L-7
L-7
Training Turboprop Aircrafts
Basic Information
Name
L-7
Designation
L-7
Alternate Designation
—
Equipment Type
Training Turboprop Aircrafts
Manufacturer
Hongdu Aircraft Industry Group
Date of Introduction
2018
Description
The Hongdu Aviation Industry Group (HAIC) has built six L-7 prototypes with the first airplane showcased at the Zhuhai air show in November 2010 but no maiden flight has been reported yet. The PLAAF may accept the L-7 basic turboprop aircraft in the 2016-2018 timeframe.
Air & Air Defense Specifications
Crew
2
Max Speed
500.0 km/h
Range
1400.0 km
Service Ceiling
4000 m
Overview (Deagel)
Group
Training Turboprop Aircrafts
Status
Under Development
Origin
China
Contractor
Hongdu Aircraft Industry Group
Initial Operational Capability (IOC)
2018
First Flight
2017
Total Production
?
Specifications (Deagel)
Crew
2
Number of Engines
1
Propeller Blades
3
Service Life Flight Hours
10000
G-load — Max Maneuvering Load Factor
9 g
G-load — Min Maneuvering Load Factor
-7.00 g
Mass — Fuel Load
200 kilogram
Mass — Max Takeoff Weight
1,320 kilogram
Performance — Ceiling
4,000 meter
Performance — Landing Run Distance
360 meter
Performance — Max Range
1,400 kilometer
Performance — Take Off Run Distance
175 meter
Power — Max Power at TakeOff
360 hp
Speed — Stall Speed
100 kph
Speed — Top Speed at High Altitude
500 kph
Time — Service Life
30 year
Variants
Variant 1
L-7
Variant 2
Yak-152
Details
Country of Origin
China
Sources
deagel.com: https://www.deagel.com/x/x/a002982
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
—
Height
—
Weight
1320 kg
Operators (1)
China
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