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PiperJet Altaire the original Single Engine VLJ
The PiperJet Altaire was Piper Aircraft's ambitious entry into the very light jet (VLJ) market, designed to combine a single-engine turboprop's efficiency with a business jet's performance. Targeting a maximum cruise speed of 360 knots and a range of 1,300 nautical miles, the Altaire promised a spacious cabin for up to six passengers, advanced avionics, and competitive operating costs. Despite hitting technical milestones and securing over 150 pre-orders, the project was indefinitely suspended in 2011 due to rising development costs and weak market projections for light jets. Piper preserved the Altaire's intellectual property, leaving a legacy of innovation cut short by economic realities.
The PiperJet Altaire was developed as an innovative single-engine business jet, leveraging Piper Aircraft's expertise in single-engine turboprop design to create a cost-effective alternative to twin-engine competitors. With a projected price of $2.6 million, the Altaire aimed to offer a 1,300-nautical-mile range, a 360-knot cruise speed, and a 35,000-foot service ceiling, all powered by a Williams International FJ44-3AP turbofan engine. Its circular fuselage design provided a roomier cabin compared to earlier concepts, with 170 cubic feet of cabin space, 20 cubic feet of pressurized baggage, and optional configurations for a lavatory or seventh seat. However, after five years of development and $5.6 million in facility upgrades, Piper suspended the program in 2011, citing unsustainable costs amid stagnant demand for light jets.
The aircraft's design featured a natural-laminar-flow wing mounted low on the fuselage to maximize cabin space, with the wing spar positioned below the cabin floor to eliminate intrusions. The Williams FJ44-3AP engine, mounted high on the tail, utilized passive vectored thrust to counteract nose-down pitch during power changes, reducing reliance on complex trim systems.
The Altaire's cabin stood out for its ergonomic layout, offering 9 inches more headroom and 4 inches more elbow room than Piper's initial PA-46-based prototype. The interior included LED lighting, dual-zone climate control, and a modular lavatory option. Avionics were anchored by the Garmin G3000 suite, featuring touchscreen controls, synthetic vision, and advanced terrain awareness. Safety systems included an autoland capability, enhanced vision systems for low-visibility conditions, and a solid-state flight data recorder.
Despite these innovations, the Altaire faced skepticism from regulators and buyers. The FAA hesitated to certify single-engine jets for operations above 25,000 feet, undermining one of the aircraft's key selling points. Additionally, its $2.6 million price tag overlapped with twin-engine jets like the Cessna Citation Mustang, eroding its market appeal.
Piper's journey with the Altaire began in 2006 by announcing the original PiperJet, a PA-46-derived prototype. By 2008, the company had 200 pre-orders and a flying prototype, but financial constraints prompted a redesign. 2010 the Altaire emerged with a larger, circular fuselage, improved aerodynamics, and the FJ44-3AP engine. Key milestones included:
- 2006: Program launch at NBAA; Williams FJ44 engine selected.
- 2008: First flight of the original PiperJet prototype.
- 2010: Altaire redesign unveiled with enhanced cabin and systems.
- 2011: Structural testing began, but the program was suspended in October due to economic forecasts.
By 2011, Piper had invested heavily in production infrastructure, including new Vero Beach, Florida manufacturing facilities. However, with light jet deliveries projected to remain below 100 annually through 2015, the company concluded it could not recoup development costs, leading to layoffs of 150 employees and refunds for depositors.
Main Competitors
The very light jet (VLJ) market of the late 2000s was marked by fierce competition among established manufacturers and ambitious startups. While Altaire aimed to carve its niche with a single-engine design, it faced formidable rivals that offered diverse approaches to the VLJ segment.
Cessna Citation Mustang Strengths: Twin-engine reliability established service network. Weaknesses: Higher acquisition ($3.2M) and operating costs ($870/hour). | ![]() |
![]() | Eclipse 500 Strengths: Fastest cruise speed (370 knots) in class. Weaknesses: Early models were plagued by engine failures and limited cabin space. |
Adam A700 Design: Twin Williams FJ33 engines, carbon-fiber airframe, modular 6–8 seat cabin. Performance: 1,400 nm range, 340-knot cruise, 41,000-foot ceiling. Fate: Adam Aircraft filed for bankruptcy in 2008 despite Russian investment interests. | ![]() |
![]() | Cirrus Vision SF50 Post-Altaire Entry: Certified in 2016, proving single-engine VLJ viability with 1,200 nm range. |
Comparative Analysis
Specification | PiperJet Altaire | Cessna Citation Mustang | Eclipse 500 | Adam A700 |
Engines | 1 × FJ44-3AP | 2 × PW615F | 2 × PW610F | 2 × FJ33-4 |
Max Cruise Speed | 360 knots | 340 knots | 370 knots | 340 knots |
Range | 1,300 nm | 1,150 nm | 1,125 nm | 1,400 nm |
Cabin Volume | 170 cu ft | 140 cu ft | 120 cu ft | 165 cu ft |
Base Price | $2.6M | $3.2M | $2.7M | $2.5M |
Operating Cost/Hour | $730 | $870 | $850 | $800 |
Legacy and Lessons
The Altaire, Eclipse 500 and Adam A700 shared a common fate: they fell victim to the 2008 economic downturn and FAA certification hurdles. However, their innovations influenced later aircraft:
- Single-Engine Certification: The Altaire’s HALO framework discussions paved the way for the Cirrus Vision SF50’s 2016 certification.
- Composite Construction: Adam’s carbon-fiber techniques were adopted by startups like Stratos Aircraft.
Piper’s decision to preserve Altaire’s IP suggests potential future interest in single-engine jets, particularly as sustainable aviation fuels reduce engine redundancy requirements.
PiperJet Altaire Detailed Specifications
Country: United States
PERFORMANCE AND CAPACITY
Propulsion Type: Turbofan
Engine: Williams FJ44-3AP (2,500 lbf thrust)
Max Range: 1,300 nm
Max Speed: 360 knots
Service Ceiling: 35,000 ft (projected)
Passenger Capacity: 6
Max Takeoff Weight: 10,500 lbs
AIRCRAFT DESIGN
- Length: 37.6 ft
- Wingspan: 44.5 ft
- Cabin Dimensions: 12.5 ft (L) × 5.0 ft (W) × 4.8 ft (H)