The Piper PA-42 Cheyenne is a 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).
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]
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 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 400 mph, it was renamed the Cheyenne 400LS when Lear Siegler owned Piper, then the Cheyenne 400.[2]
Flat rated to ISA+37, the turboprops maintain their power to almost . The Dowty Rotol propellers had four round-tip composite blades and of ground clearance. Its empennage was enlarged for stability at higher speeds and altitudes, and its fuselage was strengthened. Pressurization was increased to to elevate its ceiling from while maintaining a cabin.[2]
The aircraft's top speed is and was faster than the Citation I on most trips while burning one-third less fuel. It can cruise at the same long-range speed over, more; it can carry eight passengers farther than a King Air 200 while cruising faster. It can operate out of runways with a 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.[2] It can climb directly to FL 410 at its MTOW and typical single-pilot BOWs are . It can hold of fuel plus two passengers with baggage, while each extra passenger costs of range. It has a 98% dispatch reliability and its cabin 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]
| Variant | III (PA-42)[8] | IIIA (PA-42-720) | 400 (PA-42-1000) | |
|---|---|---|---|---|
| Crew | 1-2 | |||
| Passengers | 6-9 | |||
| Length | 43ft 5in / 13.2m | |||
| Span | 47ft 8in / 14.5m | |||
| Height | 14ft 9in / 4.5m | 17ft 0in / 5.18m | ||
| Wing area | 293sq ft / 27.2 m2 | |||
| Cabin W × H | 4ft 3in by 4ft 8in / 1.30m by 1.42m | |||
| MTOW | 11,080lb / 5,026kg | |||
| OEW | 6,389lb / 2,898kg | |||
| Fuel Capacity | ||||
| 2× Turboprops | P&WC PT6A-41 | P&WC PT6A-61 | Garrett TPE331-14 | |
| Unit power | ||||
| Cruise | LR Max | LR Max | ||
| Range | 1,330 nmi / 2,463 km | |||
| BFL | ||||
| Ceiling[9] | ||||
| Climb rate | 2,380 ft/min / 12.1 m/s[10] | |||
| Wing loading | ||||
| power/mass | ||||
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.