Technical characteristics of AN-74TK-300
·Maximum take-off weight 37500 kg
·Maximum landing weight 33000 kg
·Maximum payload 10000 kg
·Maximum fuel load (r=0.775 kg/dm) 13 210 kg
·Maximum cruising speed 750 km/h
·Operating ceiling 10100 m
·Required runway length (SA, H=0) 1900 m
·Specific fuel consumptions 280
·Number of passengers 52
·Flying range:
  - with 10 tons load 1500
  - with 52 passengers 3500
  - with maximum fuel reserve 5200
·Crew (2 pilots and 1 flying attendant)

 AN-74TK-300 with a new interior designed and produced by InterAMI Interior

Flight control equipment
Flight control equipment conforms with ICAO 2015 regulations
Navigation system corresponds to B-RNAV, RNP-5


· NCS NVS-74TM "Malva"
· GPS "SN-3301"
· Heading reference
· IRS "Buran-74T"
· Dual RA "A-073"
· Dual VOR/ILS
· Dual DME
· Shoran "Beep-M"
· Dual ADF "ARK-22"
· RMI
· ATC Transponder "SO-72M"
· TCAS 2000 (with mode S transponder)

Avionics

· IFMS
· FES
· GPWS
· IFF


Cockpit of AN-74TK-300
4.4 Mb (Acrobat Reader)
  Power unit

Power unit of AN-74TK-300 airplane		 Power unit consists of two double-flow turbojet engines of modular construction (D-36 4A series).


Take-off mode (H=0, Ì=0)
Thrust 6 500 kGs (63.8 Kilonewton) kN
Fuel consumptions (maximum) 0,358 kgs/hour
Extreme altitude 11 000 m
Altitude performance:
 (engine start)
On the ground 5000 m
In the air 8000 m

The reliable and economical D-36 engine is also installed on An-72, An-74, Yak-42, Tu-334 and Be-200 airplanes
Installed on the planes:

An-72   Yak-42   Be-200
An-74   Tu-334
Radio equipment

· HF radiostation "Arlekin"- DA
· VHF (Frequency spectrum of 8.33 kHz) 2 radiostations "Orlan"-85ST
· ICS "Liner" - MVL
· CVR "Opal" - B
· Emergency MW/UHF
· Emergency beacon "Cospas Sarsat"
Cargo-range chart
Cargo-range chart of AN-74TK-300 Airplane photo
Plane in three views
AN-74TK-300 aircraft - view from above AN-74TK-300 aircraft - side view
AN-74TK-300 aircraft - front view
AN-74TK-300 aircraft - side view AN-74TK-300 aircraft - front view