Factsheet.pdf

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BAC / Aérospatiale
Developed in the 1960s and beginning service in 1976, the graceful
Concorde travelled at over twice the speed of sound and could fly its
passengers across the Atlantic in as little as three hours. 14 aircraft in
total entered commercial service with British Airways and Air France.
The Concorde fleet was grounded in 2000 following the crash of an
Air France flight, but resumed flying the following year after safety
improvements. In 2003 both airlines withdrew Concorde from
service because of rising operating costs, and the surviving aircraft are
now displayed in museums across Europe and North America.
Capacity:
approx. 100 passengers (varies with seat layout)
Flight crew:
Two pilots, one flight engineer
Cabin crew:
Six
Range
(with typical payload)
:
6,580 km (4,090 miles)
Engines:
Four Rolls-Royce/SNECMA Olympus 593,
each producing 38,000 lbs thrust with reheat
Take-off speed:
397 km/hr (246 mph)
Cruising speed:
Mach 2.04 (2,150 km/hr or 1,350 mph)
Landing speed:
300 km/hr (187 mph)
Service ceiling:
18,290 m (60,000 ft)
Length:
61.7 m (202 ft 4 in)
Wingspan:
25.56 m (83 ft 10 in)
Height:
12.2 m (40 ft 0 in)
Fuel capacity:
119,500 litres (26,290 Imp. gallons)
Fuel consumption
: 25,629 litres (5,638 Imp. gallons) per hour
Maximum take-off weight:
185 tonnes (408,000 lb)
Landing gear:
Eight main wheels, two nose wheels
Concorde
Droop nose positions
0°
(visor up)
Used during supersonic
cruise and when parked
0°
(visor down)
Used during subsonic cruise
5°
(visor down)
Used during taxiing and take off
12.5°
(visor down)
Used during landing and taxiing
DANGER
DANGER
RAMPS WILL BE OPERATIVE
DURING SYSTEM TESTING
DO NOT USE FOR ACCESS
LES RAMPES PEUVENT
FONCTIONNER PENDENT LES
ESSAIS DU SYSTEME, NE PAS
UTILISER COMME ACCES
LES RAMPES PEUVENT
FONCTIONNER PENDENT LES
ESSAIS DU SYSTEME, NE PAS
UTILISER COMME ACCES
DANGER
NOT TO BE USED AS AN
ACCESS. THIS FLAP WILL
BE OPERATIVE DURING
SYSTEM TESTING
NO STEP
SORTIE EXIT
SORTIE EXIT
TO
FULLY
DEPRESS
TO
FULLY
DEPRESS
DANGER
RAMPS WILL BE OPERATIVE
DURING SYSTEM TESTING
DO NOT USE FOR ACCESS
NE PAS UTILISER COMME
ACCES. CE VOLET PEUT
FONCTIONNER PENDENT
LES ESSAIS DU SYSTEME
NOT TO BE USED AS AN
ACCESS. THIS FLAP WILL
BE OPERATIVE DURING
SYSTEM TESTING
NE PAS UTILISER COMME
ACCES. CE VOLET PEUT
FONCTIONNER PENDENT
LES ESSAIS DU SYSTEME
TO OPEN
FULLY
DEPRESS
SORTIE EXIT
ATTENTION
ICI
ENREGISTREUR
DE VOL
CAUTION
FLIGHT
RECORDER
HERE
NO
STEP
OVERPRESSURE
O2
STATIC PORTS DO NOT
PLUG OR DEFORM HOLES
AREA INDICATED
MUST BE SMOOTH,
CLEAN AND FREE OF ICE.
PRISES DE PRESSION NE PAS
BRANCHEZ OU DEFORMEZ
PAS LES TROUS.
LE SECTEUR INDIQUE DOIT
ETRE LISSE ET PROPRE.
SURPRESSION
O2
CREW O2
ROLLS
ROLLS ROYCE – SNECMA
OLYMPUS 593
ROYCE
0
Metres
Feet
10
10
50
20
30
100
40
Scale 1:360
concorde_factsheet.pdf
© 2006 by Ralph Currell
http://www.currell.net
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