Reference ChartsFuel Transfer ProceduresFlight Info

CONCORDE SSTSIM -- B38

ROUTE INFORMATION

For detailed instructions on how to fly this aircraft, see the Aircraft Operation Manual
and Simulator Tutorial documents located in the aircraft’s folder.

Technical Specifications:

Cruise Chart:

Descent and Landing Charts:

Performance
Maximum Operation Cruise SpeedMach 2.04 (1350 mph)
Maximum Permissable Range4500 miles (3900 nm)
Average Take-Off Speed250 mph
Average Landing Speed185 mph
Maximum Landing Gear Speed270 kts
Maximum Operating Altitude60,000 ft
Maximum Visor Down Speed325 kts
Maximum Nose Down 5° Speed325 kts
Maximum Nose Down 12.5° Speed270 kts below FL200
Maximum Fuel Jettison Speed Mach0.93
Maximum Total Air Temp (TMO)127° C (Nose)

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Weights
Max Zero Fuel Weight203,000 lbs (92,080 kgs)
Operating Weight Empty173,500 lbs (78,700 kgs)
Max Payload29,500 lbs (13,380 kgs)
Max Take-Off Weight408,000 lbs (185,000 kgs)
Max Taxi Weight412,000 lbs (186,880 kgs)
Max Landing Weight245,000 lbs (111,130 kgs)
Max Weight of Fuel26,400 gal (95,680 kgs)

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Powerplant
Engine ModelOlympus 593 Mrk610 turbojet
Engine ManufacturerRolls-Royce/SNECMA
Max thrust at TO (per engine)38,050 lbs (w/ afterburner)
Max thrust at supersonic cruse (per engine)10,000 lbs
Fuel TypeA1 Jet fuel
Fuel Capacity26,400 gal /95,680 kgs
Fuel Consumption (at Idle Power)1100 kgs/hr (302 Gallons/hr)
Fuel Consumption (at Full Power)10500 kgs/hr (2885 Gallons/hr)
Fuel Consumption (at Full Re-heated power)22500 kgs/hr (6180 Gallons/hr)

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Cruise/Climb Performance Chart
ISA-30-20-15-10-50+5+10+15
FL600125115110105100095095--
FL580135125120115110105100095-
FL560150135130125120115115105095
FL540165150145135130130125115105
FL520165165160150145140135130115

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CONSTANT ALTITUDE DECELERATION AND DESCENT
ISA + 5° C AND ABOVE
 DISTANCE COVERED
(nm)
FLIGHT
LEVEL
MEAN
TAS
(kts)
FUEL
(kg)
TIME
(min)
50 KT
HEAD
ZERO
WIND
50 KT
TAIL
600618269019174189204
580609263019172186201
560603257018169184198
540597255018166180194
520590253018161174188
500579251017155167181
480564243017143155168
46047018501391101110
4504671820138998107
4304561770128392101
410445172012788695
390438167011738189
370430162011697684
350418158010657179
330410155010616775
31040615209576369
29040014909525864
27039514608485459
25038214308444954
23037514007404550
21036713707374145
19036413406333741
17035413006303337
15034112705272932
13032612405232528
11032212104202224
10031611904192022
903771202111214
703729018910
50367601567
30362201223
* Lookup current altitude then lookup descent altitude
* Subtract the two figures to obtain descent distance
* Add the difference between ISA and +5° C. Add this figure to the decsent distance obtained in the previous step.

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CONSTANT ALTITUDE DECELERATION AND DESCENT
TO FL410 AND M1.00
ISA + 5° C AND ABOVE
PROCEDURE:
DECELERATE TO 35O KT IAS
AT 350 KT IAS, DESCEND TO FL410
DECELERATE AT CONSTANT ALTITUDE TO M1.00
FLIGHT
LEVEL
FUEL
(kg)
TIME
(min)
MEAN
TAS
(kts)
DISTANCE COVERED (nm)
TAILWIND (kts) HEADWIND (kts)
10080604020SA20406080100
6009507.885312312111811611411110810610210097
5909407.78541211181161141121091071041019896
5809307.6846119116114112110107105102999694
5709007.4848116114111110108105103100979592
5609007.483811411210910810610310199969391
5509107.383711311010810710510210098959390
5409107.28431111091071051031019896949290
5309007.0842108106104102100989693918987
5208906.88401051031019997959391898785
5108806.683810199989694929088868482
5008706.38409896949290888685838179
4908305.98369189878684828079777573
4807805.68168482817978767473716968
4707405.28107876757372706967666463

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AUTOLAND MAX WINDS
HEAD25 kts
TAIL10 kts
CROSS15 kts

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LANDING VREF SPEEDS
LANDING
WEIGHT (kg)
VREF
96 ...................................... 150
98 ...................................... 152
100 ...................................... 154
102 ...................................... 155
104 ...................................... 157
106 ...................................... 158
108 ...................................... 160
110 ...................................... 161
111 ...................................... 162
115 ...................................... 165
120 ...................................... 168
125 ...................................... 172
130 ...................................... 175
135 ...................................... 179
140 ...................................... 182
145 ...................................... 185
150 ...................................... 188
155 ...................................... 191
160 ...................................... 194
165 ...................................... 197
170 ...................................... 201
175 ...................................... 204
180 ...................................... 207