ANTONOV An-24

Aircraft
Name: 
An-24
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Tail: 
Regular tail, high set
WTC
M
APC
B
Type Code: 
L2T
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
ANTONOV An-24
XIAN Y-7-100
XIAN Y-7-200
XIAN Y-7E

AN24

Regional airliner and freighter. In service since 1963. Original aircraft of the Antonov family of twin turboprop civil and military transports. Developed to AN-26, An30, AN32. Chinese version Y-7 series. More than 1100 An-24s were built. Approximately 880 remain in commercial service. Ukrainian production ceased in 1978, Chinese production continues.

Technical Data
Wing span: 
29.20 m
Length: 
23.50 m
Height: 
8.30 m
Powerplant: 

An24: 2 x 2.550 SHP Ivchenko AI-24A turboprops with 4 blade propellers.

Engine Model: 
Dongan WJ5, Ivchenko AI-24
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
1750 m
MTOW: 
21000 kg
Initial Climb (to 5000 ft)
IAS: 
200 kts
ROC: 
1000 ft/min
Initial Climb (to FL150)
IAS: 
230 kts
ROC: 
300
Initial Climb (to FL240)
IAS: 
180 kts
ROC: 
1000 ft/min
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
242 kts
MACH: 
n/a
Ceiling: 
275
Range: 
1700 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
240 kts
ROD: 
1000 ft/min
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
1590 m

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