Fairchild Hiller FH-227
Technical Specifications
First Flight: |
September 1964 |
Number Built: |
78 were built for commercial use |
Length: |
83 feet 8 inches |
Wing Span: |
95 feet 2 inches |
Height: |
27 feet 7 inches |
Max Take-Off Wt.: |
43,500 lbs. |
Max Landing Wt.: |
43,000 lbs. |
Empty Wt.: |
24,000 lbs. |
Max Cruising Speed: |
294 mph 255 kts |
Normal Cruising Speed: |
265 mph 230 kts |
Approach Speed: |
150 mph 130 kts |
Landing Speed: |
130 mph 115 kts |
Stall Speed: |
97 mph 84 kts |
Service Ceiling: |
28,000 feet |
Fuel Capacity: |
1364 US gallons |
Range: |
1647 miles w/maximum fuel load
612 miles w/maximum payload |
Fuel Type: |
JP-4 or Jet A |
Fuel Consumption: |
220 gph flight plan burn w/max fuel
593 gph flight plan burn w/max load |
Engines: |
2 Rolls-Royce Mk 532-7 rated at 2250 ESHP each |
Seating: |
56 passengers |
Crew: |
2 Pilots 2 Flight attendents |
Engine Specifications
|
Rolls-Royce Mk 532-7
|
Type: |
Axial-Flow Prop-Jet |
Diameter: |
N/A |
Length: |
N/a |
Compressor Stages: |
N/A |
Turbine Stages: |
N/A |
Weight: |
N/A |
Starter: |
Airframe Furnished |
Fuel Grade: |
JP-4 or Jet A |
Performance: |
Rated 2250 ESHP |
|