Factopedia
[O]bjects
[C]omparisons
Comparisons
/ Comparison of Bombardier Q100 (Dash 8-100) and North American B-25 Mitchell
Please fix the following errors:
Comparison of Bombardier Q100 (Dash 8-100) and North American B-25 Mitchell
[S]ave
Attribute
North American B-25 Mitchell
×
Bombardier Q100 (Dash 8-100)
×
General
Manufacturer
North American Aviation NAA
Bombardier Aerospace
Model
North American B-25 Mitchell
Bombardier Q100 (Dash 8-100)
Country
United States
Canada
1
↑
Manufactured from (year)
1940
1983
Manufactured to (year)
1945
-
Type
Military Propellor Planes
Light Passenger Jets
Icao
B25
Q100
Performance
Engine
2x Wright R-2600-92 Twin Cyclone
Pratt & Whitney Canada PW120
Power, hp (hp)
1,700
2,000
Avionics
-
UNS-1Ew FMS, EFI-890R
Max cruise speed (km/h)
437
535
Approach speed (km/h)
148
250
Travel range (km)
2,167
2,084
Service ceiling (m)
7,376
7,620
Rate of climb (m/sec)
5.08
7.49
Take off distance (m)
-
1,000
Landing distance (m)
-
780
Weights
Max take off weight (kg)
15,876
15,650
Max payload (kg)
3,060
4,536
Fuel tank capacity (l)
3,687
3,161
Baggage volume (m³)
-
8.5
Dimensions
Seats
5
4
Cabin height (m)
-
1.95
Cabin width (m)
-
2.5
Cabin length (m)
-
9.16
Exterior length (m)
16.13
22.25
Tail height (m)
4.98
7.5
Fuselage diameter (m)
1.4
2.69
Wing span (m)
20.6
25.9
Wing tips
No Winglets
No Winglets
Help
·
Contact us
·
Disclaimer
·
Contributors
·
Developers
·
Donate