Fokker 50: Difference between revisions

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→‎Specs: formatting
(Removed the cockpit screenshot now in the infobox.)
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==Specs==
==Specs==
*Crew:2
{| class="wikitable"
*Passengers max.: 58 
|-
*Propulsion: 2 Turboprop Pratt & Whitney Canada PW125B (each)1864 kW2500 shp 
| Crew
*Speed: 284 kts
| 2
*Service Ceiling: 7.620 m / 25.000 ft
|-
*Range: 1.421 NM 
| Passengers
*Empty Weight: 12.570 kg / 27.712 lbs
| max. 58
*Max. Takeoff Weight: 18.990 kg / 41.866 lbs 
|-
*Wing Span: 29m / 95,1 ft
| Propulsion
*Wing Area: 70,0 m² / 753 ft²
| 2 Pratt&Whitney Canada PW125B turboprop engines, each with 1864 kW (2500 shp)
*Length: 25,20 m / 82,7 ft
|-
*Height: 8,30 m / 27,2 ft 
| Speed
*First Flight: 28.12.1985
| 284 kts
*Production Status: out of production
|-
*Production Range:1987-1997
| Service Ceiling
*Total Production: 213  
| 7620 m (25,000 ft)
*Variants: Fokker 60
|-
 
| Range
| 1421 nm
|-
| Empty Weight
| 12,750 kg (27,712 lbs)
|-
| Max. Takeoff Weight
| 18,990 kg (41,866 lbs)
|-
| Wing Span
| 29 m (95.1 ft)
|-
| Wing Area
| 70.0 m² (753 ft²)
|-
| Length
| 25.20 m (82.7 ft)
|-
| Height
| 8.30 m (27.2 ft)
|-
| First Flight
| 28.12.1985
|-
| Production Status
| out of production
|-
| Production Range
| 1987-1997
|-
| Total production
| 213
|-
| Variants
| Fokker 60
|}


== External links ==
== External links ==
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