Charter flights, About Air Charters. flight details

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Charter flight, Charter flights Aviation The Wings of our fly

What is charter flight?What is charter flight? How to chose charter flight, charter flights aviation  providing the all the information of the crafts , seating capacity, cursing speed of the craft, and engine  , Cheap charter flights, charter air flights, charter flight, charter travel,  to all the question select your craft on your  choice, You would need to view the entire charter fleet together, or else you would never know the range of choices you could have. The exact kind of charter aircraft that would be appropriate for your trip is decided by a number of factors like:
• The no. of passengers traveling with you  • The amount and nature of cargo/baggage • Your budget • The destination • Your aircraft preferences

King Air C90GTi

King Air 100
Role Civil utility aircraft

King Air C90GTi Specifications Crew: 1-2, Capacity: 7 passengers maximum, depending on cabin configuration, Length: 35 ft 6 in (10.82 m) , Wingspan: 50 ft 3 in (15.32 m), Height: 14 ft 3 in (4.34 m), Wing area: 294 ft² (27 m²), Empty weight: 6,950 lb (3,150 kg), Max. takeoff weight: 10,100 lb (4,580 kg), Power plant: 2 × Pratt & Whitney Canada PT6A 135A turboprops, driving Hartzell HC-E4N-3N propellers, 550 shp (410 kW) each, Performance detail
Maximum speed: 311 mph TAS (270 knots TAS, 500 km/h TAS)
Cruise speed: 260 mph TAS (226 kts TAS, 416 km/h TAS), Stall speed: 90 mph (78 knots, 145 km/h) IAS (flaps down) Range: 1,530 miles (1,321 nm, 2,446 km)
Service ceiling: 30,000ft (9,144 m), Rate of climb: 2,000 ft/min (10.2 m/s), Wing loading: 34.3 lb/ft² (170 kg/m²), Power/mass: 0.099 hp/lb (179 W/kg)

PLATUS PC -12

Pilatus PC-12 Passenger and cargo aircraft

Pilatus PC-12 NG General characteristics
Crew: one or two pilots Capacity: 9 passenger’s standard, 6-8 executive, Payload: 1,500 kg (3,502 lb), Length: 14.40 m (47 ft 3 in). Wingspan: 16.23 m (53 ft 3 in), Height: 4.26 m (14 ft 0 in), Wing area: 25.81 m² (277.8 ft²), Empty weight: 2,761 kg (5,867 lb), Loaded weight: 4,700 kg (10,450 lb), Max. takeoff weight: 4,740 kg (10,450 lb), Powerplant: 1 × Pratt & Whitney Canada PT6A-67P turboprop, 895 kW (1,200 shp), Maximum landing: 4,700 kg (10,450 lb), Maximum payload full fuel: 539 kg (1,189 lb), Tail wingspan: 5.20 m (17 ft 1 in), Propeller: Hartzell HC - E4A - 3D/E10477K – 4 blade aluminum , Propeller diameter: 2.67 m (8 ft 9 in), Propeller RPM: 1,700 rpm
Performance
 Cruise speed: 500 km/h (312.5 mph/270 KTAS/280 KTAS @ 20000 ft (PC-12NG)) Stall speed: 120 km/h (74.8 mph/ 65 KCAS/66 KCAS (PC-12NG)) Service ceiling: 9,150 m (30,000 ft) Rate of climb: 512 m/min at sea level (1,680 ft/min) Wing loading: 174.3 kg/m² (35.7 lb/ft²) Power/mass: 3.7 kg/shp (8.2 lb/shp)  Range 0 passenger: 4,149 km (2,593 mi) (2,239 nm Range 9 passenger: 2,804 km (1,753 mi) (1,513 nm) Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft) Takeoff distance ground roll: 450 m (1,475 ft) Landing distance over 15 m (50 ft) obstacle: 558 m (1,830 ft) Landing distance ground roll: 228 m (945 ft) Avionics Honeywell Primus APEX (PC-12

King Air B200

Beechcraft B200 King Air
Role Civil utility aircraft
Manufacturer Beechcraft

King Air B200 General characteristics
 Crew: 1–2  Capacity: 13 passengers  Length: 43 ft 9 in (13.34 m) Wingspan: 54 ft 6 in (16.61 m)  Height: 15 ft 0 in (4.57 m)  Wing area: 303 ft² (28.2 m²)  Empty weight: 7,755 lb (3,520 kg)  Max. takeoff weight: 12,500 lb (5,670 kg) Powerplant: 2 × Pratt & Whitney Canada PT6A-42 turboprops, 850 shp (635kW) each
Performance
 Maximum speed: 339 mph (294 knots, 545 km/h) at 25,000 ft (7,600m)
 Cruise speed: 333 mph (289 knots, 536 km/h) at 25,000 ft (7,620 m) (max cruise)
 Stall speed: 86 mph (75 knots, 139 km/h) IAS (flaps down)
 Range: 2,075 mi (1,800 nm, 3,338 km) with maximum fuel and 45 minute reserve Service ceiling: 35,000 ft (10,700 m) Rate of climb: 2,450 ft/min (12.5 m/s) Wing loading: 41.3 lb/ft² (201.6 kg/m²)  Power/mass: 0.14 hp/lb (220 W/kg)

Gulf stream 200

Gulfstream G200
Role Business jet
Manufacturer Gulfstream Aerospace

Gulfstream G200 data General characteristics
 Crew: 2
 Capacity: seating for 8 or more in executive-style, or up to 18 as a corporate shuttle
 Payload: 4,050 lb (1,840 kg) Length: 62 ft 3 in (18.97 m)  Wingspan: 58 ft 1 in (17.70 m)  Height: 21 ft 5 in (6.53 m)  Wing area: 369 ft² (34.3 m²)  Empty weight: 19,200 lb (8,709 kg)  Max. takeoff weight: 35,450 lb (16,080 kg) Powerplant: 2 × Pratt & Whitney Canada PW-306A turbofans, 6,040 lbf (26.9 kN) each
Performance Maximum speed: Mach 0.85 (487 knots, 560 mph, 900 km/h) at altitude Cruise speed: Mach 0.80 (459 knots, 528 mph, 850 km/h) normal cruise at altitude
 Range: 3,400 nmi (3,910 mi, 6,300 km) at Mach 0.75 with 4 passengers
 Service ceiling: 45,000 ft (13,700 m)

Citation CJ2

A Cessna 525 CitationJet
Role Business Jet

Hawker 850 XP

Raytheon Hawker 800XP of NetJets Europe
Role Mid-size business jet

Specifications Hawker 850XP

General characteristics
Crew: 2 pilots
Capacity: 8 passengers typical, 13 maximum
Length: 51 ft 2 in (15.6 m) Wingspan: 54 ft 4 in (16.5 m) Height: 18 ft 1 in (5.5 m)
Empty weight: 15,670 lb (7,108 kg)
Max. takeoff weight: 28,000 lb (12,701 kg)
Powerplant: 2 × Honeywell TFE731-5BR turbofan, 4660 lbf () each
Performance
Maximum speed: 448 kts (514 mph) 830 km/h
Cruise speed: 402 kts (463 mph) 745 km/h
Range: 2,642 nm (4,893 km)
Service ceiling: 41,000 ft (12,497 m)

Global XRS

A Global Express
Role Business jet
Bombardier Global Express

Global Express XRS Specifications
General characteristics
 Crew: Two (minimum) - four (typical)
 Capacity: 8-19 passengers
 Length: 99 ft 5 in (30.3 m) Wingspan: 94 ft 0 in (28.65 m) Height: 24 ft 10 in (7.57 m)  Wing area: 1,022 ft² (94.9 m²)  Empty weight: 49,750 lb (22,600 kg)  Useful load: 1,775 lb w/full fuel (805 kg)  Max. takeoff weight: 99,500 lb (44,500 kg)
 Powerplant: 2 × Rolls-Royce Deutschland BR710A2-20 turbofans, 14,750 lbf (65.5 kN) each  Cabin length: 48 ft 4 in (14.73 m)  Cabin max width (centerline): 8 ft 2 in (2.49 m)  Cabin max width (floorline): 6 ft 11 in (2.11 m)  Cabin height: 6 ft 3 in (1.91 m)  Cabin floor area: 335 ft² (31.1 m²)
Performance
 Maximum speed: Mach .89 (513 kt, 590 mph, 950 km/h)  Cruise speed: Mach .85 (488 kt, 564 mph, 907 km/h)  Range: 6,325 nm (7,080 mi, 11,390 km)  Service ceiling: 51,000 ft (15,500 m)  Wing loading: 95.9 lb/ft² (468 kg/m²)  Thrust/weight: 0.301  Balanced field length (SL, ISA, MGTOW): 6,120 ft (1,870 m) Landing distance (SL, ISA, MLW): 2,670 ft (814 m)

Boeing 727 VIP

Manufacturer BOEING
Model 727-200 SUPER27

Boeing BBJ

Boeing Business Jet
Role Business jet
Manufacturer Boeing Commercial Airplanes

Cessna 208 Caravan

Cessna 208 Caravan

A 2004 Cessna 208B
Role Light transport turboprop
Manufacturer Cessna

Cessna 208 Caravan Specifications

General characteristics
Crew: one
Capacity: nine passengers or 14 with FAR Part 23 waiver
Length: 12.67 m (41 ft 7 in)
Wingspan: 15.88 m (52 ft 1 in)
Height: 4.32 m (14 ft 2 in) Wing area: 26.0 m2 (280 sq ft) Empty weight: 2,073 kg (4,570 lb) Gross weight: 3,970 kg (8,752 lb) Powerplant: 1 × Pratt & Whitney PT6A-114A , 505 kW (677 hp)Propellers: 3-bladed Hartzell variable pitch
Performance
Cruising speed: 317 km/h (197 mph; 171 kn)
Range: 2,000 km (1,243 mi; 1,080 nmi) with max fuel and reserves
Rate of climb: 3.9 m/s (770 ft/min)

Challenger 300

Bombardier Challenger 300
Role Business jet
Manufacturer Bombardier Aerospace

Challenger 604

Bombardier CL-604,
Role Business jet
Manufacturer Bombardier Aerospace

Specifications (CL-601-3A)
General characteristics
 Crew: Two (pilot & co-pilot)
 Capacity: Up to 19 passengers, depending on configuration
 Length: 20.85 m (68 ft 5 in)
 Wingspan: 19.61 m (64 ft 4 in)  Height: 6.30 m (20 ft 8 in)  Wing area: 48.3 m² (520 ft²) Empty weight: 9,292 kg (20,485 lb) Loaded weight: 19,618 kg (43,250 lb)
 Useful load: 1,814 kg (4,000 lb) Max. takeoff weight: 19,550 kg (43,100 lb)
 Powerplant: 2 × General Electric CF34-3A turbofans, 40.7 kN (9,140 lbf) each
Performance
 Maximum speed: 882 km/h (476 knots, 548 mph)
 Cruise speed: 851 km/h, (459 knots, 529 mph)
 Range: 6,236 km (3,366 nm, 3,875 mi)
 Service ceiling: 12,500 m (41,000 ft)
 Rate of climb: 1,355 m/min (4,450 ft/min)

Challenger 605

Challenger 600/601/604/605
Bombardier CL-604,
Role Business jet
Manufacturer Bombardier Aerospace

General characteristics
 Crew: Two (pilot & co-pilot)
 Capacity: Up to 19 passengers, depending on configuration
 Length: 20.85 m (68 ft 5 in) Wingspan: 19.61 m (64 ft 4 in) Height: 6.30 m (20 ft 8 in) Wing area: 48.3 m² (520 ft²) Empty weight: 9,292 kg (20,485 lb) Loaded weight: 19,618 kg (43,250 lb) Useful load: 1,814 kg (4,000 lb)  Max. takeoff weight: 19,550 kg (43,100 lb) Powerplant: 2 × General Electric CF34-3A turbofans, 40.7 kN (9,140 lbf) each
Performance
 Maximum speed: 882 km/h (476 knots, 548 mph) Cruise speed: 851 km/h, (459 knots, 529 mph) Range: 6,236 km (3,366 nm, 3,875 mi) Service ceiling: 12,500 m (41,000 ft) Rate of climb: 1,355 m/min (4,450 ft/min)

Citation Bravo Cessna S550

Cessna S550 Citation SI

Citation CJ2

CitationJet/ CJ series
A Cessna 525 CitationJet
Role Business Jet

Specifications (Citation CJ1+)
General characteristics
 Crew: 1
 Capacity: 3-9 passengers
 Payload: 615 lb (279 kg) Length: 42 ft 7 in (12.98 m) Wingspan: 46 ft 11 in (14.30 m)  Height: (4.19 m) Empty weight: 6,765 lb (3,069 kg) Useful load: 3,835 lb (1,740 kg) Max. takeoff weight: 10,700 lb (4,853 kg) Powerplant: 2 × Williams FJ44-1AP turbofan, 1,965 lb (8.74 kN) each
Performance
 Cruise speed: 389 ktas (720 km/h)
 Stall speed: 83 kcas (153 km/h)  Range: 1,300 nm (2,408 km) Service ceiling: 41,000 ft (12,497 m)  Rate of climb: 3,290 ft/min (1,003 m/min)

Citation Sovereign

Citation Sovereign

Role Business jet
Manufacturer Cessna

Specifications (Citation Sovereign)
General characteristics
 Crew: 2
 Capacity: 8-12 passengers
 Payload: 2,680 lb (1,216 kg) Length: 63 ft 6 in (19.37 m) Wingspan: 63 ft 1 in (19.24 m) Height: 20 ft 4 in (6.2 m) Empty weight: 17,700 lb (8,029 kg) Useful load: 12,430 lb (5,638 kg) Max. takeoff weight: 30,300 lb (13,743 kg) Powerplant: 2 × Pratt & Whitney Canada PW306C turbofans
Performance
 Never exceed speed: Mach .8 Maximum speed: 458 knots (848 km/h) Range: 2,847 nm (5,273 km) Service ceiling: 47,000 ft (14,326 m) Rate of climb: 4,016 ft/min ()

Citation XLS

Citation Excel
Citation XLS / Citation XLS+

Cessna 560XL Citation Excel of the Swiss Air Force
Role Business jet
Manufacturer Cessna

Specifications (Citation XLS+)
Data from Cessna Citation XLS+ web site [5]
General characteristics
 Crew: 2
 Capacity: 7-10 passengers
 Length: 52 ft 6 in (16.0 m)
 Wingspan: 56 ft 4 in (17.17 m) Height: 17 ft 2 in (5.23 m) Empty weight: 12,800 lb (5,086 kg) Useful load: 7,400 lb (4,077 kg) Max. takeoff weight: 20,200 lb (9,163 kg) Powerplant: 2 × Pratt & Whitney Canada PW545C turbofans, 4,119 lb (18.32 kN) each
Performance
 Cruise speed: 441 ktas (815 km/h) Range: 1,858 nm (3,441 km) Service ceiling: 45,000 ft (13,716 m) Rate of climb: 3,500 ft/min (1,067 m/min)

Dornier 328 JET

Dornier 328

An Air Alps Dornier 328-110 landing at Fiumicino Airport, Rome
Role Airliner
Manufacturer Dornier,
Fairchild-Dornier

Specifications (Dornier 328-110)
General characteristics
 Crew: Three (2 Pilots, 1 Flight Attendant)
 Capacity: 30 to 33 (14 in First Class Config) passengers
 Length: 21.11 m (69 ft 7 in) Wingspan: 20.98 m (68 ft 10 in) Height: 7.24 m (23 ft 9 in) Wing area: 40 m² (431 ft²) Empty weight: 8,920 kg (19,670 lb)
 Useful load: 3,450 kg (7,606 lb)
 Max. takeoff weight: 13,990 kg (30,840 lb)
Performance
 Maximum speed: 620 km/h (335 knots, 385 mph)
 Range: 1,850 km (1,000 nm, 1,150 mi)
 Service ceiling: 9,455 m (31,020 ft)
Avionics Honeywell PRIMUS 2000

Embraer Legacy 600

An Embraer Legacy 600
Role Business jet
Manufacturer Embraer

General characteristics
 Crew: Three - pilot, co-pilot, flight attendant (optional)
 Capacity: 13 passengers + 1 in cockpit jumpseat
 Length: 26.33 m (86 ft 5 in) Wingspan: 21.17 m (68 ft 11 in)
 Height: 6.76 m (22 ft 2 in) Empty weight: 16,000 kg (30,000 lb)
 Max. takeoff weight: 22,500 kg (49,604 lb)
 Powerplant: 2 × Rolls-Royce AE 3007/A1P turbofans, 39,2 kN (8,810 lbs) each
Performance
 Maximum speed: 834 km/h (450 kt, 518 mph) Range: 6,060 km (3,250 nm, 3,740 mi) Service ceiling: 12,496 m (41,000 ft) Thrust/weight: 0.36:1
Max fuel capacity: 18,800 lb (Legacy Executive) / 11,321 lb (Legacy Shuttle) - both figures approx.

Falcon 2000

Falcon 2000
Role Business jet

Falcon 2000 EX

Falcon 2000EX

Role Business jet

Falcon 7x

Falcon 7X
Role Business jet
Manufacturer Dassault Aviation

Falcon 900

Falcon 900B
Role Business jet

Specifications (Falcon 900B)
General characteristics
 Crew: Two
 Capacity: 19 passengers
 Length: 20.21 m (66 ft 4 in) Wingspan: 19.33 m (63 ft 5 in) Height: 7.55 m (24 ft 9.5 in) Wing area: 49 m² (527 ft²) Empty weight: 10,255 kg (22,608 lb) Max. takeoff weight: 20,640kg (45,503 lb)
 Powerplant: 3 × Honeywell TFE731-5BR-1C turbofan, 21.13 kN (4,750 lbf) each
Performance Maximum speed: Mach 0.84-0.87 Cruise speed: 950 km/h (513 knots, 590 mph) at 36,000ft (10,970 m) (Mach 0.85) Stall speed: 158 km/h (85 knots, 98 mph) (wheels and flaps down) Range: 7,400 km (3,995 nm, 4,598 mi) (7 passengers) Service ceiling: 15,500 m (51,000 ft) Wing loading: 435kg/m² (91lb/ft²)

falcon-2000-3

Falcon 2000
Role Business jet

Global 5000

Global Express / Global 5000

Role Business jet

Global 5000General characteristics
 Crew: Two – Three
 Capacity: 8 in a typical configuration, up to 19 in high density arrangement
 Length: 96.8 ft (29.5 m) Wingspan: 94 ft 0 in (28.65 m) Height: 25.5 ft (7.7 m) Wing area: 1,882 ft² (53.29 m²) Useful load: 1,775 lb (w/full fuel) (805 kg) Max. takeoff weight: 92,750 lb (42,071 kg) Powerplant: 2 × Rolls-Royce Deutschland BR710A2-20 turbofans, 14,750 lbf (65.6 kN) each Cabin length: 42.47 f (12.94 m)
 Cabin width (centerline): 8.17 ft (2.49 m) Cabin width (floorline): 6.92 ft (2.11 m) Cabin height: 6.25 ft (1.91 m) Cabin floor area: 317 ft² (29.4 m²) Cabin Total Volume 1,884 ft³ (53.9 m³)
Performance
 Maximum speed: Mach .89 (513 kt, 590 mph, 950 km/h) Cruise speed: Mach .85 (488 kt, 562 mph, 904 km/h) Range: 5,200 nm (9,360 km) Service ceiling: 51,000 ft (15,000 m) Basic Operating Weight: 50,840 lb (23,061 kg) Maximum Ramp Weight: 92,750 lb (42,071 kg) Maximum Takeoff Weight: 92,500 lb (41,957 kg) Maximum Zero Fuel Weight: 56,000 lb (25,401 kg) Maximum Fuel Weight 39,250 lb (17,804 kg) Balanced field length (SL, ISA, MTOW): 5,540 ft (1,689 m) Landing distance (SL, ISA, MLW): 2,670 ft (814 m)
Avionics
 Rockwell Collins Pro Line Fusion avionics suite

Global XRS

Global Express / Global XRS

Role Business jet

Specifications
Global Express XRS
General characteristics
 Crew: Two (minimum) - four (typical) Capacity: 8-19 passengers Length: 99 ft 5 in (30.3 m) Wingspan: 94 ft 0 in (28.65 m) Height: 24 ft 10 in (7.57 m) Wing area: 1,022 ft² (94.9 m²) Empty weight: 49,750 lb (22,600 kg) Useful load: 1,775 lb w/full fuel (805 kg) Max. takeoff weight: 99,500 lb (44,500 kg) Powerplant: 2 × Rolls-Royce Deutschland BR710A2-20 turbofans, 14,750 lbf (65.5 kN) each Cabin length: 48 ft 4 in (14.73 m) Cabin max width (centerline): 8 ft 2 in (2.49 m) Cabin max width (floorline): 6 ft 11 in (2.11 m) Cabin height: 6 ft 3 in (1.91 m) Cabin floor area: 335 ft² (31.1 m²)
Performance
 Maximum speed: Mach .89 (513 kt, 590 mph, 950 km/h) Cruise speed: Mach .85 (488 kt, 564 mph, 907 km/h) Range: 6,325 nm (7,080 mi, 11,390 km) Service ceiling: 51,000 ft (15,500 m) Wing loading: 95.9 lb/ft² (468 kg/m²) Thrust/weight: 0.301 Balanced field length (SL, ISA, MGTOW): 6,120 ft (1,870 m) Landing distance (SL, ISA, MLW): 2,670 ft (814 m)

Gulf stream 200

G200 / G280

Gulfstream G200
Role Business jet
Manufacturer Gulfstream Aerospace

SpecificationsG200 Gulfstream G200 data[17]
General characteristics
Crew: 2
Capacity: seating for 8 or more in executive-style, or up to 18 as a corporate shuttle Payload: 4,050 lb (1,840 kg) Length: 62 ft 3 in (18.97 m)Wingspan: 58 ft 1 in (17.70 m)Height: 21 ft 5 in (6.53 m) Wing area: 369 ft² (34.3 m²)Empty weight: 19,200 lb (8,709 kg)Max. takeoff weight: 35,450 lb (16,080 kg)Powerplant: 2 × Pratt & Whitney Canada PW-306A turbofans, 6,040 lbf (26.9 kN) each
Performance
Maximum speed: Mach 0.85 (487 knots, 560 mph, 900 km/h) at altitude
Cruise speed: Mach 0.80 (459 knots, 528 mph, 850 km/h) normal cruise at altitude
Range: 3,400 nmi (3,910 mi, 6,300 km) at Mach 0.75 with 4 passengers
Service ceiling: 45,000 ft (13,700 m)

Amphibious Cessna 208 Caravan

Sea plane

• 10 seat (9 passengers + Pilot), Wipline 8000A amphibious floats, Turbine 675 shaft horsepower PT6 114A Pratt & Whitney engine, Range - 790 nautical miles, Maximum take-off weight 8360 lbs, Take-off run (water) 3,280' at gross weight, Take-off run (land) 1,340' at gross weight, Landing distance typically less than 1123' (water) and 735' (land), Cruise speed (75%) 140 Knots True Air Speed (KTAS) 20,000' service ceiling

Amphibious Cessna Turbo Stationair T206H

Sea plane

• 6 seat (5 passengers + Pilot), Wipline 3450 amphibious floats, Fuel injected 310 horsepower TIO- 540, Textron Lycoming engine, Range - 713 nautical miles, Gross weight 3,792 lbs Take-off run (water) 1,700' at gross weight. Take-off run (land) 900' at gross weight, Landing distance typically less than 500' (water), Cruise speed (75%) 128 KTAS, 27,000' service ceiling

Specifications (206H Stationair) General characteristics

• Crew: one Capacity: 5 passengers Length: 28 ft 3 in (8.61 m) Wingspan: 36 ft 0 in (10.97 m) Height: 9 ft 3½ in (2.83 m) Wing area: 175.5 ft² (16.30 m²) Airfoil: NACA 2412 (modified) Empty weight: 2,176 lb (987 kg) Max. takeoff weight: 3,600 lb (1,632 kg) Powerplant: 1 × Lycoming IO-540-AC1A air-cooled flat-six engine, 300 hp (224 kW) + Click here for more informationPerformance Maximum speed: 174 mph (151 knots, 280 km/h) at sea level, Cruise speed: 163 mph (142 knots, 263 km/h) at 6,200 ft (1,890 m)
  Stall speed: 63 mph (54 knots, 100 km/h), Range: 840 mi (730 nmi, 1,352 km), Service ceiling: 15,700 ft (4,785 m), Rate of climb: 988 ft/min (5.0 m/s)
  

Gulf stream G150

Gulfstream G100

Role Business jet
Manufacturer Gulfstream Aerospace

General characteristics
 Crew: 2
 Capacity: 4 passengers Payload: 3,291 lb (1,496 kg) Length: 55 ft 7 in (16.96 m) Wingspan: 54 ft 7 in (16.64 m) Height: 18 ft 2 in (5.54 m) Empty weight: 14,400 lb (6,531 kg) Loaded weight: 24,800 lb (11,249 kg) Useful load: 885 lb (401 kg) Max. takeoff weight: 24,900lb (11,500 kg) Powerplant: 2 × Honeywell TFE731-40R-200G turbofans, 4,250 lbs () each
Performance
 Never exceed speed: Mach .875 Maximum speed: 472 kts Cruise speed: 460 kts Range: 2,700 / 2,950 mi (IFR/VFR) (5,465 / 6,034 km) Service ceiling: 45,000 ft (13,716 m) Fuel capacity: 9,365 lb (4,247 kg)

Gulf stream Gulf IV

Gulfstream IV / G400 C-20F/G/H/JGIV-SP / G350 / G450

Gulfstream GIV.
Role Business jet
Manufacturer Gulfstream Aerospace

Specifications
GIV GIV-SP G350 G450
Cockpit crew Two
Seating capacity 14-19 19 maximum12-16 typicalLength 88 ft 4 in (26.9 m) 89 ft 4 in (27.2 m)Wingspan 77 ft 10 in (23.7 m) Overall height 24 ft 5 in (7.44 m) 25 ft 2 in (7.67 m)Maximum take-off weight(MTOW) 73,200 lb (33,200 kg) 74,600 lb (33,800 kg) 70,900 lb (32,200 kg) 73,900 lb (33,500 kg)Empty weight 35,500 lb (16,100 kg) 42,700 lb (19,400 kg) 43,000 lb (19,500 kg)Cruising speed Mach 0.80 (460 knots, 528 mph, 850 km/h at altitude) Maximum speed Mach 0.88 (505 knots, 581 mph, 935 km/h at altitude)
Range 4,220 nmi (7,820 km; 4,860 mi) 4,220 nmi (7,820 km; 4,860 mi) 3,800 nmi (7,040 km; 4,370 mi) 4,350 nmi (8,060 km; 5,010 mi) Service ceiling 45,000 ft (13,700 m) Engines (×2) Rolls-Royce Tay 611-8 Rolls-Royce Tay 611-8C Thrust (×2) 13,850 lbf (61.6 kN)

Hawker 400

Hawker 400

Raytheon Aircraft Beechjet 400A
Role Business jet
Manufacturer Hawker Beechcraft

HAWKER-850XP

Hawker 800 Raytheon Hawker 800XP of NetJets Europe
Role Mid-size business jet
Manufacturer Hawker Beechcraft (since 2007)
Raytheon
British Aerospace

Specifications (Hawker 850XP)
General characteristics
 Crew: 2 pilots
 Capacity: 8 passengers typical, 13 maximum
 Length: 51 ft 2 in (15.6 m)
 Wingspan: 54 ft 4 in (16.5 m)
 Height: 18 ft 1 in (5.5 m)
 Empty weight: 15,670 lb (7,108 kg)
 Max. takeoff weight: 28,000 lb (12,701 kg)
 Powerplant: 2 × Honeywell TFE731-5BR turbofan, 4660 lbf () each
Performance
 Maximum speed: 448 kts (514 mph) 830 km/h
 Cruise speed: 402 kts (463 mph) 745 km/h
 Range: 2,642 nm (4,893 km) Service ceiling: 41,000 ft (12,497 m)

Lear jet 45

Learjet 45
Role Business Jet

Specifications
Learjet 45 General characteristics
 Crew: 2
 Capacity: 9 passengers
 Length: 58 ft 0 in (17.68 m)
 Wingspan: 47 ft 10 in (14.58 m) Height: 14 ft 1 in (4.30 m) Wing area: 311.6 ft² (28.95 m²) Empty weight: 12,850 lb (5,829 kg) Max. takeoff weight: 20,200 lb (9,163 kg) Powerplant: 2 × Honeywell TFE731-20 turbofan, 3,500 lb (15.57 kN) each
Performance
 Maximum speed: 533 mph (463 knots, 858 km/h, Mach 0.81) (max cruise)
 Cruise speed: 500 mph (434 knots, 804 km/h, Mach 0.76) Range: 1,968 mi (1,710 nmi, 3,167 km) (4 passengers) Service ceiling: 51,000 ft (15,545 m)

Lear jet 60

Learjet 60
Role Business jet
Manufacturer Bombardier Aerospace

Premier jet 1A Jet

Premier I/IA

Raytheon 390 Premier IA
Role Civil utility aircraft
Manufacturer Raytheon/Hawker Beechcraft

Specifications (Premier I)
A Premier IA at an aviation industry trade fair in Germany
General characteristics
 Crew: 1-2
 Capacity: 6-7 passengers (depending on crew complement)
 Length: 46 ft 0 in (14.02 m) Wingspan: 44 ft 6 in (13.56m) Height: 15 ft 4 in (4.67 m) Wing area: 247.0 sq ft (22.95 m²) Aspect ratio: 8.0:1
 Empty weight: 7,996 lb (3,627 kg) Max. takeoff weight: 12,500 lb (5,670 kg)
 Powerplant: 2 × Williams FJ44-2A turbofan, 2,300 lbf (10.23 kN) each
Performance Maximum speed: 530 mph (461 knots, 854 km/h) at 33,000 ft (10,060 m) (max cruise)
 Range: 1,645 mi (1,430 nmi, 2,648 km) with single pilot and four passengers
 Service ceiling: 41,000 ft (12,500 m)

Piper PA-42 Cheyenne

PA-42 Cheyenne

Cheyenne 400LS
Role Turboprop
Manufacturer Piper Aircraft

Specifications (PA-42-720 Cheyenne IIIA)
General characteristics
 Crew: One or two
 Capacity: 1 to 9 passengers
 Length: 43 ft 4¾ in (13.23 m) Wingspan: 47 ft 8 in (14.53 m) Height: 14 ft 9 in (4.50 m) Wing area: 293.0 ft² (27.22 m²) Empty weight: 6,837 lb (3,101 kg)
 Max. takeoff weight: 11,200 lb (5,080 kg) Powerplant: 2 × Pratt & Whitney Canada PT6A-41 turboprop, 720 shp (537 kW) each
Performance
 Maximum speed: 314 knots (582 km/h, 362 mph) Cruise speed: 282 knots (523 km/h, 325 mph) at 35,000 ft (10,700 m) Stall speed: 89 knots (165 km/5, 103 mph) (flaps and undercarriage down) Range: 2,270 nmi (4,207 km, 2,614 mi) Service ceiling: 35,840 ft (10,925 m) Rate of climb: 2,380 ft/min (12.1 m/s) Wing loading: 38.2 lb/ft² (186.7 kg/m²) Power/mass: 0.13 hp/lb (0.21 kW/kg)