standard rather than FAA airworthiness requirements. The accepted consensus standard is defined by ASTM International Technical Committee F37. Aircraft built to the consensus standard may be factory-built and sold with a special airworthiness certification or may be assembled from a kit under the experimental rules under experimental airworthiness. A company must have produced and certified at least one S-LSA in order to be permitted to sell E-LSA kits of the same model. E-LSA kits are not subject to the normal experimental amateur built requirement 14 CFR 21.191 which identifies an aircraft, the "major portion of which has been fabricated and assembled by persons who undertook the construction project solely for their own education or recreation."
United States
The FAA defines a light sport aircraft as an aircraft, other than a helicopter or Powered-lift, that since its original certification, has continued to meet the following:- Max. Gross Takeoff Weight: 1,320 lbs or 1,430 lbs for seaplanes
- Max. Stall Speed: CAS
- Max. Speed in Level Flight : CAS
- Max. Seats: Two
- Max. Engines / Motors: One
- Propeller: Fixed-pitch or ground adjustable
- Cabin: Unpressurized
- Fixed-pitch, semi-rigid, teetering, two-blade rotor system, if a gyroplane.
- Landing Gear: Fixed
- Can be manufactured and sold ready-to-fly under a new Special Light Sport Aircraft certification category. Aircraft must meet industry consensus standards. Aircraft under this certification may be used for sport and recreation, flight training, and aircraft rental.
- Can be licensed Experimental Light Sport Aircraft if kit- or plans-built. Aircraft under this certification may be used only for sport and recreation and flight instruction for the owner of the aircraft.
- Can be licensed Experimental Light Sport Aircraft if the aircraft has previously been operated as an ultralight but does not meet the FAR Part 103 definition of an ultralight vehicle. These aircraft must have been transitioned to E-LSA category no later than January 31, 2008.
- Will have a standard FAA registration - N-number.
- Category and class includes: Airplane, Gyroplane, Airship, Balloon, Weight-Shift-Control, Glider, and Powered Parachute.
- U.S. or foreign manufacture of light sport aircraft is authorized.
- Aircraft with a standard airworthiness certificate that meet above specifications may be flown by sport pilots. However, the aircraft must remain in standard category and cannot be changed to light sport aircraft category.
- May be operated at night if the aircraft is equipped per FAR 91.205, if such operations are allowed by the aircraft's operating limitations and the pilot holds at least a Private Pilot certificate and a minimum of a third-class medical.
FAA certification
The US definition of an LSA is similar to some other countries' definition of "microlight" or "ultralight" aircraft. Except for the LSA's relatively generous MTOW of 1320 pounds, the other countries' microlight definitions are typically less restrictive, not limiting airspeed or the use of variable-pitch propellers.
By contrast, the US FAA has a separate definition of ultralight aircraft defined in Federal Aviation Regulations. Aircraft falling within the US ultralight specifications are extremely lightweight, are intended for manned operation by a single occupant, have a fuel capacity of five US gallons or less, a maximum calibrated airspeed of not more than, and a maximum stall speed of not more than. Ultralight aircraft in the US do not require pilot licensing, medical certification, or aircraft registration.
Aircraft certified as light-sport aircraft exceed the limitations defined for ultralight aircraft and require that the pilot possess, at a minimum, a sport pilot certificate. Among these aircraft were found those that were specifically designed to meet the LSA requirements, as well as overweight ultralights that previously were operated in technical violation of 14 CFR 103.
In addition to aircraft specifically designed to meet the LSA requirements, certain certificated aircraft, such as the original Piper Cub, happen to fall within the definition of a light-sport aircraft and can be operated by individuals holding FAA sport pilot certificates. The aircraft can not be re-certificated as LSA, however: although sport pilots may operate conventionally certificated aircraft that fall within the definition of an LSA, the aircraft themselves continue to be certificated in their original categories.
Several designers and manufacturers of experimental aircraft kits have developed models that are compliant with the light-sport aircraft rules.
In June 2012 the FAA indicated that they would re-visit the LSA program after their own studies indicated that "the majority" of LSA manufacturers they had inspected failed to show that they were in compliance with the standards. The FAA announcement said that as a result the "original policy of reliance on manufacturers' Statements of Compliance"... "should be reconsidered." AOPA points out that this is a normal development of a maturing standard and does not expect any significant changes in the rules, only more scrutiny by FAA to assure compliance.
FAA certified models
Aircraft that met light-sport requirements when the rules were announced appear in FAA's listSome additional models of S-LSA, E-LSA and E-AB aircraft that meet light-sport requirements are listed here.
Manufacturer | Design | Engine | Max. cruise | Max. range | Orders | Availability | Type | - |
3Xtrim | 3Xtrim Navigator 600 | 100 HP Rotax 912 S | 104 kn | 747 NM | 2008 | Certified | - | |
Advanced Composites Solutions | ACS-100 Sora | 120 kn | Kit | - | ||||
Aeropro / fly-Aerotrek.com | Aerotrek A240 or A220 | Rotax 912 A/ 912 S | 115 kn | 570 NM | 300+ sold | since 1990 | Certified | - |
Aeroprakt Manufacturing | A-22LS | Rotax 912UL,Rotax 912ULS or Rotax 912 iS | 110 kn | 594 NM | since 2016 | Certified | - | |
AMD | Zodiac 650B | Continental O-200 + Others | 120 kn | Certified | - | |||
The Airplane Factory | The Airplane Factory Sling 2 | Rotax 912S or 912 ULS | 110 kn | 880 NM | 100+ | 2010 | Certified RTF & Kit | - |
Aviasud Engineering | Aviasud Mistral | Rotax 582 DCDI | 65 kn | 270 NM, 500 km | Certified | - | ||
BOT Aircraft | SC07 Speed Cruiser | Rotax 912ULS or D-Motor LF26 | 116kn | 648NM | 2016 | E-LSA, pending S-LSA certification | - | |
Breezer | Breezer | Rotax 912 UL2 | 96 kn | 497 NM | - | |||
CGS Aviation | Hawk Arrow II SLSA | Rotax 582, Rotax 912 F, HKS 700e, HKS 700T, Jabiru 2200 | 70 kn | 130 NM | 170+ | 2008 | Certified | - |
Cessna | Cessna 162 | Continental O-200D | 112 kn | 470 NM | 195. 80 in stock for spares | Since 2009 - discontinued Feb 2014 | Certified | - |
Cirrus Design | Cirrus SRS | Rotax 912 S | 120 kn | Unknown, project suspended | Certified | - | ||
Comco Ikarus | Ikarus C42 | Rotax 912 F | 105 kn 194 km/h | Certified | - | |||
Cub Crafters | CubCrafters CC11-160 Carbon Cub SS | Titan 340CC, 180 HP | 88 kn | 391 NM | 300+ | 2009 | ELSA Kit/Certified | - |
Czech Sport Aircraft | SportCruiser/PiperSport | Rotax 912 S | 118 kn | 600 NM | 170+ delivered | Available since 2006 | Certified | - |
Czech Sport Aircraft/Wet Aero USA | CZAW Mermaid | Jabiru 3300 or Rotax 912S | 110 kn | 450 NM | 2006 | Certified | - | |
DOVA Aircraft | DV-1 SKYLARK | Rotax 912S | 124,19kn | 539 NM | 2004 | Certified | - | |
Ekolot | Ekolot KR-030 Topaz | Rotax 912UL | 119 kn | 2010 | LSA Certified | - | ||
Europa Aircraft | Europa XS | Rotax 912 / 912 ULS / 914 or Jabiru Aircraft | 120 kn | 750 NM | 2009 | Kit | - | |
FANTASY AIR | Allegro 2007 | Rotax 912 F or 912 S | 119 kn | 750 NM | 2008 | Certified | - | |
FK-Lightplanes | FK12 Comet | Rotax 912UL/ULS, 914, or Lycoming IO-233 | 97 kn | 351 nm | 1997 | Certified | - | |
Flight Design | Flight Design CTsw: CTLS: CTLSi | Rotax 912S ; Rotax 912iS | 120 kn | 850 NM | 350+ | 2005 | Certified | - |
Higher Class Aviation | Sport Hornet LRS | Rotax 912 F or Rotax 582 | 100 kn | 450 NM | 040+ | 2009 | Certified | - |
JIHLAVAN airplanes, s.r.o. | Skyleader 600 | Rotax 912 100 hp & 115 hp | 120 kn | 860 NM | Available | Certified | - | |
ICON Aircraft | ICON A5 | Rotax 912 iS | 105 kn | 300 nmi | 1500+ | 2015 | FAA Approved | - |
Kitfox Aircraft | Kitfox | Rotax 912 S | 109 kn | 530 NM | 4000+ | 2008 | ELSA Kit/Certified | - |
Paradise Aircraft | Paradise P-1 | 100 HP, Rotax 912 S | 120 kn | 747 NM | 2008 | Certified | - | |
Pipistrel | Pipistrel Sinus LSA | Rotax 912 80 hp | 120 kn | 790 NM | 1000+ | since 1995 | Certified LSA Airplane & Glider RTF & Kit | - |
Pipistrel | Pipistrel Virus LSA | Rotax 912 80 hp | 120 kn | 790 NM | 1000+ | since 1999 | Certified LSA Airplane & Glider RTF & Kit | - |
Pipistrel | Pipistrel Virus SW LSA | Rotax 912 80 hp & 100 hp | 120 kn | 790 NM | 1000+ | since 2008 | Certified LSA Airplane & Glider RTF & Kit | - |
Pipistrel | Pipistrel Taurus LSA | Rotax 503, 55 hp | 120 kn | 150 NM | since 2004 | Certified LSA Glider RTF | - | |
Pipistrel | Pipistrel Alpha Trainer | Rotax 912 80 hp | 120 kn | 790 NM | since 2012 | Certified LSA Airplane RTF | - | |
Progressive Aerodyne | SeaRey Elite LSA | Rotax 914 | 91 kn | 379 NM | LSA Kit/Certified | - | ||
Progressive Aerodyne | SeaRey Sport LSA | Rotax 912UL | 80 kn | 363 NM | LSA Certified | - | ||
Rainbow Aircraft ltd. | Cheetah XLS | Rotax 912 or Rotax 582 or Jabiru 2200A | 83 kn | 450 NM | 100+ | 2001 | ELSA Kit/Certified | - |
Remos Aircraft | Remos G-3 | Rotax 912 S, 100HP | 120 kn | 550 NM / 1018 km | 2007 | Certified | - | |
Remos Aircraft | Remos GX | Rotax 912 S 100HP | 115 kn | 450 NM | Certified | - | ||
Renegade Light Sport originally T&T Aviation | Falcon LS | Lycoming IO-233-LSA | 112 kn | 460 nmi | 2010 | LSA Certified | - | |
Skyeton | Skyeton K-10 Swift | Rotax 912 S, 100HP | 120 kn | 486 NM | 2006 | Certified | - | |
SkyRunner, LLC. | SkyRunner MK 3.2 | 914 UL | 35 kn | 120 nm | US$139,000 | 2016 | FAA Approved / S-LSA | |
TL Ultralight | TL Ultralight TL-96 Star | Rotax 912 F | 120 kn | 790 NM | 70+ | Available | Certified | - |
Storm Aircraft | Storm Rally | Rotax 912 S | 120 kn | 450 NM | 2004 | Certified | - | |
Storm Aircraft | Storm Century | Rotax 912 S | 120 kn | 450 NM | 2004 | Certified | - | |
Tecnam Aircraft | Tecnam P2004 | Rotax 912 S | 116 kn | 100+ | 2005 | Certified | - | |
Terrafugia | Terrafugia Transition | Rotax 912 S | 100 | 2012 | Experimental/Certification planned | - | ||
Van's Aircraft | RV-12 | Rotax 912 iS | 117 kn | 564 NM | 1000+ | 2008 | ELSA Kit/Certified | - |
Europe
In June 2011, the European Aviation Safety Agency published CS-LSA "Certification Specifications for Light Sport Aeroplanes". This introduced a new category of manufactured sport aeroplanes similar to the light-sport category found in the USA and elsewhere.Australia
A new certification category for 'Light Sport Aircraft' came into effect on 7 January 2006. This category does not replace the previous categories, but created a new category with the following characteristics:- A maximum take-off weight of or for an aircraft intended and configured for operation on water or for a lighter-than-air aircraft.
- A maximum stalling speed in the landing configuration of CAS.
- Maximum of two occupants, including the pilot.
- A fixed landing gear. A glider may have retractable landing gear.
- A single, non-turbine engine fitted with a propeller.
- A non-pressurised cabin.
- If the aircraft is a glider a maximum never exceed speed of CAS