*****AIRCRAFT “Antonov
- AN26”*****
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: High wing
Engine
position: (Front) Wing leading mounted
Tail
configuration: Regular tail, high set
Landing
gear: Tricycle retractable
Wing
Span:
Length:
Height:
Power
plant: 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.
Accommodation:
Crew of 5 (Pilot, Co-pilot,radio operator, navigator and flight engineer) and up
to 40 troops or 24 patients.
Notes: 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.
Alternative names:
ANTONOV An-26,
XIAN Y-7H, Y-7H.
*****Total Flight Simulator aircraft weight
with full fuel*****
VMO -
Maximum Operating Speed 235 KIAS
MMO -
Maximum Operating Speed Mach nd Mach
Turbulent
Air Penetration Speed 000 KIAS/.00 Mach
VLO -
Maximum Gear Operating Speed 000 KIAS
VLE -
Maximum Landing Gear Extension Speed
000 KIAS/.00 Mach
*****Maximum Flap Placard Speeds*****
Flaps
degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 1200 mt
V2
(IAS): 120 kts
*****Climbing*****
-(to
IAS: 150 kt
ROC: 1500 ft/min
-(to
FL150)
IAS: 200 kt
ROC: 1000 ft/min
-(to
FL240)
IAS: 200 kt
ROC: 800 ft/min
-(mach)
mach: na
ROC: na ft/min
*****Cruise*****
TAS: 235 kt
MACh: nd
Ceiling: FL260
Range: 600 NM
*****Descent *****
- (to
FL240)
mach: nd
ROD: nd ft/min
- (to
FL100)
IAS: 240 kt
ROD: 1500 ft/min
*****Approach*****
IAS: 240 kt
MCS: 170 kt
ROD: 1500 ft/min
*****Landing*****
Vht
(IAS): 105 kt
APC: B
Distance: 700 mt