Piper PA-47 PiperJet

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PA-47 PiperJet
Piper PA-47 Piper Jet N360PJ Lakeland FL 23.04.09R.jpg
The prototype PA-47 PiperJet at Lakeland, Florida, in April 2009
Role Very light jet
National origin United States
Manufacturer Piper Aircraft
First flight 30 July 2008[1]
Status Cancelled
Number built 1
Unit cost
$2.199M (in 2006 USD)

The Piper PA-47 PiperJet was a single-engined very light jet (VLJ) that was intended to be developed and built by Piper Aircraft. However, following a change of ownership at Piper, it was decided to redesign the aircraft into the PiperJet Altaire. Despite being technically successful, the Altaire project was cancelled in October 2011 due to economic conditions.

Design and development[edit]

PiperJet[edit]

The PiperJet was announced in October 2006, as a competitor to the twin-engined Eclipse 500 and Cessna Citation Mustang. The aircraft's fuselage was the same cross section as the propeller-driven Piper PA-46 series, with a 4 feet (1.2 m) increase in length.[2] It was to be capable of carrying up to 7 passengers and cruise at 360 knots (666.7 km/h), at a maximum altitude of 35,000 feet (10,668.0 m). Maximum range was expected to be 1,300 nautical miles (2,407.6 km), with a full-fuel payload of 800 pounds. Piper selected Williams International to supply its FJ44-3AP turbofan engine for the PiperJet.[3]

Due to the engine being mounted above the center of gravity, power was highly stabilizing (addition of power would push the nose down), which could have been disconcerting to pilots. Initially, Piper designers incorporated an automatic pitch trim system to coordinate horizontal stabilizer angle of incidence with power setting.[4] This system was later replaced by a vectored thrust nozzle, developed by Williams International, which resulted in reduced weight and simplified manufacturing processes.[5]

A design feature of the aircraft was the use of a straight duct air intake design for the vertical stabilizer (tail) mounted engine, similar in engineering design concept to a McDonnell Douglas DC-10, rather than the s-duct arrangement of most trijet aircraft designs such as the Dassault Falcon 900.[6]

A selling price of US$2.199 million in 2006 dollars was initially set and as of February 19, 2007, Piper announced that it had received 180 pre-orders. An entry-into-service date of early 2010 was initially anticipated, later changed to 2011-12. In October 2009 the company indicated that it had delayed the delivery of the first customer aircraft to mid-2013 and had informed depositors.[7][8]

The PiperJet did not enter production and in October 2010 Piper announced it would instead develop an aircraft with a larger circular-section fuselage known as the Piper PiperJet Altaire.[2][9] The 160 customers who had placed orders for the PiperJet retained their delivery positions with the new aircraft and at the same $2.2 million price.[9]

Altaire[edit]

Based on the PA-47 PiperJet prototype, the Altaire featured a slightly larger fuselage with a rounded cross-section, and included a conventional control yoke for flight control, as opposed to the original PiperJet's side-stick.[9]

Piper had been tooling up its facilities in Vero Beach, Florida (USA) to build four Altaire prototypes to be used for FAA (safety & performance) certification of the aircraft through 2013. First delivery of aircraft to customers was scheduled for 2014.[10] The first flight was expected in 2012.[9]

The fuselage of the original Piperjet was designed using the Piper Meridian single-engine turboprop as a template. The new owners of Piper, Imprimis, found fault with this design prompting a revision without direct reference to the Meridian. According to Piper CEO Geoffrey Berger, "We wanted to give our jet customers an even roomier light jet that incorporates a scalable design, paving the way for a future family of competitive business jets,".[10] The new fuselage design provided an additional 4 inches of headroom and nine more inches of elbow room and does away with a hump in the cabin floor that accommodated the wing spar in the old design.

The Altaire had been designed for single-pilot operation allowing one passenger to occupy the co-pilot's seat. Combined with 4 passenger seats in the cabin behind the flight deck, the jet would typically have seated 5 passengers. The cabin would have been specially configured to add an additional seat such that a total of 6 passengers can be accommodated in addition to the pilot. There was 20 cubic feet (570 L) of baggage space behind the passenger seats and another 20 cu ft (570 L). of heated but unpressurized space in the nose of the aircraft.

The Altaire would have been powered by the Williams International FJ44-3AP. This model of engine employs a "passive vectored thrust" design that helps compensate for nose-down pitch of the aircraft when power is increased as a result of mounting the engine relatively high up in the tail. Piper estimated that this engine would get the Altaire up to a 35,000 feet (11,000 m) maximum cruise altitude and a 320 knot cruise speed. Maximum cruise speed was projected to be 360 knots. The aircraft was expected to have a 1,200-to-1,300-nautical-mile (2,200 to 2,400 km) non-stop range.

The aircraft was expected to retail for around US$2.6 million, 'standard' equipped. Piper estimates variable operating cost at about US$730 per hour. This compares with about US$870 for the comparable model Cessna Mustang.

Cancellation[edit]

On 17 October 2011 the company announced that the PiperJet Altaire program was "under review". Piper's new interim CEO, appointed that same day, Simon Caldecott said, "This is being undertaken to ensure the company is properly aligning business goals and light-jet market forecasts with investment strategies and economic forecasts." The next day, on 18 October 2011, AVweb editor-in-chief Russ Niles called for the project to be ended, calling it "unrealistic" to pursue the design in the face of Federal Aviation Administration opposition to certifying a single engined jet to 35,000 ft (10,668 m) and the lack of economic reasoning as the aircraft would cost the same as most twin-engined jets. Niles called on Piper saying, "the sooner it ends its "review" of the project and puts a bullet in it the better."[11][12] On 24 October 2011, despite the Altaire's development being "on schedule and on budget", the program was indefinitely suspended by Piper due to economic issues, with the company laying off a number of workers who had been assigned to the project.[13] It was stated the company would entertain offers for the PiperJet/Altaire project.[14]

In 2012, the prototype was located at the Florida Air Museum.[15]

Specifications (original PA-47 PiperJet)[edit]

Data from Piper Aircraft[16][17]

General characteristics

  • Crew: 2
  • Capacity: 6-7 passengers
  • Length: 35 ft 8 in (10.87 m)
  • Wingspan: 44 ft 3 in (13.49 m)
  • Height: 15 ft 8 in (4.78 m)
  • Full fuel payload: intended to be 800 lbs (363 kg) +/-5%
  • Powerplant: 1 × Williams FJ44-3AP turbofan, 2,820 lbf (12.5 kN) thrust

Performance

  • Cruise speed: 360 kn (414 mph; 667 km/h) (intended maximum cruise speed +5% -2.5%)
  • Range: 1,300 nmi (1,496 mi; 2,408 km) (intended maximum range +/-5%)
  • Service ceiling: 35,000 ft (11,000 m)

Avionics

See also[edit]

Aircraft of comparable role, configuration and era

References[edit]

  1. ^ "PiperJet Makes First Flight" (Press release). Oshkosh, WI: Piper Aircraft. 30 July 2008. Archived from the original on 21 January 2009. Retrieved 30 July 2008. 
  2. ^ a b Marsh, Alton K. (18 October 2010). "Piper heavily revamps PiperJet". AOPA. Archived from the original on 23 October 2010. Retrieved 12 July 2011. 
  3. ^ "Piper Selects the Williams FJ44-3AP to Power the Revolutionary PiperJet" (Press release). Piper Aircraft. 9 November 2006. Archived from the original on 29 September 2007. Retrieved 29 April 2007. 
  4. ^ "PiperJet Flies". Airways. Flying. Vol. 135 no. 11. Hachette Filipacchi Media U.S. November 2008. p. 23. ISSN 0015-4806. Retrieved 19 August 2016 – via Google Books. 
  5. ^ Haines, Thomas B. (28 July 2009). "Nozzle mutes PiperJet pitch changes". AOPA. Archived from the original on 25 September 2009. Retrieved 17 August 2009. 
  6. ^ "The Aeronautical Journal". Royal Aeronautical Society. 1974, pp. 392, 398. Retrieved 2008-12-11
  7. ^ Business Aviation, February 19, 2007
  8. ^ Grady, Mary (28 October 2009). "Piper Pushes Jet Production To Mid-2013". AVweb. Retrieved 29 October 2009. 
  9. ^ a b c d Croft, John (19 October 2010). "Piper reinvents its personal jet with Altaire". Flightglobal. Retrieved 19 October 2010. 
  10. ^ a b Harrison, Kirby J. (18 October 2010). "New and improved PiperJet morphs into Piper Altaire". AINonline. Retrieved 20 October 2010. 
  11. ^ Grady, Mary (17 October 2011). "Another New CEO At Piper". AVweb. Retrieved 20 October 2011. 
  12. ^ Niles, Russ (18 October 2011). "Altaire A Dated Concept". AVweb. Retrieved 24 October 2011. 
  13. ^ Schneider, Mike; The Associated Press (October 24, 2011). "205 to lose jobs after Piper decides to mothball Altaire jet program". West Palm Beach, FL: WPTV Channel 5. Archived from the original on January 20, 2012. Retrieved 24 October 2011. 
  14. ^ Trautvetter, Chad (24 October 2011). "Piperjet Altaire Program Suspended 'Indefinitely'". AINonline. Retrieved 24 October 2011. 
  15. ^ Croft, John (5 April 2012). "Florida Air Museum is resting place for PiperJet". As the Cro(ft) Flies. Flightglobal. Archived from the original on 2 August 2012. Retrieved 16 July 2012. 
  16. ^ "Specifications". Piper Aircraft. n.d. Archived from the original on 2008-10-21. Retrieved 10 November 2009. 
  17. ^ "Piper selects garmin avionics for the piperjet". Piper Aircraft. September 2007. Archived from the original on 2008-10-21. Retrieved 15 November 2009. 

External links[edit]