ANTONOV An-26

Aircraft
Name: 
An-26
Manufacturer: 
ANTONOV
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-26
XIAN Y-7H

AN26

Military tactical transport aircraft. In service since 1968. More powerful development of An-24 with rear loading ramp and redesigned tail for military use. Chinese versions Y-7 and Y-7H. Civil version An-26S. In production from 1968 to 1985. Over 550 An-26s are in world wide civil service.

Technical Data
Wing span: 
29.90 m
Length: 
23.80 m
Height: 
8.60 m
Powerplant: 

2 x 2.820 SHP Ivchenko AI 24VT turboprops with 4 blade propellers and 1 x 8.83 kN RU 19-300 aux turbojet in starboard nacelle.

Engine Model: 
Ivchenko AI-24
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
1240 m
MTOW: 
n/a
Initial Climb (to 5000 ft)
IAS: 
200 kts
ROC: 
1000 ft/min
Initial Climb (to FL150)
IAS: 
200 kts
ROC: 
800
Initial Climb (to FL240)
IAS: 
200 kts
ROC: 
400 ft/min
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
214 kts
MACH: 
n/a
Ceiling: 
275
Range: 
1700 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
1740 m

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