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Baron G58
Hawker Beechcraft Corporation
фотография с сайта www.airliners.com
SpecificationsDesign Weights
Max. Ramp Weight 5,524 lb (2,506 kg)
Max. Takeoff Weight 5,500 lb (2,495 kg)
Max. Landing Weight 5,400 lb (2,449 kg)
Max. Zero Fuel Weight * 5,215 lb (2,365 kg)
Fuel Capacity
(194 gal fuel system) 1,164 lb (528 kg)
* Calculated weight based on MTOW minus fuel required to fly 1.5 hours at HSC.
Weight Breakdown
Basic Empty Weight ** 3,880 lb (1,760 kg)
1 pilot 170 lb (77 kg)
Basic Operating Weight 4,050 lb (1,837 kg)
Typical Options:
Air-conditioning 88 lb (40 kg)
Prop unfeathering accumulators 12 lb (5 kg)
Typically Equipped Basic Operating Weight 4,150 lb (1,882 kg)
Max. Payload (without pilot) 1,235 lb (560 kg)
Useful Load (without pilot) 1,544 lb (700 kg)
** Basic Empty Weight includes standard interior, avionics, unusable fuel and oil
Characteristics
Seating (Crew + Pax) 1 + 4 / 5
Wing Loading 27.6 lb/sq ft
Power Loading 9.17 lb/SHP
External Dimensions
Length 29 ft 10 in (9.09 m)
Height 9 ft 9
in (2.97 m)
Span 37 ft 10 in (11.53 m)
Engines
Manufacturer 2 Teledyne Continental
Model IO-550-C
Output 300 hp
Inspection Interval 1,700 hrs
Weights
Max Ramp 5,524 lb (2,506 kg)
Max Takeoff 5,500 lb (2,495 kg)
Max Landing 5,400 lb (2,449 kg)
Max Zero Fuel 5,215 lb (2,365 kg)
Typically Equipped
Basic Operating (w/1 pilot) 4,150 lb (1,882 kg)
Payload / Capacities
Max Payload (without pilot) 1,235 lb (560 kg)
Useful Load (without pilot) 1,544 lb (700 kg)
Max Fuel Capacity 1,164 lb (528 kg)
(1 US gal = 6.0 lb/US gal) 194 US gal
Fuel w/max payload 309 lb (140 kg)
Cabin Dimensions
Length 12 ft 7 in (3.84 m)
Height 4 ft 2 in (1.27 m)
Width 3 ft 6 in (1.07 m)
Cabin Volume
Cockpit 36 cu ft (1.02 cu m)
Passenger Cabin
(including baggage) 101 cu ft (2.86 cu m)
Total Volume 137 cu ft (3.88 cu m)
PerformanceAirport Performance
Takeoff Field Length
Max. TO Wt., SL, ISA 2,300 ft (701 m)
Max. TO Wt., 5,000 ft elevation, 25°C 4,000 ft (1,219 m)
Accelerate-Stop Distance
Max. TO Wt, SL, ISA 3,000 ft (914 m)
Max. TO Wt, 5,000 ft elevation, 25°C 4,330 ft (1,320 m)
Landing Distance
Max Landing Wt., SL, ISA 1,300 ft (396 m)
Vapproach 95 kt
Climb Performance (Max Takeoff Weight)
Time to Climb / Altitude 10 min / FL 100
Climb Rate 1,700 fpm (518 m/min)
Climb Gradient 851 ft/ nm (140 m/km)
Engine-out Rate 390 fpm (119 m/min)
Engine-out Gradient 207 ft/nm (34 m/km)
Ceilings
All-Engine Service 20,688 ft (6,306 m)
Engine-out Service 7,284 ft (2,220 m)
Cruise Performance
High-Speed Cruise (25 in Hg (or Full Throttle)
@ 2,500 RPM
6,000 ft 202 kt/232 mph (374 km/hr)
8,000 ft 200 kt/230 mph (370 km/hr)
10,000 ft 198 kt/228 mph (367 km/hr)
Normal Speed Cruise (23 in Hg (or Full Throttle) @ 2,300 RPM
6,000 ft 190 kt/219 mph (352 km/hr)
8,000 ft 192 kt/221 mph (356 km/hr)
10,000 ft 189 kt/217 mph (350 km/hr)
Long Range Cruise (21 in Hg (or Full Throttle)
@ 2,100 RPM
6,000 ft 167 kt/192 mph (309 km/hr)
8,000 ft 173 kt/199 mph (320 km/hr)
10,000 ft 177 kt/204 mph (328 km/hr)
Maximum Range at Various Altitudes and Speeds (1 pilot + 2 passengers – VFR)
High-Speed Cruise (25 in. Hg (or Full Throttle)
@ 2,500 RPM
6,000 ft 948 nm/1,091 sm (1,756 km)
8,000 ft 1003 nm/1,154 sm (1,858 km)
10,000 ft 1052 nm/1,211 sm (1,948 km)
Normal Speed Cruise (23 in. Hg (or Full
Throttle) @ 2,300 RPM
6,000 ft 1,031 nm/1,186 sm (1,909 km)
8,000 ft 1,050 nm/1,208 sm (1,945 km)
10,000 ft 1,101 nm/1,267 sm (2,039 km)
Long Range Cruise (21 in. Hg (or Full Throttle)
@ 2,100 RPM
6,000 ft 1,388 nm/1,597 sm (2,571 km)
8,000 ft 1,370 nm/1,577 sm (2,537 km)
10,000 ft 1,383 nm/1,592 sm (2,561 km)
Maximum Range Performance (VFR reserves)
Executive Payload (1 pilot + 4 passengers)
Range 888 nm (1,645 km)
Average Speed 160 kt (296 km/hr)
Trip Fuel 645 lb (293 kg)
Ferry (1 pilot only)
Range 1,563 nm (2,895 km)
Average Speed 164 kt (304 km/hr)
Trip Fuel 1,081 lb (490 kg)
Mission Performance (1 pilot + 3 passengers)
200 nm mission
Flight Time 1 hr 02 min
Trip Fuel 226 lb (103 kg)
Flight Level FL 060
500 nm mission
Flight Time 2 hr 31 min
Trip Fuel 531 lb (241 kg)
Flight Level FL 060
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