Velocity Edge GX570 Bedienungsanleitung PDF herunterladen (Seite 8)

August 2011, Preliminary

2. PERFORMANCE

1. GENERAL DESCRIPTION (Continued)

1.3 Design Weights and Capacities

Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,800 lb (4,899 kg)

Maximum Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,700 lb (4,853 kg)

Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9,900 lb (4,491 kg)

Maximum Zero Fuel Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,400 lb (3,810 kg)

Standard Empty Weight * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,773 lb (3,072 kg)

Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4,009 lb (1,818 kg)

Fuel Capacity (useable) at 6.70 lb/gal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,309 lb (1,501 kg)

* Standard empty weight includes unusable fuel, full oil, standard interior, and standard avionics.

Takeoff Runway Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,250 ft (991 m)

(Maximum Takeoff Weight, Sea Level, ISA,

Balanced Field Length per Part 25, 15° Flaps)

Climb Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 min to 41,000 ft (12,497 m)

(Maximum Takeoff Weight, Sea Level, ISA)

Maximum Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41,000 ft (12,497 m)

Maximum Cruise Speed (±3%) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 400 KTAS (741 km/hr, 460 mph)

(Mid-Cruise Weight, 31,000 ft (9,449 m), ISA)

NBAA IFR Range (100 nm alternate) (± 4%) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,300 nm (2,408 km, 1,496 mi)

(Maximum Takeoff Weight, Full Fuel, Optimal Climb

and Descent, Maximum Cruise Thrust at 41,000 feet)

Landing Runway Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2,590 ft (789 m)

(Maximum Landing Weight, Sea Level, ISA, per Part 25)

Certificated Noise Levels

Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73.5 EPNdB

Sideline . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85.2 EPNdB

Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88.5 EPNdB

All performance data is based on a standard aircraft con-

figuration, operating in International Standard Atmosphere

conditions with zero wind. Takeoff and landing field

lengths are based on a level, hard surface, dry runway.

Actual performance will vary with individual airplanes and

other factors such as environmental conditions, aircraft

configuration, and operational/ATC procedures.

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