ANTONOV An-26
ANTONOV An-26
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