An-74TK-300 Transport aircraft. First flight: 1995

 


 Technical specifications      Photos      Video

 

 

The An-74TK-300 is a convertible cargo/passenger jet aircraft to haul either 52 passengers or 10 t of cargo. A further An-72/An-74 derivative, it is powered by two D-36 Series 4A engines producing 6,500-kg thrust. It differs from the baseline aircraft in its underwing engine arrangement, a modified wing, uprated aircraft systems, an up-to-date flight navigation suite compliant with international standards, as well as enhanced comfort of the cockpit and passenger cabin. 

The aircraft completed its maiden flight on 20 April, 2001. In the future, the plane is going to be outfitted with 7,500-kgf D-436T1 engines. It is being productionised by the Kharkovbased KhGAPP aircraft plant.

 

An-74TK-300 © Konstantinos Panitsidis

 


THREE-VIEW DRAWING

An-74TK-300 © Konstantinos Panitsidis

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Antonov
COUNTRY
Ukraine
TYPE
Transport aircraft
CREW
2
POWER-PLANT
2 TJE Progress D-36 seria 4A 
Thrust, kN
2 x 63.80
DIMENSIONS
 
Length, m
28,07
Height, m
8,65
Wing span, m
31,89
Wing area m2
98,62
WEIGHT
 
Maximum take-off, kg
37.500
Normal take-off, kg
-
Empty aircraft, kg
19.000
Internal fuel, kg
13.210
PERFORMANCE
 
Maximum speed, km/h
740
Cruising speed, km/h
700
Service ceiling, m
11.000
Ferry range, km
5.300
Range, km
1.500
Payload, kg
or up to 10.000 kg freight
ARMAMENT
-