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Piper Cherokee
Development
At the time of the introduction of the Cherokee, Piper's primary single-engine plane was the Comanche Piper cash PA-24, a larger, faster aircraft with retractable landing gear and constant speed propeller. Karl Bergey, Fred Weick and John Thorp designed the Cherokee as a less expensive alternative to the Comanche, with lower manufacturing costs and parts to compete with the Cessna 172, though some later Cherokees also had retractable landing gear and constant speed propellers.
The Cherokee and Comanche lines continued in parallel production serving different market segments over a decade, until the Comanche production was ended in 1972, to be replaced by the Piper PA-32R family.
Cherokee PA-28
The PA-28-161 Warrior II flying in the livery of Singapore Youth Flying Club. The Warrior II is still widely used around the world flight training base.
PA-28-180 on floats
The original Cherokees were the Cherokee 150 Cherokee 160 (PA-28-150 and AP-28-160), which started production in 1961 (unless otherwise stated, the model number always refers to horsepower).
In 1962, Piper Cherokee, added the 180 (PA-28-180) powered by a power of 180 (134 kW) Lycoming O-360 engine. The extra power made practical to fly with four seats occupied (depending on passenger weight and fuel load) and the model remains popular in the used-airplane market. In 1968, the cockpit was modified to replace the "push-pull" style engine controls with levers. In addition, a third window was added to each side, giving the fuselage a more modern look seen in current production. [Citation needed]
Piper continued to expand the line quickly. In 1963, the company introduced the even more powerful Cherokee 235 (PA-28-235), which competes favorably with the Cessna 182 for load capacity. The Cherokee 235 featured a Lycoming O-540 engine derated to 235 hp (175 kW) and a long wing that eventually would be used for the Cherokee Six. 17 including tip tanks gallons capacity each, which total fuel capacity of the Cherokee 235-84 gallons. The aircraft fuselage was lengthened in 1973 giving more leg room in the rear. The stabilizer area was also increased. In 1973 the trade name has been changed from "235" for the magazine. In 1974 it was changed again to the Pathfinder. Pathfinder production continued until 1977. There was no 1978 model. In 1979, the aircraft was given the Piper tapered wing and was renamed again the Dakota. [Citation needed]
PA-28-140, built 1966
In 1964, the company squarely in the lower end of the line with the Cherokee 140 (PA-28-140), which was designed for training and initially shipped with only two seats. One source of confusion is the fact that the PA-28-140 was slightly modified engine shortly after introduction to produce 150 horsepower (112 kW), but retained the name of -140.
Piper PA-28R-200 Cherokee Arrow showing the landing gear doors that separate This model of retractable landing gear
Piper PA-28R-201 Cherokee Arrow IV with its distinctive "T" tail
In 1967, Piper introduced the PA-28R-180 Cherokee Arrow. This aircraft was equipped with a constant speed propeller, retractable landing gear and was powered by a power of 180 (134 kW) Lycoming IO-360-B1E. A 200 horsepower (149 kW) version powered by a Lycoming IO-360-c1c was offered as an option starting in 1969 and designated the PA-28R-200, 180-hp model force was released after 1971. When the arrow was introduced, Piper removed the Cherokee 160 and Cherokee 150 production.
The Arrow II was published in 1972, with a five inch fuselage to increase legroom for rear seat passengers. In 1977, Piper introduced the Arrow III (PA-28R-201), which offered semi-tapered wing and stabilizer more time, a design feature that had previously been successfully introduced in the PA-28-181 and provided better handling at low speed. It also provided more fuel tanks, increasing the capacity of 50-77 gallons.
The first turbocharged model, the PA-28R-201T was also featured in 1977, powered by a six-cylinder Continental TSIO-360-F equipped with a turbocharger Rajay. A three-bladed propeller was optional.
In 1979, the Arrow was re-designed again as the PA-28RT-201 Arrow IV, with a "T" tail that resembled the other aircraft in the Piper line at the moment.
In 1971, Piper Cherokee Published a variant called 140 Cherokee Cruiser 2 +2. Although the aircraft maintains the name 140, which was, in fact, a power 150 (110 kW) flat (112 kW), and sent mainly as a four-seat version. In 1973, the Cherokee 180 Cherokee Challenger was, and that its fuselage lengthened slightly and extended her wings, and the Cherokee 235 was appointed charger with similar changes fuselage. In 1974, Piper marketing changed the names of some of the Cherokee models again, renaming the Cruiser 2 +2 (140) simply Cruiser, the Challenger the Archer (model PA-28-181) and charger (235) of Pathfinder.
Piper Cherokee 150 reintroduced in 1974, the new designation of Cherokee Warrior (PA-28-151) and gives body lying in the Archer and a new wing, semi-conical.
Polly Vacher, a UK pilot unprecedented in its PA-28-236 Dakota. The plane was built in 1994.
In 1977, Piper stopped producing the Cruiser (140) and Pathfinder (235), but introduced a new 235-horsepower (175 kW) of aircraft, the Dakota (PA-28-236), based on models Cherokee 235, Charger, Pathfinder, but with the new wing lengths.
The PA-28-201T Turbo Dakota post introduction of the PA-28-236 Dakota in 1979. The fuselage was essentially the same as a fixed gear Arrow III, and was powered by a turbocharged Continental TSIO-360-FB production engine 200 hp (149 kW). The plane did not sell well and production ended in 1980.
In 1978, Piper Warrior updated 160 horsepower (119 kW) PA-28-161 changing its name to Cherokee Warrior II. This aircraft had slightly improved aerodynamic fairing the wheels. The latest models of the Warrior II, manufactured from July 1982 to incorporate an increased gross weight of 2440 pounds, giving a payload of more than 900 pounds. This same aircraft, now available with a cab glass is available as Guerrero III, and is marketed as a training aircraft.
PA-32
Main article: Piper Cherokee Six
In 1965, Piper developed the Piper Cherokee Six, designated PA-32, by stretching of the AP-28 design. It featured a lengthened fuselage and seats a pilot and five passengers.
Brazil and Argentina production
PA-28 were built under license in Brazil as the Embraer EMB-711 EMB-711C Corisco (PA-28R-200), EMB-711B (PA-28R-201) EMB-711T (PA-28RT-201) and EMB-711ST Corisco Turbo (PA-28RT-201T) and the EMB-712 Tupi (PA-28-181). Argentina's production was carried by SA Chincul of San Juan, Argentina. Chincul SA 960 airplanes built between 1972 and 1995, including the Cherokee Archer, Dakota, Arrow, Turbo Arrow.
New Piper Aircraft
The original Piper Aircraft Company was declared bankruptcy in 1991. In 1995, The New Piper Aircraft Company was created. Piper Aircraft was renamed once again in 2006. The company currently produces two PA-28 Cherokee variants: 160 hp (119 kW) Warrior III (PA-28-161) and 200 horsepower (149 kW) retractable Arrow (PA-28R-201). All are now available with Avidyne Entegra glass booths.
Design
Wing
Originally, all Cherokees had a constant planform rectangular wing, popularly known as the Hershey Bar wing because of its resemblance to the candy bar background.
Beginning with the Warrior in 1974, Piper moved to a tapered wing with the NACA 652-415 profile and a wingspan of two feet long. Both variants have a Cherokee wing wing root angle, ie the edge of the wing is swept forward as it nears the fuselage body, rather than meeting the body at a perpendicular angle.
The documented takeoff distance, cruise speed, and landing distance of Cherokees of the same power with different types of wing is very similar and some of the differences that exist in the rear wing cone models can be attributed to a better fairings and seals more than the design different wings. The Hershey bar wing design is not markedly lower than the tapered design, and in some respects is quite advantageous. As a designer John Piper Cherokee Thorp says, "Tapered wings tend to put an outboard motor, which reduces the effectiveness of the ailerons and the increased likelihood of a roll-off in a turn."
As Peter Garrison, explains further: "To avoid post-edge designers have resorted to providing the outer parts of the wings of conic sections more curved profile, fell or enlarged edges, fixed or automatic top slots or edge strips, and, more commonly, money wing or washed out. The problem with these solutions is that they all increase the resistance, the cancellation of any profits from the tapered wing was to deliver in the first place. "
Flight Controls
For the family Piper used their traditional configuration Cherokee flight control. The horizontal tail is a stabilizer with an anti-servo tab (sometimes called a form of struggle against the scale). The tab moves against the servo in the same direction of motion stabilizer, making pitch control "heavier" as the stabilizer is moved from the cut position. Flaps can extend up to 40 years, but are considerably smaller and possibly less effective, the fins a Cessna 172. Typically, you use 25 flaps for a short or soft-field takeoff. The ailerons, flaps, stabilizer, stabilization and adjustment are controlled via cables and pulleys.
In the cockpit, all Cherokees use control yokes rather than sticks, together with the rudder pedals. The pilot operates the flaps manually using a bar Johnson located between the front seats: for zero degrees the lever is flat against the floor and pulled up to select the stop position 10, 25 and 40.
Seniors Cherokees use an overhead crank for adjusting stabilizer (correctly called anti-servo tab), while the later use an adjustment wheel on the floor between the front seats immediately behind the bar tab.
All Cherokees have a brake lever on the driver's side dashboard. differential brakes toe in rudder pedals were an optional add-on for earlier Cherokees, and became standard with later models.
Some earlier Cherokees, used knobs control in the gas mixture, and propeller advance (where applicable), while later Cherokees use a collection of two or three levers of control in a quadrant accelerator.
Cherokees tend to include a button to adjust the rudder, which actually controls a set of springs acting on the rudder pedals instead of a tab external regulation in the rudder in other words, the surface is cut by tension rather than aerodynamically control.
Variants
PA-28-140 Cherokee Cruiser
Two place, fixed land airplane landing gear, the Lycoming O-320-E2A 150 hp (112 kW), gross weight 1950 lbs (885 kg). First Certificate on February 14, 1964. Approved in 2150 a pound (975 kg) gross weight of four aircraft on 17 June 1965.
-PA 28-150 Cherokee
Four place, fixed landing aircraft Earth Arts, Lycoming O-320-A2B or O-320 engine-E2A 150 hp (112 kW), gross weight 2150 lbs (975 kg). First Certificate 2 June 1961.
PA-28-151 Cherokee Warrior
Four place, fixed land airplane landing gear, the Lycoming O-320-E3D 150 hp (112 kW), gross weight 2325 lbs (1,055 kg). First certificate on August 9 1973. Changes for PA-28-150 includes a tapered wing.
-PA 28-160 Cherokee
Four place landplane fixed landing gear, Lycoming O-320-B2B or motor O-320-D2A of 160 hp (119 kW), gross weight 2200 lbs (998 kg). First letter of 31 October 1960.
PA-28-161 Warrior II
Four place, land airplane landing gear fixed, Lycoming O-320-D3G engine or O-320-D2A 160 hp (119 kW), gross weight 2325 lbs (1,055 kg). In the first certified the November 2, 1976. Changes for PA-28-160 includes a wing sharp. Certified on 1 July 1982 the gross weight of 2.440 pounds (1.107 kg).
PA-28-161 Warrior III
Four place, fixed land airplane landing gear, the Lycoming O-320-D3G 160 hp (119 kW), gross weight 2440 lbs (1107 kg). First registered on July 1, 1994.
-PA 28-180 Cherokee
Four place aircraft terrestrial fixed landing gear, Lycoming O-360-A3A or engine O-360-A4A 180 hp (134 kW), gross weight 2400 lbs (1,089 kg). First certified August 3, 1962.
PA-28-180 Archer
Four place landplane fixed landing gear, Lycoming O-360-A4A or engine O-360-A4M 180 hp (134 kW), gross weight 2450 lbs (1,111 kg). First Certificate on May 22, 1972. Changes for PA-28-180 Cherokee include a five inch fuselage extension, increase wing span, over the horizontal tail, weight gain Gross and other minor changes.
-PA 28-181 Archer II
Four fixed place of land airplane landing gear, Lycoming O-360-A4M or engine O-360-A4A 180 hp (134 kW), gross weight 2550 lbs (1,157 kg). First certified July 8, 1975. The changes in the PA-28-180 include a tapered wing.
PA-28-181 Archer III
Four place landplane fixed undercarriage, the Lycoming O-360-A4M 180 hp (134 kW), gross weight 2550 lbs (1,157 kg). First certified August 30, 1994.
Turbo Dakota PA-28-201T
Four place landplane fixed landing gear, turbocharged Continental TSIO-360-FB, engine 200 hp (149 kW), gross weight 2900 lbs (1,315 kg). First certified on December 14, 1978.
PA 28-235 Cherokee-Pathfinder
Four place landplane fixed landing gear, Lycoming O-540-B2B5, O-540-B1B5, or O-540-B4B5 engine 235 hp (175 kW), gross weight 2900 lbs (1,315 kg). First certified July 15, 1963.
PA 28-235 Cherokee-Pathfinder
Four place landplane fixed undercarriage, Lycoming O-540-B4B5 235 hp (175 kW), gross weight 3000 lbs (1,361 kg). First certified June 9, 1972. Changes to the certification Pathfinder PA-1963 28-235 Cherokee include a five inch fuselage extension, increased wing span, over the horizontal tail, increased gross weight and other minor changes.
PA-28-236 Dakota
Four place landplane fixed landing gear, Lycoming O-540-J3A5D engine 235 hp (175 kW), gross weight 3000 lbs (1,361 kg). First certified place on 1 June 1978. Changes for PA-1972 certification 28-235 Cherokee Pathfinder include tapered flanges.
PA-28S-160 Cherokee
Four place seaplane Fixed landing gear, a Lycoming O-320-D2A 160 hp (119 kW), gross weight 2140 lbs (971 kg). First certified February 25, 1963.
PA-28S-180 Cherokee
Four place seaplane fixed landing gear, Lycoming O-360-A3A or engine O-360-A4A 180 hp (134 kW), gross weight 2222 lbs (1,008 kg). First Certificate 10 May 1963.
PA-28R-180 Arrow
Four place, land airplane retractable landing gear, Lycoming IO-360-B1E 180 hp (134 kW), gross weight 2500 lbs (1134 kg). First certified on 8 June 1967.
PA-28R-200 Arrow
Four place, land airplane retractable landing gear, Lycoming IO-360-200 c1c HP (149 kW), gross weight 2600 lbs (1,179 kg). First certified January 16, 1969.
PA-28R-200 Arrow II
Four place, land airplane retractable landing gear, Lycoming IO-360-C1C6 c1c engine or 200 hp (149 kW), gross weight 2650 lbs (1,202 kg). In the first certified the December 2, 1971. Changes from the 1969 Arrow PA-28R-certified 200 include a five inch fuselage extension, increases the length of the wings, tail largest horizontal, increased gross weight and other minor changes.
PA-28R-201 Arrow III
Four place, land airplane retractable landing gear, Lycoming IO-360-C1C6 engine 200 hp (149 kW), gross weight 2750 lbs (1,247 kg). First Certificate on November 2, 1976.
PA-28R-201T Turbo Arrow III
Four place, land airplane retractable landing gear, turbocharged Continental TSIO-360-F or engine TSIO-360-FB 200 hp (149 kW), gross weight 2900 lbs (1,315 kg). In the first certified the November 2, 1976.
PA-28RT-201 Arrow IV
Four place landplane retractable landing gear, Lycoming IO-360-C1C6 engine 200 hp (149 kW), gross weight 2750 lbs (1,247 kg). In the first certified the November 13, 1978. It has a T. tail
Turbo Arrow IV PA-28RT-201T
Four place, land airplane retractable landing gear, turbocharged Continental TSIO-360-FB 200 hp (149 kW) gross weight 2900 lbs (1,315 kg). First registered on November 13, 1978. It has a tail T.
Operators
military operators
Chile
Air Force Chile
Finland
Finnish Air Force
Accidents and Incidents
September 9, 1969, Allegheny Airlines Flight 853 collided with a Piper PA-28-181 Archer City of Fairland, Indiana, killing all aboard both aircraft.
August 31, 1986, Aeromxico Flight 498 collided with a Piper PA 28-181 Archer, the city Cerritos, California, killing all aboard both aircraft and 15 people on the ground. It was the worst air disaster in the history of Los Angeles.
February 18, 2010, Andrew Joseph Stack III deliberately flew his Piper PA-28-236 in Dakota building an office complex of Echelon in Austin, Texas, in an apparent revenge attack in the office Internal Revenue Service is there.
Specifications (1964 model PA-140 Cherokee 28-140)
Piper Aircraft Data Owner's Manual
Features General
Crew: one pilot
Capacity: three passengers
Length: 23.3 feet (7.16 m)
Wingspan: 30.0 feet (9.2 m)
Height: 7.3 feet (2.25 m)
Wing area: 160 m² (15.14 m)
Airfoil: NACA 652-415
Weight: 1201 lbs (544 kg)
Loaded Weight: 2150 lbs (975 kg)
Payload: 949 lbs (430 kg)
Max takeoff weight: 2150 lbs (975 kg)
Powerplant: 1 Lycoming M74DM Sensenich O-320-E2A 150 hp (113 kW)
Propeller diameter: 74 inches (1.9 m)
Performance
Maximum speed: 123 knots (142 mph, 230 km / h)
Cruising speed: 108 knots (124 mph (200 km / h), 201 km / h)
stall speed: 47 knots (54 mph, 87 kmh)
Distance: 465 nm (535 cm, 867 km)
Service ceiling: 14,300 feet (4400 m)
Rate of climb: 660 m / min (3.4 m / s)
Wing loading: 13.4 lb square feet (64.4 kg / m²)
Power / mass: 14.3 lb / hp (0.116 kW / kg)
Avionics
1964 factory standard, no
See also
Related development
Piper PA-32
Piper PA-44 Seminole
Similar Aircraft
Beechcraft Musketeer
Cessna 172
Cessna 177
Cessna 182
Diamond DA40
Socata TB
Grumman AA-5 Traveler, Cheetah, and Tiger
Related Lists
List of airliners
List of civil aircraft
References
^ Abcdefghijk plane and the pilot: 1978 Aircraft Directory, pages 62-64. Werner & Werner Corp, Santa Monica California, 1977. ISBN 0-918312-00-0
^ Twombly, Mark R. (Undated). "Training Aircraft Review: The Piper Warrior III." http://flighttraining.aopa.org/learntofly/articles/2988.cfm. Retrieved on 02/06/2008.
↑ New Piper Aircraft (undated). "Welcome to the Arrow." http://www.newpiper.com/aircraft/arrow/default.asp. Retrieved on 02/06/2008.
^ Ab New Piper Aircraft (undated). "Welcome to the Warrior III." iii http://www.newpiper.com/aircraft/warrior ~ / default.asp. Retrieved 2008-02-05.
^ Piper Aircraft (2009). "Aircraft discontinued." http://www.newpiper.com/pages/DiscontinuedAircraft.cfm. Retrieved on 03/06/2009.
^ Niles, Russ (July 2009). Piper Likes Imprimis future. " Http: / / www.avweb.com/news/airventure/EAAAirVenture2009_Piper_Imprimus_200831-1.html. Retrieved 07/29/2009.
^ Collins, Richard L. (May 2005). "Flying Four by fours." http://www.flyingmag.com/article.asp?section_id=13&article_id=552. Retrieved on 02/06/2008.
^ New Piper Aircraft (undated). "Welcome to the Saratoga II TC". http://www.newpiper.com/aircraft/saratoga ~ tc /. Retrieved 02/06/2008.
^ "Karl Bergey, Chairman and CEO." September 25, 2007. Http: / / www.bergey.com / About_BWC.htm # Key Personnel. Retrieved 09/25/2007.
Abc ^ Twombly, Mark: "Arrow Piper," AOPA Pilot, June 1986.
^ Abcde Airliners.net (undated). "The Piper Cherokee PA-28 Series." http://www.airliners.net/info/stats.main?id=304. Retrieved on 02/06/2008.
ABCDEFGHIJKLMNOPQRSTU VWXYZ ^ Federal Aviation Administration (January 2009). "CERTIFICATE TYPE DATA SHEET NO. 2A13 Version 49. "Http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/a44b41c7e7d7d7458625753c004f4a2d/ $ FILE/2A13.pdf. Retrieved on 24/02/2010.
^ Taylor, John WR: Jane's Pocket Book Light Aircraft revised edition, page 171. Jane's Publishing Company Ltd, 1982. ISBN 0 7106 0195 6
^ Piper Aircraft (2009). "Warrior III price and equipment (full specifications PDF)." http://www.newpiper.com/home/pages/WarriorPriceStandardEquipment.cfm. Retrieved on 01/06/2009.
^ Pereira de Andrade, Roberto.: Enciclopdia of perverse Brasileiros, Editora Globo, 1997. ISBN 8525021377
^ Ab Garrison, Peter (January 2003). "Wings rectangular." http://www.flyingmag.com/rectangular-wings?page=0, 1. Retrieved on 26/12/2009.
^ Abcdefgh Piper Aircraft: Cherokee PA-140 Owner's Manual 28-140. Piper Aircraft Corporation publication 753 584, February 1964, revised May 27, 1977
Network Aviation Security ^: Allegheny Airlines Flight 853
Network Aviation Security ^: Aeromexico Flight 498
^ Austin American Statesman coverage plane crash
External Links
Wikimedia Wikipedia on Piper Cherokee PA-28
Aircraft.co.za – Piper PA-28 family
Aircraft-Info.net – Piper Cherokee PA-28 series
New Homepage Piper Aircraft
Cherokee Pilots Association includes performance statistics for most PA-28 PA-32 models
Piper Cherokee and Arrow Report Highlights AOPA safety of safety and accidents caused by the AP-28 and PA-28R
Check Six.com – The history of the aircraft "in a photo accident Tree" – Map of the photo is a Piper Archer
EV
Piper
Model Numbers
Civil
E-2 F-2 G-2 H-2 J-2) J-J 3-4 J 5-6 PA-PA PA-7-8 PA-11 PA-12 PA-14 PA-15 PA-16 PA-17 PA-18 PA-19 PA-20 PA-22 PA-23 PA-24 PA-25 PA-26 PA-28 PA-29 PA-30 PA-31 PA-31T PA-32 PA- 32R PA-33 PA-34 PA-35 PA-36 PA-38 PA-39 PA-40 PA-41 PA-42 PA-44 PA-46 PA-47 PA-60 PT-PiperSport 1-1 PWA PWA PWA-6-8
Military
AE C-83 HE L-4 L-14 L-18 L-21 LNP NE O-59 PA-48 TG-U 8-7
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Categories: Piper | United States civil aircraft 1969Hidden 1960-Categories: Articles with unsourced statements | Articles lacking reliable references from March 2008 | Articles needing additional references from February 2008 | | Low Single-engine airplanes | aircraft propeller aircraft
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