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