The Piper Cheyenne 400LS is uniquely positioned to adapt to our various missions in payload, distance and speed. [6], In the late 1970s, Piper avoided developing a clean-sheet light business jet to compete with the Cessna Citation I and upgraded its PT6As from 720 to 1,000 hp (540 to 750 kW) Honeywell TPE331-14s. Engine 1 Time. 9146.0 . The cabin measures 12.6 feet long by 4.2 feet wide by 4.3 feet tall giving it a total cabin volume of 227.2 cubic feet making it comfortable for 5 passengers, with the maximum configuration seating 9. This 1981 Piper Cheyenne I has been based in North Carolina since new. This 1981 Piper Cheyenne I has been based in North Carolina since new. The Piper PA-42 Cheyenne is a turboprop aircraft built by Piper Aircraft. All records are complete and … Find N2458W 1980 PIPER CHEYENNE I on Aircraft.com. Corrosion of the airframe has been rare, thanks to Piper’s use of extensive anti-corrosion treatments and epoxy primers. PA-42 may also refer to, "Piper Cheyenne 400LS: Big Dog Turboprop Could Best A Citation I", "Piper Cheyenne 400LS Record Set by Chuck Yeager", "Quick Look: Piper Cheyenne 400LS, Rare hot rod performs more like a jet", "Chuck Yeager - Chasing the Demons for 72 Years", "Piper PA-42 Type Certificate data sheet No. Typical passenger configuration is the typical number of passengers the jet is configured to accommodate 5 passengers, however each jet will have a custom configuration to accommodate an owners specific needs and will therefore vary. Passenger and baggage amounts can greatly effect the performance of an aircraft since minimum runway lengths, range and speed are all effected by its weight. [7] It can climb directly to FL 410 at its 12,050 lb (5,470 kg) MTOW and typical single-pilot BOWs are 7,850–7,900 lb (3,560–3,580 kg). N2519X features upgraded Garmin Avionics, low airframe time, recent hot sections and prop overhauls. No Damage History All Logs are Complete Since New Airframe. Internal baggage capacity is the amount of available baggage which can be stowed inside the aircraft where the… Structurally, they have weathered well over the years. The PIPER Cheyenne IIXL has a 4,387' balanced field length and 2,673' landing distance. This model, designated the PA-31T-620, was manufactured from 1974 to 1977. Deliveries of production Cheyenne IIIs began on June 30, 1980. It can hold 3,819 lb (1,732 kg) of fuel plus two passengers with baggage, while each extra passenger costs 100 nmi (190 km) of range. Total Time. The PA-42 Cheyenne III was announced in September 1977. The PIPER Cheyenne III has a 4,065' balanced field length and 3,065' landing distance. The PIPER Cheyenne IIXL, manufactured from 1981 - 1984, requires a 2 person crew and can transport up to 5 passengers. The PIPER Cheyenne III, manufactured from 1978 - 1983, requires a 2 person crew and can transport up to 6 passengers. All records are complete and there is no damage history. The Cheyenne has the capacity for 1-2 crew members and 6-9 passengers. Aircraft.com is the leading registry for planes, jets, and helicopters. [7], Due to its top speed over 400 mph, it was renamed the Cheyenne 400LS when Lear Siegler owned Piper, then the Cheyenne 400. Aircraft of comparable role, configuration, and era, Twin engine turboprop aircraft produced 1979-1993, "PA-42" redirects here. Piper; Cheyenne I PA-31T-500; 1981 Cheyenne I PA-31T-500 for Sale. The PA-42 Cheyenne is a larger development of the earlier PA-31T Cheyennes I and II (which are, in turn, turboprop developments of the PA-31 Navajo). Pressurization was increased to 7.6 psi (0.52 bar) to elevate its ceiling from 35,000 to 41,000 ft (10,700 to 12,500 m) while maintaining a 10,000 ft (3,000 m) cabin. The Piper PA-31T Cheyenne is a turboprop development of the earlier PA-31P Pressurized Navajo. The Piper Cheyenne IIXL Small Jet is manufactured by Piper between 1981 and 1984. This would be a great entry level turboprop for your business or growing family. The Cheyenne is the most economical cabin-class, twin-engine, turboprop on the market today. Piper Cheyenne. Other records later set by the 400LS, again piloted by Yeager in 400LS N4118Y (later reregistered as N46HL) for the C-1e Group 2 class, were: Miami-to-Boston, Miami-to-New York City, San Francisco-to-Charleston, West Virginia, San Francisco-to-Cincinnati, San Francisco-to-Los Angeles, New York City-to-Paris, Washington, DC-to-Paris and Gander-Paris. The aircraft has a maximum operating altitude of 35,000', a normal cruise speed of 275 KTS/316 MPH, and a 972 NM/1,119 SM seats-full range. It has a 98% dispatch reliability and its cabin is quieter than a King Air. Piper Cheyenne Series Questions Hi there, my boss wants to upgrade to a Piper Cheyenne IA, II or a IIXL from a Piper Seneca - I need opinions about the stability augmentation system of the II, reliability etc - and generell opinions from people who have flown one of these 'tuned navajos' :-) [7] The PA-42-1000 Cheyenne IV was certified in 1984, 44 were built until 1991 and 37 remain in service in 2018. In October of 2019, with four occupants, we traveled through Canada, Greenland, Iceland, Ireland, Italy … Originally, the aircraft was an upgraded version of the Pressurized Navajo equipped with two Pratt & Whitney Canada PT6A-28 turboprop engines. [7], The 400LS made aviation history on 16 April 1985 by setting two new time-to-climb records for its class (C-1e Group 2, 3000m and 9,000m) and shattering two time-to-climb records for all turboprop classes (6,000m and 12,000m): with retired United States Air Force Brigadier General Chuck Yeager at the helm of N400PS (with co-pilot Renald "Dav" Davenport flying right-seat), the aircraft departed from Portland-Hillsboro Airport's Runway 31L, immediately reached a 5,959-foot-per-minute climbout and achieved its 3,000m record in 1 minute, 47.6 seconds; the 6,000m record in 3 minutes, 42.0 seconds; its 9,000m record at 6 minutes, 34.6 seconds; the 12,000m record at 11 minutes, 8.3 seconds (time-to-altitude records were captured by on-board video camera aimed at relevant panel gauges, timed with superimposed timer; also verified by Hillsboro Airport tower personnel via radar, using encoded altimeter data transmitted from aircraft to tower via transponder). Design work on the Cheyenne began in 1965 as a turboprop-powered version of Piper’s Pressurized Navajo. Within our first year of ownership, my wife and I traveled to Bermuda, multiple Caribbean locations, and a 1,400-nm nonstop from Aspen, Colorado to Leesburg, Virginia. Its empennage was enlarged for stability at higher speeds and altitudes, and its fuselage was strengthened. The aircraft has a maximum operating altitude of 31,000', a normal cruise speed of 264 KTS/304 MPH, and a 749 NM/862 SM seats-full range. Interior: New refurbishing, 5 Pax Grey leather seats + 2 pilots seats. The 106 in (2.7 m) Dowty Rotol propellers had four round-tip composite blades and 8 in (20 cm) of ground clearance. Compare price and specifications of all Piper Cheyenne models in our listings. View all new & used Piper Cheyenne TurboProp aircraft for sale at ASO.com. Location: Georgia (USA) Serial Number: 8104028. 1980 Piper Cheyenne I Loading photos. PT-GLG . Share with Friend Loan Calculator Print Listing Proudly presented by Paradise Jet Brokers. Overview New to the market is this beautiful 1980 Cheyenne I. Airframe Notes. The first production Cheyenne III flew for the first time on May 18, 1979 and FAA certification was granted in early 1980. Internal baggage capacity is the amount of available baggage which can be stowed inside the aircraft where the… The PA-31T led to the development of the PA-42 Cheyenne III and IV. Piper’s Impressive Cheyenne III. The Piper Cheyenne 400LS, PA-42-1000, is the final development and improvement of the venerable Cheyenne line of twin turboprop business aircraft. The Cheyenne series of turboprop aircraft were manufactured by Piper Aircraft Company. Piper’s Impressive Cheyenne III By LeRoy Cook; July 22, 2016; Featured Plane; When Piper Aircraft announced its plans to build a big-cabin turboprop in late 1977, time was of the essence – only, we didn’t know it. Engine 1. [8][9][10], The 400LS has 100-hour inspection intervals, engine midlife inspections are due at 1,500 hours and overhauls come at 3,000 hours. The Navajo airframe was fitted out with 620-shaft-horsepower Pratt & Whitney PT6A-28 engines, given a pair of 30 gallon wing-tip fuel tanks, and certified in May 1972. Piper Cheyenne Series Aircraft Information Built by Piper Aircraft, the Piper Cheyenne is a turboprop powered aircraft. 1981 Cheyenne I PA-31T-500. The PA-31T, manufactured by Piper Aircraft, took its first flight on August 29, 1969. Price: $349,500 . [7], Flat rated to ISA+37, the turboprops maintain their power to almost 20,000 ft (6,100 m). Post Free 90-Day Ads that Display on Multiple Sites! Year: 1981 . There have been 1-014 Cheyenne-series airplanes built since first flight in May 1979- and 787 are still in operation today (according to JETNET records). Compared with the Cheyenne II, the PA-42-720 was about 1 m (3 ft) longer, was powered by 537 kW (720-shp) PT6A-41 turboprops and introduced a T-tail, the most obvious external difference between the PA-31T and PA-42, as well as the most significant change to the series. A23SO", Piper Aircraft News Release: Extended Range for Cheyenne IIIs (1980), Piper Aircraft News Release: Cheyenne III Deliveries Underway (1980), https://en.wikipedia.org/w/index.php?title=Piper_PA-42_Cheyenne&oldid=989981415, Short description is different from Wikidata, Creative Commons Attribution-ShareAlike License, This page was last edited on 22 November 2020, at 03:08. It can cruise at the same long-range speed over 1,842 nmi (3,411 km), 400 nmi (740 km) more; it can carry eight passengers farther than a King Air 200 while cruising 50 kn (93 km/h) faster. View photos, ownership, registration history, and more. The Cheyenne is the most economical cabin-class, twin-engine, turboprop on the market today. 1979 PIPER CHEYENNE 1 N2348W S/N 31T-7904057 1600 hrs Available on the Engines before TBO. A number of companies also use the aircraft as part of fractional ownership programs. This aircraft delivers the great performance at a lower cost when compared to other aircraft in its class. Here's a new catch from CZNL, a Piper PA-42-720 Cheyenne III C-GRDF seen on the approach and landing at CZNL in Nelson, British Columbia. Refinements to the Cheyenne I made in 1983, including more power at altitude, revised cowlings and interior, resulted in the Cheyenne IA. The PA-42 Cheyenne is a larger development of the earlier PA-31T Cheyennes I and II (which are, in turn, turboprop developments of the PA-31 Navajo). The fuselage is limited to a 15,000-hour life, while the wing and empennage have 20,000-hour life limits.[7]. Later, the aircraft was further refined and developed, including aerodynamic improvements and fuselage extensions. Piper introduced the lower powered (373kW/500shp PT6A-11s) and less expensive Cheyenne I in 1978, and renamed the original Cheyenne the Cheyenne II. Registration No: 38RE. Price: $349,500 . The aircraft is operated by private individuals, companies and executive charter operators. Passenger and baggage amounts can greatly effect the performance of an aircraft since minimum runway lengths, range and speed are all effected by its weight. Ads Now Automatically Display on: Scroll All Categories The PA-31T-500-I Cheyenne I seats up to 6 passengers plus 1 pilot. Typical passenger configuration is the typical number of passengers the jet is configured to accommodate 6 passengers, however each jet will have a custom configuration to accommodate an owners specific needs and will therefore vary. The Piper Cheyenne I--also known as the Piper PA-31T Cheyenne--was originally designed as an upgraded version of the Piper PA-31 Navajo. hello,I am stil looking for turbine plane for private use.I pik Piper Cheyenne now,there are in good price.Does anybody know what is mantinance cost like annual or 100h hours inspection?.What I should know before buy? It can operate out of 3,000 ft (900 m) runways with a 97 kn (180 km/h) minimum control speed, similar to a King Air 300; it can operate from much shorter hot and high runways than a Citation I and landing is shortened by the rotating speedbrake effect of the propellers in beta pitch. Two Pratt & Whitney PT6A-11 turboprop engines power the Piper Cheyenne I with 500 shp. The Piper PA-42 Cheyenne is a turboprop aircraft built by Piper Aircraft. It entered production in 1974. This aircraft delivers the great performance at a lower cost when compared to other aircraft in its class. [7], The aircraft's top speed is 351 kn (650 km/h; 404 mph) and was faster than the Citation I on most trips while burning one-third less fuel. Empty weight is 6837 lb (3101 kg) and maximum takeoff weight is 11,200 lb (5080 kg). Total Time: 9597 hrs. Twin engine turboprop aircraft with retractable landing gear. Paint and Interior are in good shape. Carolina Jet, Inc. is proud to offer N2519X for sale. It is derived directly from the Cheyenne III series, but utilizes the far more powerful TPE331 engines with four-blade propellers which produce significantly faster airspeeds than its predecessors. Data from Jane's All the World's Aircraft 1976–77 [3], Aircraft of comparable role, configuration, and era, Turboprop-powered series of the PA-31 light transport aircraft, The Piper PA-31T Cheyenne history from Airliners.net, https://en.wikipedia.org/w/index.php?title=Piper_PA-31T_Cheyenne&oldid=965225418, 1970s United States civil utility aircraft, Articles with unsourced statements from December 2014, Aircraft specs templates using more performance parameter, Creative Commons Attribution-ShareAlike License, PA-31T1 Cheyenne in landing configuration, This page was last edited on 30 June 2020, at 03:30. Piper: Model: Cheyenne III : Condition: Used Aircraft: Sale Type: For Sale: Currency: AU $ Price: $620,000 plus GST: Location: Australia: Year Built: 1981: Total Time Airframe: 8,685: Engine Specifications; PRATT & WHITNEY PT6A-41 720 HP. Jonathan Ranney Boynton Beach Florida (USA) 33437. 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When compared to other aircraft in its class manufactured by Piper aircraft and fuselage extensions % dispatch reliability its! Is 6837 lb ( 3101 kg ) and maximum takeoff weight is 6837 (.
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