AIRCRAFT LEARNING CENTER
Eclipse 500 and 550
ECLIPSE 500 and 550
Exterior Dimensions
Side View
Top Down View
Front View
Exterior Dimensions | |
---|---|
Overall Length | 33ft 5in |
Overall Height | 11ft 0in |
Wingspan | 37ft 11in |
Horizontal Tail Span | 13ft 6in |
Nose to Trailing Edge (T-Hangar Constrain) | 18ft 0in |
Landing Gear Base (Nose to Main) | 14ft 0in |
Landing Gear Tread (Main to Main) | 10ft 11in |
Interior Dimensions
Cross Section View
Six Seat Configuration
Five Seat Configuration
Four Seat Configuration
Internal Dimensions | |
---|---|
Cabin Width | 4ft 8in |
Cabin Length | 12ft 4in |
Cabin Height | 4ft 2in |
Entry Width | 1ft 11.5in |
Entry Height | 3ft 11in |
Total Baggage Volume | 16ft3 |
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16ft3 |
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N/A |
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N/A |
Design Weights and Capacities
Design Weights | Capacity |
---|---|
Maximum Ramp Weight | 6,034 lbs |
Maximum Takeoff Weight | 6,000 lbs |
Maximum Landing Weight | 5,600 lbs |
Maximum Zero Fuel Weight | 4,922 lbs |
Basic Empty Weight | 3,634 lbs |
Maximum Payload (No Pilot) | 1,288 lbs |
Useful Load (No Pilot) | 2,400 lbs |
Fuel Capacity (useable) at 6.70 lb/gal | 1,698 lbs |
Useful Load w/full fuel (No Pilot) | 702 lbs |
Performance
Performance | |
---|---|
Takeoff Runway Length (Max. Takeoff Weight, Paved, Sea Level, ISA, Part 23 Normal Category, over a 50 foot obstacle) | 2,394 ft |
Maximum Altitude | 41,000 ft |
Maximum Cruise Speed (Mid-Cruise Weight, 33,000 ft, ISA) | 370 KTAS |
NBAA IFR Range (100 nm alternate)(Max. Takeoff Weight, Optimal Climb & Descent, Max. Cruise Thrust at 41,000 feet) | 1,125 nm |
Landing Runway Length (Max. Â Landing Weight, Paved, Sea Level, ISA, per Part 23 Normal Category, from a 50 foot obstacle) | 2,790 ft |
Structural Design Limitations
Limit Speeds | |
---|---|
VMO | 285 KEAS |
MMO | Mach 0.64 |
Flap Extension Speeds | |
---|---|
VFE 0° to Takeoff/Approach Extension | 200 KEAS |
VFE Takeoff/Approach to Landing Extension | 140 KEAS |
Landing Gear Operating and Extended Speeds | |
---|---|
VLO (retracting) | 200 KEAS |
VLO (extending) | 200 KEAS |
VLE | 285 KEAS |
Buyer/Seller Resources
Buyer’s Guide & FAQ
As the global leader in Eclipse 500 sales, AEROCOR has learned a thing or two about the Eclipse fleet. We know how hard it is to find up to date information on the Eclipse and so we’ve created a one of a kind buyer’s guide to answer all of the most frequently asked questions that we get from prospective owners. It includes detailed technical comparisons, information on the purchase process, and describes what to expect when owning and operating your first turbine aircraft. The AEROCOR Eclipse 500 buyers’s guide is by far our most requested and positively reviewed publication.
2023 Q1 Market Update
AEROCOR maintains the most comprehensive Eclipse 500 specific database in the world. It contains the exact configuration and transaction history of every aircraft in the fleet. We track important data on every sale and can provide inventory levels by day dating back to 2014. This information is provided to our customers in real time to make informed purchase/sales decisions. The Eclipse Market report is a bi-annual publication which provides a summary of recent sales data and analysis on how it relates to past and future activity. If you are thinking about buying or selling an Eclipse the Market Report is a must read.
History and General Description
Conceived in the late 1990’s, the Eclipse 500 introduced an altogether new category of aircraft known as the VLJ or Very Light Jet. While the jet boasted some impressive performance figures (including a 370 knot cruise and a maximum operating altitude of 41,000 feet), it was the first multi-engine jet to also claim high levels of efficiency and affordability, bringing turbine class aircraft within reach of a much wider range of buyers.
Beyond performance, the Eclipse 500 also introduced several new technologies to the general aviation market. The aircraft is equipped with an impressive “glass cockpit” system from Innovative Solutions & Support (IS&S) known as Avio NG. The system includes a wide range of features normally reserved for larger aircraft, such as full synoptic displays of all aircraft systems as well as an auto-throttle system.
The aircraft was also the first to implement many innovative manufacturing techniques, becoming the first aircraft to utilize friction stir welding during construction of the major fuselage components. A somewhat new process at the time, friction stir welding allowed the Eclipse to be built to more demanding tolerances and achieve an overall lighter weight than what would have been possible from traditional manufacturing techniques. This same process has since been utilized by several modern space vehicles, such as the SpaceX Falcon 9 orbital class rocket.
The Eclipse 500 and its derivatives (The Eclipse 550, Total Eclipse, and Eclipse Special Edition) are often compared along side other turbine aircraft within the same category. This includes other jet aircraft, such as the Cessna Citation Mustang and Embraer Phenom 100, as well as high performance turbo-prop aircraft, such as the Socata TBM and the Piper Malibu Meridian.
By offering such a well balanced blend of performance, affordability, and ease of use, the Eclipse has become one of the most sought after aircraft among “owner-operators.”
Final Thoughts
Designed to integrate cutting edge technologies as the world’s first Very Light Jet (VLJ), the Eclipse 500 is unlike any other aircraft flying. With cruise speeds up to 370 knots and an operational ceiling of 41,000 feet, the Eclipse 500 offers truly extreme performance. Perhaps equally impressive, however, is the fuel sipping economy. With fuel burns of less than 70 gallons per hour, the Eclipse 500 costs less to operate per mile than nearly any other jet or turbo-prop available today (including smaller single-engine turbo-prop aircraft).
Extreme performance, extreme economy, and extremely fun to fly. It’s time to treat yourself to everything the Eclipse 500 has to offer!
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