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Performance
/ Specification |
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Baron
58 |
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Performance
/ Specification |
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Design
Weights |
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Max. Ramp Weight
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5,524 lb. 2,505 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 (with optional 194 gal. fuel system)...............................
1,164 lb. 528 kg.
* Calculated weight based on MTOW minus weight of fuel for
1.5 hr at High Speed Cruise.
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Weight
Breakdown |
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Basic
Empty Weight .......................................................................
3,770 lb.
1 pilot..............................................................................................
170 lb.
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1,710 kg |
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77 kg |
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Basic Operating
Weight...................................................................
3,940 lb. 1,787 kg |
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Typically
Equipped Basic Operating Weight 4,060 lb. |
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Max. Payload (including
1 pilot) ........................................................ 1,325
lb. 601 kg.
Useful Load (including 1 pilot) ..........................................................
1,634 lb. 741 kg.
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Characteristics |
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Seating (Crew +
Pax) .......................................................................
1 + 4 / 5
Wing Loading ..................................................................................
27.6 lb./sq. ft.
Power Loading .................................................................................
9.17 lb./SHP
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Payload
/ Capacities |
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Max Payload ....................................................................................
1,325 lb. (601 kg.)
Useful Load.......................................................................................
1,634 lb. (741 kg.)
Max Fuel Capacity (with optional 194 gal. fuel system) .........................
1,164 lb. (528 kg.)
(1 US gal = 6.0 lb./US gal.)................................................................
194 US gal.
Fuel w/max payload...........................................................................
309 lb. (140 kg.)
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Cabin
Dimensions |
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Length..............................................................................................
12 ft. 7 in. (3.83 m)
Height ...............................................................................................
4 ft. 2 in. (1.27 m)
Width ................................................................................................
3 ft. 6 in. (1.07 m)
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Cabin
Volume |
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Cockpit ..........................................................................................
36 cu. ft. (1.02 cu. m)
Passenger Cabin ...........................................................................
101 cu. ft. (2.86 cu. m)
(including baggage)
Total Volume .................................................................................137
cu. ft. (3.88 cu. m)
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Climb
Performance (Max Takeoff Weight) |
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Time to Climb /
Altitude ................................................................
10 min / FL 100
Climb Rate ..................................................................................
1,700 fpm (518 m/min)
Climb Gradient..............................................................................
851 ft/ nm (259 m/km)
Engine-out Rate ..............................................................................
390 fpm (119 m/min)
Engine-out Gradient .........................................................................
207 ft/nm (63 m/km)
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Ceilings |
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All Engine Service
............................................................................
20,688 ft. (6,306 m)
Engine-out Service .............................................................................
7,284 ft. (2,220 m)
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Cruise
Performance |
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High Speed
Cruise (25 In. Hg (or Full Throttle) @ 2,500 RPM |
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6,000 ft ..........................................................................
202 kt/233 mph (374 km/hr)
8,000 ft ..........................................................................
200 kt/230 mph (370 km/hr)
10,000 ft ........................................................................
198 kt/228 mph (367 km/hr)
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Normal Speed
Cruise (23 In. Hg (or Full Throttle) @ 2,300 RPM |
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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)
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Long Range
Cruise (21 In. Hg (or Full Throttle) @ 2,100 RPM |
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6,000 ft ...........................................................................
159 kt/183 mph (294 km/hr)
8,000 ft ...........................................................................
164 kt/189 mph (304 km/hr)
10,000 ft .........................................................................
167 kt/192 mph (309 km/hr)
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Back to Top |
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©Copyright
2003. All Rights Reserved. Yokota Aviation Incorporated. |
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