*********10********20********30********40********50********60
*****AIRCRAFT
“NAMC - YS-11A”*****
REFERENCE INFORMATION (by Wikipedia)
*****notes*****
Il NAMC
YS-11 è un aereo di linea turboelica costruito dal
consorzio giapponese Nihon Aircraft Manufacturing Corporation.
Il
progetto fu varato dal locale Ministero del Commercio
Internazionale
e dell'Industria nel 1954.
Il primo
aeromobile uscì di fabbrica nel 1962 e la produzione
cessò nel 1974.
*****Aircraft
Features*****
Wing position: low
Engine position:
Tail configuration:
Landing gear:
Wing Span: 32,0 m (105 ft 0 in)
Length: 26,3 m (86 ft 3 in)
Height: 8,99 m (29 ft 6 in)
Power plant: 2 turboeliche
Rolls-Royce Dart Mk.542-10K
3.099 CV (3.060 hp, 2.280 kW)
Flightcrew of
two and typical 64 passengers, up to 64 in high density configuration.
*****Total
Flight Simulator aircraft weight with full fuel*****
max 51.808 lbs - 23.500 kg
VMO - Maximum Operating Speed 000 KIAS
MMO - Maximum Operating Speed Mach .00 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: .
Distance: 0000
mt
V2 (IAS): 000
kts
*****Climbing*****
Climb rate 6,2
m/s (1.220 ft/min)
-(to 5000 ft)
IAS: 000
kt
ROC: 0000
ft/min
-(to FL150)
IAS: 000
kt
ROC: 0000
ft/min
-(to FL240)
IAS: 000
kt
ROC: 0000
ft/min
-(mach)
mach: 0.00
ROC: 0000
ft/min
*****Cruise*****
TAS: 454
km/h (282 mph, 245 kt)
MACh: no data
Ceiling: 6.982
m (22.900 ft)
Range: 454 km/h (282 mph, 245 kt)
*****Descent
*****
- (to FL240)
mach: 0.00
ROD: 0000
ft/min
- (to FL100)
IAS: 000
kt
ROD: 0000
ft/min
*****Approach*****
IAS: 000
kt
MCS: 000
kt
ROD: 0000
ft/min
*****Landing*****
Vht
(IAS): 000 kt
APC: .
Distance: 0000
mt