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Home > Aircraft > Transport Aircraft > Y-7 > Specifications

Y-7 Specifications

HISTORY
First flight 25 December 1970
Operator PLA Air Force, PLA Naval Air Force, Army Aviation Corps
Variants Y-7, Y-7-100, Y-7-200A/B, MA-60, Y-7H, Y-7G
CREW
Y-7 5
Y-7-100 3
Y-7H 3
Y-7-200/MA-60/Y-7G 2
DESIGN
Role Y-7: Passenger transport
Y-7H: Cargo/troop transport
Designer Antonov Design Bureau
Manufacturer Xi'an Aircraft Corporation
DIMENSIONS
Length 23.71m
Wingspan 29.64m
Height 8.55m
WEIGHTS
Empty 14,900kg
Normal take-off N/A
Max take-off 61,800kg
Payload 5,700kg cargo, or 50 passengers, or 24 equipped troops
PROPULSION
Powerplant

(Y-7/-100) 2 X WJ-5A-I turboprop, each rated at 2,900hp
(Y-7H) 2 X WJ-5E, , each rated at 3,050hp, plus a PY19A-300 auxiliary turbojet rated at 900kg
(Y-7-200/MA-60/Y-7G) 2X Pratt & Whitney PW127C turboprop

PERFORMANCE
Max speed 540km/h
Cruising speed 450~475km/h
Service ceiling 9,000m
Max range 2,400km (with maximum fuel); or 750km (with maximum load)
Flight endurance 6.5 hours
In-flight refuelling No
Runway (take-off) 640m
Runway (landing) 645m

 

 

 

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