• PASSENGER AIRCRAFT
• Yak-40
• An-140
• An-74
• An-24rb
• TRANSPORTATION AIRCRAFT

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PASSENGER AIRCRAFT

 

Yak-40

 

Maximum take-off weight	17.2 tons
Maximum landing weight	17.2 tons
Maximum payload weight	2.72 tons
Equipped aircraft weight	9.85 tons
Maximum cruising speed	510 km/h
Operating ceiling	8100 m
Flying range
with maximum fuel reserve	1800 km
with maximum payload (fuel reserve)	1350 km
Required runway length (ISA conditions, at sea level)	1250 m
Crew	5 people

An-140

 

Crew	5 persons
Passenger capacity	52 persons
Maximum takeoff weight	21500 kg
Maximum landing weight	21000 kg
Maximum payload	6000 kg
Maximum fuel load weight (q = 775 kg/m3)
gravity filling	4440 kg
single point fueling	4440 kg
Maximum cruising speed	537 km/h

An-74

Àn-74ÒÊ-200 UR-74026 Aircraft:

Year of manufacture	1992
Crew	6
Maximum takeoff weight, t	36,5
Maximum payload, t	10,0
Maximum range, km	3800
Maximum fuel, kg	13500
Maximum flight rate, km/h	750
Cruising rate, km/h	650
Operating ceiling, m	10100
Takeoff roll, m	620
Landing run, m	420
Required runway length, m	1200

An-24rb

 Àn-24RV UR-MSI Aircraft

Year of manufacture	1975ã.
Crew	5
Maximum takeoff weight, t.	22,5
Maximum payload, kg	2720
Maximum passenger capacity, person	48
Maximum range, km	1500
Cruising rate, km/h	475
Landing rate, km/h	180
Climb time 6000 m, min	15
Operating ceiling, m	8400
Takeoff roll, m	650
Landing run, m	590
Required runway length, m	1300