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Wed, Jan 08, 2003

Beech 1900D Specs/Performance

Raytheon/Beech 1900D Specifications/Performance


Seating

Crew + Std/Max
 2 + 12/19

Maximum Speed 

284 KTAS/327 mph

Maximum Altitude 

25,000 ft

Max Range

1,462 nm

 

POWERPLANTS

Two Pratt and Whitney Canada PT6A-67D

Thrust: 1,279 shp

 

PERFORMANCE

Maximum Speed (16,000 ft At 14000 lb) 284 kts (327 mph)

 

Cruise Speeds (TAS At 14,000 lb)

High Speed Cruise Power (1,550 rpm)

12,000 ft 283 kts (326 mph)
16,000 ft 284 kts (327 mph)
20,000 ft 282 kts (325 mph)
25,000 ft 277 kts (319 mph)

 

Intermediate Cruise Power (1,550 rpm)

12,000 ft 265 kts (305 mph)
16,000 ft 265 kts (305 mph)
20,000 ft 262 kts (301 mph)
25,000 ft 256 kts (295 mph)

 

Long Range Cruise Power (1,400 rpm)

12,000 ft 205 kts (236 mph)
16,000 ft 212 kts (244 mph)
20,000 ft 219 kts (252 mph)
25,000 ft 224 kts (258 mph)

 

Rate Of Climb At Sea Level, Flaps Up With Two Engines

At 16,950 lb 2,625 ft / min

 

Rate Of Climb At Sea Level, Flaps Up With One Engine

At 16,950 lb 670 ft / min

 

Service Ceiling - Two Engines (100 ft / min)

At 16,950 lb Above 25,000 ft

 

Service Ceiling - One Engine (50 ft / min)

At 16,950 lb 17,500 ft

 

Stall Speeds, IAS At 16,950 lb With Idle Power

Flaps 35° 84 kts
Flaps 17° 90 kts
Flaps Up 101 kts

 

Take-Off Field Length At 16,000 lb, Flaps 17 Degrees, Standard Day, Sea Level

Decision Speed 100 KIAS
Total Distance 3,470 ft

 

Take-Off Field Length At 17,120 lb, Flaps 17 Degrees, Standard Day, Sea Level

Decision Speed 103 KIAS
Total Distance 3,813 ft

 

Landing Distance At 16,765 lb, Flaps Down, Zero Wind, At Sea Level

Approach Speed 118 KIAS
Total Distance Over 50 ft Obstacle 2,800 ft

 

Mission Profile

Mission Allows For Taxi And Run-Up; Includes Climb, Cruise And Descent; NBAA IFR Reserve Profile (100 nm Alternate); Zero Winds And ISA Conditions Enroute; 16,950 lb Take-Off Weight
Eleven Occupants @ 170 lb each, 330 lb Baggage And 4,458 lb Fuel Before Engine Start
Mission 1,000 nm
Average Speed 269 kts (310 mph)
Mission Time 3 HRS 43 min

 

Wing Area and Loadings

Wing Area 310 sq ft
Wing Loading 55.2 lb / sq ft
Power Loading 6.69 lb / shp

 

Dimensions

Wing Span 57 ft 11 in
Stabilizer Span 18 ft 6 in
Length 57 ft 10 in
Height To Top Of Horizontal Stabilizer 14 ft 11 in
Cabin Length (Excludes Pilot/Aft Baggage Compartment) 25 ft 3 in
Cabin Width 4 ft 6 in
Cabin Height 5 ft 11 in
Cabin Floor Width 4 ft 1 in
Entrance Door 25 in x 64.2 in
Cockpit Volume 103 cu ft
Cabin Volume 640 cu ft
Aft Baggage Compartment Capacity 1,630 lb, 175 cu ft


Pressurization

(5.0 PSI Differential) Cabin Altitude
Actual Aircraft Altitude 11,052 ft Sea Level
Actual Aircraft Altitude 15,000 ft 2,750 ft
Actual Aircraft Altitude 20,000 ft 6,060 ft
Actual Aircraft Altitude 25,000 ft 9,125 ft

RANGE

Allowance: Start, Taxi, Take-Off, Climb, Cruise, Descent, NBAA IFR Reserve Profile (100 nm Alternate)

Conditions: Zero Wind, ISA Conditions Enroute, 16,950 lb Take-Off Weight Maximum Fuel (4,458 lb) With Available Payload (1,917 lb)

High Speed Cruise Power (1,550 rpm)

12,000 ft
869 nm (1,000 sm)
16,000 ft
967 nm (1,113 sm)
20,000 ft
1,078 nm (1,240 sm)
25,000 ft
1,231 nm (1,417 sm)

Intermediate Cruise Power (1,550 rpm)

12,000 ft
926 nm (1,066 sm)
16,000 ft
1,039 nm (1,197 sm)
20,000 ft
1,165 nm (1,340 sm)
25,000 ft
1,331 nm (1,532 sm)

Long Range Cruise Power (1,400 rpm)

12,000 ft
1,035 nm (1,191 sm)
16,000 ft
1,140 nm (1,311 sm)
20,000 ft
1,246 nm (1,434 sm)
25,000 ft 1,367 nm (1,573 sm)


FMI: www.raytheon.com

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