Helio Courier

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Helio Courier
Helio H295 Courier Valle AZ 22.10.05R.jpg
Helio H295 Super Courier of 1967 at Valle, Arizona, in October 2005
Role STOL Utility aircraft
Manufacturer Helio Aircraft Company
Designer Otto C. Koppen, Lynn Bollinger[1]
First flight 14 April 1949
(Helioplane #1)
Introduction 1954
Status some still flying in 2015
Primary user Military forces and private pilots
Number built 500 (approximate total)
Unit cost
$151,600 in 1984
Variants Helio Stallion
Helio Courier H-295 on floats, Lake Hood Seaplane Base, Anchorage, AK

The Helio Courier is a cantilever high-wing light C/STOL utility aircraft designed in 1949.

Around 500 of these aircraft were manufactured in Pittsburg, Kansas from 1954 until 1974 by the Helio Aircraft Company. The design featured four leading edge slats that deployed automatically, and large trailing edge flaps. The engine was the 295 hp Lycoming GO-480, which had a gearbox that lowered the output RPM and allowed for the use of a large three-bladed propeller to further improve takeoff performance. Couriers were famous for their takeoffs, which often took only a few plane lengths and then climbed at very high angles. The engine, however, required constant maintenance and was a major downside to the design.

During the early 1980s, new owners (Helio Aircraft Ltd.) made an attempt to build new aircraft with direct-drive Lycoming engines, to replace troublesome and expensive geared engines. In a further effort to reduce weight, a new composite landing gear was featured. The new models also featured modest winglets. Two models were produced, the H-800 and H-700. A total of 18 aircraft were built. The rights to the Helio Stallion and Helio Courier were acquired by Helio Aircraft of Prescott, Arizona, and will soon[when?] be returned to production.[2]

Design and development[edit]

Professor Otto C. Koppen designed aircraft for the Stout Metal Airplane Division of the Ford Motor Company, including the Ford Flivver, an aircraft that was supposed to be mass-produced by Ford. Koppen went on to design the Helio Courier.[3]

The demonstrator for the Courier's concept, "Helioplane #1", was converted by the then-local Wiggins Airways firm from a Piper PA-17 Vagabond Trainer, one of the so-named "short-wing Pipers" in production following World War II. Only the cabin area of the PA-17's original airframe remained unmodified, with the fuselage lengthened by four feet (1.2 meters), given a taller fin-rudder unit, clipped the Vagabond's stock 29 ft-3 inch (8.92 meter) wingspan down to only some 28.5 feet (8.7 meters), fitted the shortened wings with full-span leading-edge slats, long-span wing flaps that forced the ailerons to be much diminished in size, and a longer-travel main landing gear of a taller design, not unlike that of the 1930s-origin Fieseler Fi 156 German military STOL pioneer aircraft. The powerplant for the demonstrator was switched to the Continental C85 boxer-four cylinder air-cooled engine, upgraded with fuel-injection, and uniquely equipped with a multi-belt speed reduction unit to drive its Aeroproducts nine-foot (2.75 meter) diameter, variable-pitch two-blade propeller, which contributed greatly to the amazing STOL flight characteristics of the demonstrator aircraft.[4][5] The demonstrator's first flight took place on April 8, 1949, flying from what was then called the Boston Metropolitan Airport, an airport located within the greater Boston suburban town of Canton, Massachusetts which was closed at the end of the 1960s, after the opening of nearby Norwood Memorial Airport (only 1.5 miles (2.5 km) NNW of the Canton facility), which itself first opened as an emergency WW II airfield in 1942.[6]

For the construction of the production Courier aircraft, its all aluminum-clad airframe features a welded 15G steel-tube center section fuselage, with shoulder harnesses that protect the occupants in an emergency. The wings are of conventional aluminum construction, but feature Handley Page leading-edge slats that deploy automatically when the aircraft's airspeed falls below a certain value — 55 to 60 miles per hour (89 to 97 km/h). The slats contribute to the Helio's outstanding short takeoff and landing (STOL) capability, and allow for stall/spin-proof controllable flight. In conjunction with the leading-edge slats, 74% of the trailing edge incorporates high-lift slotted flaps, which together with interrupter blades atop each wing when roll control is lost at very low airspeed, allows for a tight turning radius. The Helio Courier could maintain control at speeds as low as 27 miles per hour (43 km/h).[7]

The design of the Helio features a large vertical tail surface and rudder for control at very low flight speeds. However, on conventional geared aircraft (taildraggers), the airplane tends to be sensitive to crosswinds, thus a crosswind gear option is available, allowing the main tires to caster left or right 20 degrees, increasing the crosswind component to 25 miles per hour (40 km/h). The Helio has its main gear placement far forward of the cabin, enabling hard braking on unprepared landing areas. A tricycle-gear model was produced, but is unsuitable for unprepared rough terrain.

Helios are also capable of being equipped with floats; both straight and amphibious floats being offered.

Operational history[edit]

Helio Courier slow flight
Helio Courier in hangar at JAARS
A USAF U-10B from the 5th Special Operations Squadron in Vietnam, 1969.
A U-10D with a C-119
Richard Bach, author of Jonathan Livingston Seagull, and Lynn Garrison with Helio Courier G-ARMU used for Von Richthofen and Brown, 1970

With a minimum-control speed of around 28 mph, the Courier is perfectly suited for confined off-airport operations. The first one was certified in July 1954 and powered by the 260 hp Lycoming GO-435-C2B2. The first production Courier (Serial Number 001, dubbed "Ol' Number 1")C-G001 was previously owned and operated by JAARS as N242B until 2010.[8] Jaars Helio Courier has been a frequent airshow performer at EAA AirVenture Oshkosh for decades, displaying its slow flight capability in front of thousands and serving as a drop plane for the Liberty Parachute Team.[9]

In 1957, a "Strato Courier" set an altitude record over Mexico City, Mexico at 31,200 ft powered by a geared Lycoming GSO-480-A1A5 (340 hp), only one was built. The Super Courier, a more powerful derivative, was used by the US Air Force from 1958 onward, by the US Army Special Forces in the 1960s and 1970s and by Air America during the Vietnam War as the U-10. In U.S. Army and Air Force service, the U-10 Super Courier was used for liaison work, light cargo and supply drops, psychological warfare, forward air control (Air Force), insertion and extraction land and sea (Army) and reconnaissance. Various versions were produced up through the 1980s, including turbine-powered variants.

The Super Courier saw military service in the United States as the U-10 (ex L-28). Over 120 were built: The L-28A (2, later redesignated U-10A), U-10A (26), U-10B extended range and paratrooper doors (57), and the U-10D with a higher gross weight(36). There was no U-10C.

Helios remain very popular among bush pilots in Canada (32 current) and Alaska and missionaries who fly into rough, relatively unprepared jungle airstrips because of its superior STOL abilities. Some operators use the Helio Couriers for aerial observation. Both Winged Vision Inc. of Gaithersburg, Maryland and the Pima County, Arizona, Sheriff's Department each operate two of the rare tri-gear model and mount gyro-stabilized cameras under the wing for aerial observation.[10] Pima County mounts a FLIR camera for law enforcement, and Winged Vision mounts a high definition television camera for coverage of major sports events.[11]

Variants[edit]

Koppen-Bollinger Helioplane.[12]
Original prototype soon re-named Helio Courier.
Helioplane Four.
unknown possible variant.
Helioplane Two.
unknown possible variant.
Hi-Vision Courier.
unknown possible variant.
H-291.
Prototype, one built.
H-295 Super Courier.
Variant with a Lycoming GO-480-G1D6, purchased by USAF as U-10D, 173 built.
HT-295 Super Courier or Trigear Courier.
H-295 with tricycle undercarriage, 19 built.
H-250 Courier.
H-295 with lengthened fuselage and Lycoming O-540-A1A5 engine, 41 built.
H-391 Courier.
Prototype with Lycoming GO-435-C2 engine, one built.
H-391B Courier.

Production version of H-391, 102 built.

H-392 Strato Courier.
High-altitude version of H-391 with Lycoming GSO-480-A1A5 engine (340 hp).
H-395 Super Courier.
H-391B with Lycoming GO-480-G1D6, purchased by USAF as U-10A and U-10B, 138 built.
H-395A Courier.
Variant of the H-395 with a Lycoming GO-435-C2B6 engine, seven built.
H-500 Twin Courier.
Twin-engined H-395 for the CIA. Very little information available except seven delivered to the CIA under front designation U-5.
Helio H-550 Stallion.
Turboprop powered development
H-580 Twin Courier.
A longer nosed H-500 with twin wing mounted piston engines, five built.[1]
H-634 Twin Stallion
Planned twin Allison C250 powered Stallion.
H-700 Courier.
H-295 with redesigned wing and undercarriage and Lycoming TIO-540-J2B engine.
H-800 Courier.
H-700 with Lycoming IO-720-A1B engine, 18 built (H-700 and H-800 together).
L-24 Courier.
Military version of the H-391 Courier.
L-28 Courier.
Military version of the H-395 Courier.
U-5 Twin Courier.
Probable front designation for CIA Twin Couriers.
U-10 Courier
Re-designation of L-28 Courier
U-24 Stallion
Military designation for H-550 Stallion

Operators[edit]

Military operators[edit]

 Bophuthatswana
 Italy
 Peru
 Thailand
 United States

Civil operators[edit]

Aircraft on display[edit]

Helio Courier flying in the United Kingdom in 2016.
Thailand
United States

Specifications (U-10D Super Courier)[edit]

Data from [21]

General characteristics

  • Crew: one, pilot
  • Capacity: 5 passengers
  • Length: 30 ft 8 in (9.35 m)
  • Wingspan: 39 ft 0 in (11.89 m)
  • Height: 8 ft 10 in (2.69 m)
  • Useful load: 1,320 lb (600 kg)
  • Loaded weight: 3,600 lb (1,636 kg)
  • Powerplant: 1 × Lycoming GO-480-G1D6 geared 6-cylinder engine, 295 hp (220 kW)

Performance

See also[edit]

Related development
Aircraft of comparable role, configuration and era

References[edit]

Notes[edit]

  1. ^ a b Flying, March 1984, p. 54.
  2. ^ "Helio Courier." Helio Aircraft. Retrieved: October 3, 2011.
  3. ^ Peterson, Norm. "There's a Ford in your Future." Sport Aviation, August 1991.
  4. ^ a b "Smithsonian National Air & Space Museum - Collections - Helioplane - Long Description". airandspace.si.edu. National Air & Space Museum. Retrieved December 27, 2016. Professor Koppen was not a newcomer to the so-called affordable safe light plane design field as he was the designer of Ford's 1925 Flivver Plane and designed the pre-World War II two-control, spin proof General Skyfarer airplane. The professors tried several sources for financial support in government, academia, and industry for the experimental project but eventually they put up their own money. They arranged for Greater Boston Metropolitan Airport fixed base operator, E.W. Wiggins Airways and volunteers to convert a Piper PA-17 Vagabond to the two-place Helio No.1, and, in the end, the investment of the professors was about $6,000. The only unmodified part of the Vagabond was the fuselage cabin area. The original 65 hp Continental engine was replaced with a fuel-injected 85 hp Continental fitted with a multi-belt reduction unit that drove a specially designed nine-foot Koppers Aeromatic propeller. This extra large diameter propeller with its large thrust component was a major contributor to the success of the Helio-1. The propeller's wide slipstream coverage of the wing slats and slotted flaps provided a substantial added lift component during the take-off, landing and the slow/near hover flight regimes. The large propeller size dictated a higher-than-normal main landing gear with long throw shock struts to achieve sufficient propeller ground clearance...The fuselage was lengthened by nearly four feet and the Vagabond's already short 29-foot 3-inch wing was shortened by another nine inches. The wing had a complete array of the high lift devices available at that time, including leading edges with retractable full span Handley Page automatic slats and trailing edges with the equivalent of full-span slotted flaps. The ailerons could be drooped in the slow speed configuration to act as flaps and still perform for banking purposes. In addition to these devices, a later development called a lateral roll control augmenter was installed at the wing leading slat gaps. This device was aerodynamically positioned at the slat gap so that it provided excellent slow speed roll stabilization. 
  5. ^ "Simplicity and Safety, Features of the Helioplane, a Promising American Light Aircraft Prototype". Flight International. United Kingdom: Flightglobal. October 20, 1949. Retrieved September 3, 2017. 
  6. ^ Freeman, Paul (July 3, 2015). "Abandoned and Little-Known Airfields - Massachusetts, Southwest Boston Area - Massachusetts Air Terminal & Arena / Canton Airport / Massachusetts Air Terminal / Boston Metropolitan Airport, Canton, MA". www.airfields-freeman.com. Paul Freeman. Retrieved December 27, 2016. The last aircraft-related company at Canton Airport was Helio Aircraft Corporation. In the late 1940s, Otto Koppen of MIT & Dr. Lynn Bollinger of Harvard developed the first Helioplane experimental prototype, a short take off & landing (STOL) light aircraft...The professors arranged for Greater Boston Metropolitan Airport fixed base operator, E.W. Wiggins Airways & volunteers to convert a Piper PA-17 Vagabond to the 2-place Helio No.1. The successful first flight was in 1949. 
  7. ^ "Small Plane Copies Copter." Popular Science, August 1949, p. 135.
  8. ^ "Very First Helio Courier Alive and Well in Canada." Archived 2012-02-13 at the Wayback Machine. EEA, February 13, 2012.
  9. ^ Koepenick, Jim. "Antiques and Classics at Oshkosh '91." Sport Aviation, November 1991.
  10. ^ Thomas Horne (June 2014). "Eye on Sport". AOPA Pilot: 64. 
  11. ^ "News & Press Coverage." Helio Aircraft. Retrieved: October 3, 2011.
  12. ^ "Leaps Off Lawn." Popular Science, October 1949, pp. 109, 110.
  13. ^ Hatch, Paul F. (July 1985). "Air Forces of the World: Bophuthatswana Defence Force Air Wing". Air Pictorial. Vol. 47 no. 7. p. 249. 
  14. ^ aeroflight
  15. ^ "Building 1". Royal Thai Air Force Museum. Archived from the original on 26 October 2013. Retrieved 16 January 2017. 
  16. ^ "Airframe Dossier - Helio U-10B, s/n 66-14332 USAF, c/n 576". Aerial Visuals. AerialVisuals.ca. Retrieved 17 January 2017. 
  17. ^ "Hurlburt Field Memorial Air Park Guide" (PDF). Hurlburt Field. Retrieved 16 January 2017. 
  18. ^ "Airframe Dossier - Helio U-10A Super Courier, s/n 62-3606 USAF, c/n 540, c/r N11619". Aerial Visuals. AerialVisuals.ca. Retrieved 16 January 2017. 
  19. ^ "U-10B “SUPER COURIER”". Museum of Aviation. Museum of Aviation. Retrieved 16 January 2017. 
  20. ^ "Helio U-10D Super Courier". National Museum of the US Air Force. 18 May 2015. Retrieved 16 January 2017. 
  21. ^ "Helio Courier: Performance & Specifications." Helio Aircraft. Retrieved: October 3, 2011.

Bibliography[edit]

  • Ogden, Bob. Aviation Museums and Collections of North America. Tonbridge, Kent, UK: Air-Britain (Historians) Ltd, 2007. ISBN 0-85130-385-4.
  • Simpson, R. W. Airlife's General Aviation. Shrewsbury, UK: Airlife Publishing, 1995, pp. 208–210. ISBN 1-85310-577-5.
  • Taylor, Michael J. H. Jane's Encyclopedia of Aviation. London: Studio Editions, 1989. ISBN 0-517-69186-8.
  • World Aircraft Information Files. London: Bright Star Publishing, File 896, sheet 18.

External links[edit]