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STOL

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An aircraft that, at some weight within its approved operating weight, is capable of operating from a STOL runway in compliance with the applicable STOL characteristics and airworthiness, operations, noise, and pollution standards" and ""aircraft" means any machine capable of deriving support in the
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A STOL aircraft is an aircraft with a certified performance capability to execute approaches along a glideslope of 6 degrees or steeper and to execute missed approaches at a climb gradient sufficient to clear a 15:1 missed approach surface at sea level... A STOL runway is one which is specifically
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sells Robertson STOL kits, marketed under the name R/STOL, incorporate a drooped leading edge cuff, wing fences, drooping ailerons and an automatic trim system. The company says that installation "allows 15 to 25 MPH slower approaches and requires up to 40% less runway distance". R/STOL kits are
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short takeoff and landing aircraft (STOL), heavier-than-air craft, capable of rising from and descending to the ground with only a short length of runway, but incapable of doing so vertically. The precise definition of an STOL aircraft has not been universally agreed upon. However, it has been
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STOL (Short Take Off and Landing). STOL performance of an aircraft is the ability of aircraft to take off and clear a 50-foot obstruction in a distance of 1,500 feet from beginning the takeoff run. It must also be able to stop within 1,500 feet after crossing a 50-foot obstacle on
519:) The ability of an aircraft to clear a 50-foot (15 meters) obstacle within 1,500 feet (450 meters) of commencing takeoff or in landing, to stop within 1,500 feet (450 meters) after passing over a 50-foot (15 meters) obstacle. Also called STOL. 246:
and low drag result in a high rate of climb required to clear obstacles. For landing, high drag allows the aeroplane to descend steeply to the runway without building excess speed resulting in a longer ground run. Drag is increased by use of
402:. The company says: "On an average you can expect to get a 4-7 knot reduction in stall speeds. Flying at these lower stall speeds you can reduce the take-off and landing distances by 10%". Horton STOL kits are available for several 590:
tentatively defined as an aircraft that upon taking off needs only 1,000 ft (305 m) of runway to clear a 50-ft (15-m) obstacle at the end of that distance and upon landing can clear the same obstacle and then land within 1,000 ft.
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lifting ability. The payload is critical, because many small, isolated communities rely on STOL aircraft as their only transportation link to the outside world for passengers or cargo; examples include many communities in the
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The STOL mode of flight is one during which an airplane taking off or landing is operated at climb-out and approach speeds lower than the conventionally accepted margins of airspeed above the power-off stalling speed of the
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to increase lift and reduce stall speeds. The DHC-2 Beaver STOL Kit includes a contoured leading edge, flap-gap seals, wing fences and drooped wingtips. The DHC-3 Otter STOL Kit includes a contoured leading edge and drooped
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Heavier-than-air craft that cannot take off and land vertically, but can operate within areas substantially more confined than those normally required by aircraft of the same size. Derived from short takeoff and landing
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Many different definitions of STOL have been used by different authorities and nations at various times and for a myriad of regulatory and military purposes. Some accepted definitions of STOL include:
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either on- or off-airport. Typical off-airport landing areas include snow or ice (using skis), fields or gravel riverbanks (often using special fat, low-pressure
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modification kits for "STOL benefits". The Micro kits are small vortex generators that are glued to the wing leading edge, as well as the underside of the
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Additionally, some aircraft manufacturers market their products as STOL without providing evidence that the aircraft meets any accepted definition.
1235: 896: 650: 379: 495:-efficient short takeoff and landing (CESTOL), is an aircraft with both very short runway requirements and high cruise speeds (greater than 1125: 242:
Of equal importance to short ground run is the ability to clear obstacles, such as hills, on both take off and landing. For takeoff, large
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also have STOL capability, needing a short ground roll to get airborne, but capable of a near-zero ground roll when landing.
1121: 554: 179: 1027: 224:(less common). Overall STOL performance is set by the length of runway needed to land or take off, whichever is longer. 1588: 1214: 941:"Short Field Take-Off and Landing Performance as an Enabling Technology for a Greener, More Efficient Airspace System" 73:
or ice). STOL aircraft, including those used in scheduled passenger airline operations, have also been operated from
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designated and marked for STOL aircraft operations, and designed and maintained to specified standards.
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A number of aircraft modification companies offer STOL kits for improving short-field performance.
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Anatomy of a STOL Aircraft: Designing a Modern Short Take-Off and Landing Aircraft by Chris Heintz
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that were used for scheduled passenger airline operations but are now no longer in existence.
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is an airport designed with STOL operations in mind, normally having a short single runway.
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help the plane to accelerate for flight. The landing run is minimized by strong
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and on the fin. Kits are available for a large number of light aircraft types.
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or floats, allowing the choice of landing on snow/water or a prepared runway.
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US House of Representatives Committee of Science and Technology (July 1984).
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Maiersperger, Walter P., Lieutenant Colonel, USAF (Ret) (March–April 1968).
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length requirement is a function of the square of the minimum flying speed (
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Class of airplanes that are designed to takeoff and land in a short distance
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Department of Defense Dictionary of Military and Associated Terms (JP 1-02)
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McGraw-Hill Dictionary of Scientific & Technical Terms (2003).
1158:"Statement of John Kern, Deputy Director of Flight Operations, FAA" 1078:"Glossary for Pilots and Air Traffic Services Personnel (TP 1158E)" 462: 456: 187: 74: 66: 47: 1540: 1446: 1352: 626: 395: 295: 201: 1120: 703: 200:), and most design effort is spent on reducing this number. For 1491: 1476: 473: 403: 288: 284: 193: 58: 437:
of Kelowna, British Columbia, has developed STOL Kits for the
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STOLports are not common but can be found, for example, at
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McGraw-Hill Dictionary of Scientific & Technical Terms
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Micro Dynamics vortex generators mounted on the wing of a
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Lieutenant Colonel Walter P. Maiersperger, USAF (Ret)
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These wings often use 1316: 1149: 1046: 938: 836: 1122:Arizona Department of Transportation 997:"short takeoff and landing aircraft" 794: 725:"Description of the Horton STOL Kit" 555:Arizona Department of Transportation 431:available for various Cessna models. 180:de Havilland Canada DHC-6 Twin Otter 113:adding citations to reliable sources 84: 1114: 1028:United States Department of Defense 13: 1589:Shipborne rolling vertical landing 14: 1656: 1266: 702:Crosswinds S.T.O.L. Inc. (2011). 1293: 1279: 537:Dictionary of Aeronautical Terms 439:de Havilland Canada DHC-2 Beaver 398:, control surface gap seals and 362:Bellanca Champion Model 7 series 251:(devices on the wings) and by a 89: 1015: 964: 932: 907: 890: 878: 801:Micro AeroDynamics Inc (2009). 683:Georgia Tech Research Institute 570:Federal Aviation Administration 443:de Havilland Canada DHC-3 Otter 100:needs additional citations for 69:with harsh conditions (such as 643: 502: 1: 1645:Types of take-off and landing 1298:The dictionary definition of 939:Hange, Craig E (2005-04-25). 637: 511:short takeoff and landing: ( 7: 615: 450: 150:of the Philippine Air Force 10: 1661: 864:Sierra Industries (2007). 843:Sierra Industries (2007). 822:Sierra Industries (2007). 454: 164:de Havilland Canada Dash-7 18: 1619:Floating landing platform 1539: 1511:Launch and recovery cycle 1432: 1394: 1351: 1278: 1273: 777:"Horton STOL Kit Pricing" 487: 40:short takeoff and landing 1249:Fisher Flying Products. 162:, though some, like the 995:Columbia Encyclopedia. 313: 294:Most STOL aircraft can 1614:Water landing/ditching 1366:Non-rocket spacelaunch 1361:Balanced field takeoff 610: 598: 586: 574: 559: 541: 527: 326: 239: 151: 35: 1442:Brodie landing system 704:"Crosswinds STOL Inc" 622:List of STOL aircraft 599: 595:Columbia Encyclopedia 587: 575: 560: 542: 528: 509: 321: 230: 216:, low landing speed, 146: 81:Design considerations 29: 21:Stol (disambiguation) 1609:Touch-and-go landing 948:Ames Research Center 302:), and water (using 266:devices like flaps, 109:improve this article 19:For other uses, see 1594:Short-field landing 1434:Takeoff and landing 1345:takeoff and landing 470:London City Airport 394:, conical cambered 244:power/weight ratios 206:power/weight ratios 63:takeoff and landing 55:fixed-wing aircraft 34:STOL light aircraft 1386:Zero-length launch 1100:(September 2009). 920:2006-10-13 at the 435:Stolairus Aviation 414:Micro AeroDynamics 384:Wellington, Kansas 342:leading edge cuffs 327: 240: 158:STOL aircraft are 152: 36: 1627: 1626: 1569:Emergency landing 1564:Deadstick landing 1559:Crosswind landing 1554:Corkscrew landing 1396:Assisted take-off 1290: 1289: 1138:on March 14, 2009 1076:(November 2009). 428:Sierra Industries 392:leading edge cuff 388:Horton STOL-Craft 276:vortex generators 141: 140: 133: 61:requirements for 1652: 1371:Rejected takeoff 1337: 1330: 1323: 1314: 1313: 1297: 1283: 1282: 1271: 1270: 1261: 1260: 1258: 1257: 1246: 1240: 1239: 1233: 1225: 1223: 1222: 1213:. 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Index

Stol (disambiguation)

Zenair CH 701
aircraft
conventional
fixed-wing aircraft
runway
takeoff and landing
airstrips
high altitude
STOLport

verification
improve this article
adding citations to reliable sources
Learn how and when to remove this message

GAF Nomad
fixed-wing
bush planes
de Havilland Canada Dash-7
taildraggers
PAC P-750 XSTOL
Quest Kodiak
de Havilland Canada DHC-6 Twin Otter
Peterson 260SE
Autogyros
Runway
stall speed
takeoff

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