Piper PA-42 Cheyenne

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The Piper PA-42 Cheyenne is a twin engine turboprop aircraft built by Piper Aircraft. 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).

History

File:Lh-cheyenne.jpg
Lufthansa Cheyenne III with a T-tail

Cheyenne III

File:Piper PA-42-720 Cheyenne IIIA, Alitalia Flying School AN0989651.jpg
Alitalia Cheyenne IIIA with PT6 side exhausts

The PA-42 Cheyenne III was announced in September 1977. The first production Cheyenne III flew for the first time on May 18, 1979, and FAA certification was granted in early 1980. 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. Deliveries of production Cheyenne IIIs began on June 30, 1980.[1]

Cheyenne 400

File:Piper PA-42-1000 Cheyenne 400LS Private, LUX Luxembourg (Findel), Luxembourg PP1238521046.jpg
Cheyenne 400 with TPE331 rear exhaust

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 Template:Cvt Honeywell TPE331-14s.[2] The PA-42-1000 Cheyenne IV was certified in 1984, 43 were built until 1991 and 37 remain in service in 2018.[2]

Due to its top speed over Template:Cvt it was renamed the Cheyenne 400LS when Lear Siegler owned Piper, then the Cheyenne 400.[2]

Flat rated to ISA+37, the turboprops maintains its power to almost Template:Cvt. The Template:Cvt Dowty Rotol propellers have four round-tip composite blades and Template:Cvt of ground clearance. Its empennage was enlarged for stability at higher speeds and altitudes, and its fuselage was strengthened. Pressurization was increased to Template:Cvt to elevate its ceiling from Template:Cvt while maintaining a Template:Cvt cabin.[2]

The aircraft's top speed is Template:Cvt, faster than the Citation I on most trips while burning one-third less fuel. It can cruise at the same long-range speed over Template:Cvt, Template:Cvt more; it can carry eight passengers farther than a King Air 200 while cruising Template:Cvt faster. It can operate out of Template:Cvt runways with a Template:Cvt 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 distance is shortened by the rotating speedbrake effect of the propellers in beta pitch.[2] It can climb directly to FL 410 at its Template:Cvt MTOW and typical single-pilot BOWs are Template:Cvt. It can hold Template:Cvt of fuel plus two passengers with baggage, while each extra passenger costs Template:Cvt of range. It has a 98% dispatch reliability and a cabin that is quieter than a King Air.[2]

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). 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.[3][4][5]

The 400LS has 100-hour inspection intervals, engine midlife inspections are due at 1,500 hours and overhauls come at 3,000 hours. The fuselage is limited to a 15,000-hour life, while the wing and empennage have 20,000-hour life limits.[2]

Variants

  • Cheyenne III, model PA-42, equipped with Pratt & Whitney Canada PT6-41 engines
  • Cheyenne IIIA, model PA-42-720, equipped with PT6A-61 engines.[6]
  • Cheyenne IV, model PA-42-1000, later the Cheyenne 400LS, and then Cheyenne 400. This is the largest aircraft ever made by Piper, with 43 built. Powered by Template:Convert Garrett TPE-331 engines, and four-blade props.[7]
  • Customs High Endurance Tracker (CHET), special surveillance version of the Cheyenne III, fitted with an AN/APG-66 radar and a ventral FLIR; nine built for the U.S. Customs Service.

Specifications

File:Piper PA-42 Cheyenne III AN1190193.jpg
flight deck
Corporate aircraft directory[8]
Variant III (PA-42)[9] IIIA (PA-42-720) 400 (PA-42-1000)
Crew 1–2
Passengers[7] 6–9
Length 43ft 5in / 13.2m
Span 47ft 8in / 14.5m
Height 14ft 9in / 4.5m 17ft 0in / 5.18m [7]
Wing area 293sq ft / 27.2 m2[7]
Cabin W × H 4ft 3in by 4ft 8in / 1.30m by 1.42m
MTOW 11,080lb / 5,026kg Template:Cvt Template:Cvt
OEW 6,389lb / 2,898kg Template:Cvt Template:Cvt
Fuel Capacity[6] Template:Cvt
Template:Cvt
Template:Cvt
Template:Cvt
2× Turboprops P&WC PT6A-41 P&WC PT6A-61 Garrett TPE331-14
Unit power Template:Cvt Template:Cvt
Cruise Template:Cvt LR Template:Cvt Max LR Template:Cvt Max
Range 1,330 nmi / 2,463 km Template:Cvt Template:Cvt
BFL Template:Cvt Template:Cvt Template:Cvt
Ceiling[6] Template:Cvt Template:Cvt Template:Cvt
Climb rate[7] 2,380 ft/min / 12.1 m/s[10] Template:Cvt Template:Cvt
Wing loading Template:Cvt Template:Cvt Template:Cvt
power/mass Template:Cvt Template:Cvt Template:Cvt

Operators

The aircraft is operated by private individuals, companies and executive charter operators. A number of companies also use the aircraft as part of fractional ownership programs.

See also

Related development

Aircraft of comparable role, configuration, and era

References

Template:Reflist

External links

Template:Sister project

Template:Piper

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