PZL MD-12

· PZL Mielec

Airplanes

Length

15.8 m

Flat Wing Span

23.6 m

Height

5.95 m

Flat Wing Area

57 m²

Flat Wing Aspect Ratio

9.45

Max Seating

Cruise Speed

280 km/h

Max Speed

305 km/h

Max Ceiling

5200 m

Number of Engines

First Flight

1959-07-21

Entry Into service

1961-01-01

Number Built

Maximum Take-Off Weight

7 t (paragliders: kg)

Total Fuel Capacity

1600

Maximum Range

2100 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
PZL MD-12	7	1600	2100

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Farman F.211		15.9	23		Compare
Bristol Pullman	Liberty L-12	15.8496	24.6888	14	Compare
Bristol Braemar	Liberty L-12	15.5448	24.6888		Compare
Short Mayo Composite	Napier Rapier	15.5448	22.2504		Compare
Blériot 195		14.7	23.2		Compare
Potez 661	Renault 6Q	16.6	22.5		Compare

All data (26 fields)

Name: PZL MD-12
Manufacturer: PZL Mielec
Description: The MD-12 is a Polish four-engined short-range passenger and civil utility aircraft of the 1960s, which remained in the prototype stage.
First Flight: 1959-07-21
Entry Into service: 1961-01-01
Service End: 1965-01-01
Designer: PZL Mielec
Type: Passenger aircraft
Length (m): 15.8
Height (m): 5.95
Cockpit Crew: 2
Max Seating: 20
Max Speed (km/h): 305
Cruise Speed (km/h): 280
Min Speed (km/h): 100
Max Ceiling (m): 5200
Rate of Climb (m/s): 5.7912
Capacity Description: 20 passengers
Number Built: 3
Powerplant Description: 4 × WN-3 air-cooled 7-cylinder radial engines, 246 kW (330 hp) each
Primary Users: LOT Polish Airlines
Wikipedia Article (URL): en.wikipedia.org/wiki/PZL_MD-12
Flat Wing Span (m): 23.6
Flat Wing Area (m²): 57
Flat Wing Aspect Ratio: 9.45
Number of Engines: 4