Dimensional Data

 

Aircraft length

22,605 m

Wing span

24.505(25.505) m

Empty aircraft overall height at rest

8.232 m

Landing gear track

3.18 m

Wheel base

8.07 m

Wheels of nose landing gear

0.6 x 0.22 m

Wheels of main landing gear

0.81 x 0.32 m

Uner floor baggage volume

3 m³

Transport compartment length

14.51 m

Rear baggage /carg compartment volume

6.1 m³

 

Cabin Inner Space :
IRAN-140 A/C has one of the biggest body diameters in category of turbo prop
Passenger A/C with 4 passengers in width.
In this A/C , the structural weight has been reduced to its minimum rate because of completely circular cross-section.
The gallery width of the A/C is 46 cm which is more than those of DORNIER 328,SAAB 2000 and FOKKER 50 and equals to those of ATR42 and ATR72.

Commercial cabin length 14.5 m

Maximum width

2.60 m

Floor width

2.28 m

Height

1.9 m

Volume of aft baggage and cargo compartment

6.1 m3

Volume of under floor baggage and cargo compartment

3 m3

Capacity of rear baggage / cargo compartment 1040 kg
Capacity of under floor bagage /cargo compartment 560 kg
Total volume of over head bin 2.3 m

 


Main Data                                                                                                         

Overall Dimension

Length 22.46 m 73.67 ft
Wing span 24.25 m 79.54 ft
Fuselage Diameter 2.82 m 9.25   ft

Cabin Dimension

Length 11.6 m 38.05 ft
Height 1.9   m 6.23   ft
Width 2.6   m 8.54   ft

Weight

Max. Take-off Weight 21,000 kg 46,200 lb
Max. Landing Weight 21,000kg 46,200 lb
Max. zero fuel weight 19,100kg 42,020 lb
Max. Payload 6,000 kg 13,200 lb
Max. Fuel 4,370 kg 9,614   lb

Performance

Take-off Run (1-engine)* 1,350m 4,415 ft
Take-off Distance(1-engine)* 1,750 m(1,925) 5,740 ft (6,314)
Landing Distance* 1,360 m 4,460 ft
Climb,2 engine* 410 m/min 1,345 ft/min
Max. Cruise Speed (18,000 ft)* 533 km 285 KTAS
Range (Cruise Speed)** 2,100 km 1,134 NM

* MTOW, ISA,SL.

** 52 Pax,90 kg/198 lb each , 45 min hold, ISA.

 

IRAN-140 PROJECT

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