***AIRCRAFT “Caravelle III - Sud Aviation”**
REFERENCE INFORMATION (by others and wikipedia)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage mounted
Tail configuration: T tail
Landing gear: Tricycle retractable
Wing Span: see table for models
Length: see table for models
Height: see table for models
Power plant: see table for models
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 46.000-50.000 kg
VMO - Maximum Operating Speed 805-850 km/h 437 kts
MMO - Maximum Operating Speed Mach 0.77 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
*****
Technical specs *****
models III VI-N VI-R 10R 11R
10B 12
year 1959 1960 1961 1965 1967 1964 1970
pilots 3 3 3 3 3 3 3
passengers 80
80 80 80 89-99 105 140
Lenght m 31,01 31,01 31,01 31,01 32,71 33,01 36,24
wing spam m 34,3 34,3 34,3 34,3 34,3 34,3 34,3
height m 8,72 8,72 8,72 8,72 8,72 8,72 9,
02
wing surf m˛ 146,7
146,7 146,7 146,7 146,7 146,7 146,7
empty mass t 22,2 24,9 26,3
26,7 28,8 28,8 29,5
payload t 8,4 7,9 8,2 9,1 9,4 9,4 -
MTOW t 46 48 50
52 52 52 58
speed km/h 805
845 845 800 800 800 800
kts 434 456 456 432 432 432 432
mach 0.65 0.68 0.68 0.64 0.64 0.64 0.64
flight range km1700 2350
2300 2300 2300 3455 3465
Nmls 918 1269 1242 1242 1242 1865 1871
Motori RR Avon RR Avon
RR Avon P&W P&W
P&W P&W
Mk527
Mk531 Mk533RJT8D-7 JT8D-7 JT8D-7 JT8D-9
Flight Level m 12000 12000 12000 12000 12000 12000 12000
FL feetx100 390 390 390 390 390 390 390
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
0-10° 223
never
exceed 258
10-20° 175
never
exceed 202
20-35° 164
never
exceed 190
Landing gear operating speed
(Max speed for retraction/extension) :
VLO 180
kt
Landing gear extension speed
(Max speed for operation with gear extended and
locked) :
VLE 218
kt
Speed brakes
extended speed No
limitation up to VNE
Landing lights
extension speed 215
kt
Parachute deployment speeds
Normal
operating limit 115
kt
Never exceed
exeptional airspeed 130 kt
Max cross-wind
component 20
kt
*****
Operational limitations *****
ALTITUDE :
Take-off & landing limits -500 to 8300 ft
Max operating altitude
(passengers) 39300
ft
Max cabin differential pressure 8.10 psi
TEMPERATURE :
Take-off & landing -35°
to ISA + 35° C
En route limits -71.5°
to ISA + 35° C
WIND (for take-off & landing) :
Limiting tail wind component 10 kt
Max crosswind
(take-off & landing) 34 kt at 50 ft
*****Take-off*****
WTC:
Distance: 1830-1980
mt
V2 (IAS): 000
kts
Operating limitations RPM :
8000
to 8100 rpm (5 min. max)
Overspeed 8400 rpm
*****Climbing*****
climb rate 11.20
m/s 672 m/min
37
ft/s 2184 ft/min
-(to 5000 ft)
IAS: 250
kt
ROC: 2000
ft/min
-(to FL150)
IAS: 000
kt
ROC: 000
ft/min
-(to FL240)
IAS: 000
kt
ROC: 000
ft/min
-(mach)
mach: 000
ROC: 000
ft/min
*****Cruise*****
TAS: 432-456
kt
never
exceed 454-478 kt
MACh: 0.64-0.68 data
never
exceed 0.67-0.72 data
Ceiling: FL390
Range: 918-1871
NM
Operating limitations RPM :
Max contin 7750 rpm
Overspeed 8400 rpm
*****Descent
*****
- (to FL240)
mach: 000
ROD: 000
ft/min
- (to FL100)
IAS: 000
kt
ROD: 000
ft/min
*****Approach*****
IAS: 000
kt
MCS: 000
kt
ROD: 000
ft/min
Operating limitations RPM :
Min approach 4600
rpm
*****Landing*****
Vht
(IAS): 160 kt
APC: 0
Distance: 1800-1900
mt