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) |
|
ANN's Daily Aero-Linx (12.02.24)
See All