AN26
ANTONOV An-26
ANTONOV An-26
Aircraft
Name
An-26
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
XIAN Y-7H
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 (metric)
29.90 m
Length (metric)
23.80 m
Height (metric)
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(s)
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
