Y-7H Chinese Military Transport Aircraft
Y-7H
Spotted an error? Sign in to suggest an edit.
Other
Basic Information
Name
Y-7H Chinese Military Transport Aircraft
Designation
Y-7H
Alternate Designation
—
Equipment Type
—
Manufacturer
—
Date of Introduction
1992
Description
A reverse-engineered An-26 with rear loading ramp for the PLAAF, entering production in 1992.
Air & Air Defense Specifications
Crew
5
Engine
2 x turboprops; and 1 x auxiliary turbojet for takeoff assist
Max Speed
540.0 km/h
Cruise Speed
440.0 km/h
System
Alternate Designation(s)
Y-7H
Primary Function / Type
Military Transport Aircraft
Manufacturer
INA
In Service
1992-Present
Crew
5 (pilot, co-pilot, navigator, flight engineer, radio operator)
Passengers
38 to 40 seats in pressurized cargo bay; or 24 litters and attendants
Number of Engines
3
Day/Night Capable
Yes
All Weather Capable
Yes
Number of Hard Points
INA
Dimensions
Length
23.80 m
Width (Wing Span)
29.20 m
Height
8.58 m
Wing Area
74.98 sq m
Cabin Length
11.50 m
Cabin Width
2.40 m
Cabin Height
1.91 m
Weight, Empty
15,020 kg
Weight, Max Takeoff
5,500 kg
Payload, Normal
4,500 kg
Payload, Maximum
24,000 kg
Automotive
Engine Name
INA
Engine Type
2 x turboprops; and 1 x auxiliary turbojet for takeoff assist
Number of Engines
3
Engine Power
INA
Internal Fuel Capacity
7,050 liters
Maximum Speed
540 km/h
Cruise Speed
440 km/h
Takeoff Speed
200 km/h
Landing Speed
190 km/h
Maximum Range, with Maximum Payload
1,100 km
Maximum Range, with Maximum Fuel
2,550 km
Climb Rate
480 m/min
Ceiling
7,500 m
Takeoff Run
780 m
Landing Run
730 m
Communications
Radio
INA
Protection
Stealth Properties
No
Heat Signature Reduction
No
Add on Armor
No
NBC Protection
Yes
EW Counter Measures
No
Chaffs/Flares
INA
Details
Country of Origin
China
Category
Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
Y
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
23.8 m
Width
29.2 m
Height
8.58 m
Weight
5500 kg
Operators (1)
China
Something went wrong. Please reload the page.
Reload