*****AIRCRAFT “Antonov
- AN24”*****
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 2.550 SHP Ivchenko AI 24A turboprops with
4 blade
Propellers.
Y-7: 2 x 2.790 SHP Wongan
WJ5A I turboprops with 4 blade
propellers.
Accommodation:
Flightcrew of 4 and up to 50 passengers.
Notes: 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,
-30, - 32. 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.
Alternative names:
ANTONOV An-24,
XIAN Y-7-100/200,Y-7E, Y-7-100/200,Y-7E, Y-7E.
*****Total Flight Simulator aircraft weight
with full fuel*****
VMO -
Maximum Operating Speed 240 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: 900 mt
V2
(IAS): 110 kts
*****Climbing*****
-(to
IAS: 140 kt
ROC: 1500 ft/min
-(to
FL150)
IAS: 200 kt
ROC: 1000 ft/min
-(to
FL240)
IAS: 200 kt
ROC: 1000 ft/min
-(mach)
mach: na
ROC: na ft/min
*****Cruise*****
TAS: 240 kt
MACh: nd
Ceiling: FL280
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): 120 kt
APC: B
Distance: 900 mt