nice ppt and important tooo

1. Aircraft Description Seats Max
Launch
date
1st
flight
1st
delivery
Production
to
cease/ceased
A300
2 engine,
twin aisle
228-
254
361 May 1969
28
October
1972
May 1974
Air
France
27 March
2007
A310
2 engine,
twin aisle,
modified
A300
187 279 July 1978
3 April
1982
December
1985
Air
Algerie
27 March
2007
A318
2 engine,
single aisle,
shortened
6.17 m from
A320
107 117
April
1999
15
January
2002
October
2003
Frontier
Airlines
A319
2 engine,
single aisle,
shortened
3.77 m from
A320
124 156 June 1993
25 August
1995
April
1996
Swissair
A320
2 engine,
single aisle
150 180
March
1984
22
February
1987
March
1988
Air Inter
A321
2 engine,
single aisle,
lengthened
6.94 m from
A320
185 220
November
1989
11 March
1993
January
1994
Lufthansa
A330
2 engine,
twin aisle
253-
295
406-
440
June 1987
2
November
1992
December
1993
Air Inter
A340
4 engine,
twin aisle
239-
380
420-
440
June 1987
25
October
1991
January
1993
Air
France
A350
2 engine,
twin aisle
270-
350
December
2006
2011
expected
mid-2013
TAM
A380
4 engine,
double deck,
555 853 2002
27 April
2005
15th
October

2. twin aisle[31]
2007
Singapore
Airlines
Airbus aircraft numbering system
The Airbus numbering system is an alpha numeric model number followed by a dash and a three digit
number.
The model number takes the form of the letter "A" followed by a '3', a digit, then followed normally by a '0'
(except in the case of the A319, A321 and A400M) , e.g. A320. The succeeding three digit number
represents the aircraft series, the engine manufacturer and engine version number respectively. To use an
A320-200 with International Aero Engines (IAE) V2500-A1 engines as an example; The code is 2 for
series 200, 3 for IAE and engine version 1, thus the aircraft number is A320-231.
An additional letter is sometimes used. These include, 'C' for a combi version (passenger/freighter), 'F' for a
freighter model, 'R' for the long range model, and 'X' for the enhanced model.
[edit]Engine codes
Code Manufacturing Company
0 General Electric (GE)
1 CFM International (GE/SNECMA)
2 Pratt & Whitney (P&W)
3
International Aero Engines (R-R, P&W, Kawasaki, Mitsubishi, and
Ishikawajima-Harima)
4 Rolls-Royce (R-R)
6 Engine Alliance (GE and P&W)

3. The aircraft series of airbus
Airbus A300
Olympic Airlines A300B4-600R
Role Airliner
Manufacturer Airbus
First flight 28 October 1972
Introduction 30 May 1974 with Air France
Primary users FedEx Express
UPS Airlines
Japan Airlines
Air France
Produced 1974-2007
Number built 561

4. Variants A300-600ST Beluga
Airbus A310
Measurement A300B4 A300-600R A300-600F
Seats 2-class 266 n/a
Length 54.08 m or 177' 3"
Span 44.85 m or 147' 2"
Height 16.62 m or 54' 6"
Max cabin width 5.28 m
Fuselage diameter 5.64 m
Weight empty 90,060 kg or 198,132 lb 81,900 kg or 180,700 lb
MTOW 165,000 kg or 364,980 lb. 170,500 kg or 375,100 lb
Take-off Run at MTOW N/A 2324 m
Cruising speed mach 0.78
Maximum speed mach 0.86
Range fully loaded 6,670 km or 3,600 nm 2,950 nm
Max. fuel capacity 18,000 USG or 68,150 litres
Engines CF6-50C2 or JT9D-59A CF6-80C2 or PW4158
Cockpit Crew Three Two
Airbus A310
Emirates SkyCargo A310-300
Role Airliner

5. Manufacturer Airbus
First flight 3 April 1982
Introduced April 1983
Primary users FedEx Express
Air India
Air Transat
Pakistan International
Produced 1983-2007
Number built 255
Developed from Airbus A300
Variants A310 MRTT
CC-150 Polaris
The Airbus A310 is a medium to long-range widebody airliner. Launched in 1978, it was
the second aircraft created by the Airbus consortium of European aerospace companies,
which is now fully owned by EADS. The A310 is a shortened derivative of the A300, the
first twin-engined widebody airliner. The A310 (along with the A300) officially ceased
production in July 2007 although the last delivery was in June 1998.
[8]
A310-200 A310-200F A310-300 A310-300F
Crew 2
Length 46.66 m (153 ft 1 in)
Height 15.8 m (51 ft 10 in)
Wingspan 43.9 m (144 ft)
Wing sweep 28 °

6. Cross section 5.64 m (18 ft 6 in)
Passengers (2cl) 240 33t cargo 240 33t cargo
MTOW 141,974 kg (312,342 lb) 164,000 kg (361,600 lb)*
Empty weight
80,142 kg
(176,312 lb)
72,400 kg
83,100 kg
(183,300 lb)
73,900 kg
Max fuel 55,200 l (14,603 US g) 75,470 l (19,940 US g)
Cruise speed
(M)
0.80 (850 km/h.)
Max speed (M) 0.84 (901 km/h.)
Ceiling 12,000 m (40,000 ft)
Thrust (×2) (lb) 50,000-53,200 56,000-59,000
Engines PWJT9D-7R4 or CF6-80C2A2 PW4156A or CF6-80C2A8
Range
6,800 km
(3,670 nm)
Trans-continental
5,550 km
9,600 km
(5,200 nm)
Trans-atlantic
7,330 km
Airbus A320 family

7. Swiss International Air Lines A320-200
Role Narrow-body jet airliner
Manufacturer Airbus
First flight 22 February 1987
Introduced 28 March 1988
Status Active service
Primary users US Airways
United Airlines
Air France
EasyJet
Number built 3,723 as of 31 December 2008[1]
Unit cost A318: US$56.0 to $62.1m (2008)[2]
A319: $63.3 to $77.3m (2008)
A320: $73.2 to $80.6m (2008)
A321: $87.7 to $92.8m (2008)
The Airbus A320 family of short- to medium-range commercial passenger airliners are manufactured
by Airbus. Family members include the A318, A319, A320, and A321, as well as the ACJ business jet.

8. First delivered in 1988, the A320 pioneered the use of digital fly-by-wire flight control systems in a
commercial aircraft. With more than 3,700 aircraft of the A320 family built, it is the second best-selling jet
airliner family of all time after its primary competition, theBoeing 737.
Specifications
Measurement A318-100 A319-100 A320-200 A321-200
Cockpit crew Two
Seating
capacity
117 (1-class)
100 (2-class)
156 (1-class)
124 (2-class)
180 (1-class)
148 (2-class)
220 (1-class)
185 (2-class)
Length
31.45 m (103 ft
2 in)
33.84 m (111
ft)
37.57 m (123
ft)
44.51 m (146
ft)
Wingspan 34.10 m (111 ft 10 in)
Wing
Sweepback
25°
Height
12.56 m (41 ft 2
in)
11.76 m (38 ft 7 in)
Cabin Width 3.70 m (12 ft 1 in)
Fuselage
Width
3.95 m. (13 ft)
Typical empty
weight
39,300 kg
(86,650 lb)
40,600 kg
(89,950 lb)
42,400 kg
(93,500 lb)
48,200 kg
(106,300 lb)
Maximum 68,000 kg 75,500 kg 77,000 kg 93,500 kg

9. take-off weight (149,900 lb) (166,500 lb) (169,000 lb) (206,100 lb)
Cruising speed Mach 0.78
Max. speed Mach 0.82
Take off run
at MTOW
1,355 m (4,446
ft)
1,950 m (6,398
ft)
2,090 m (6,857
ft)
2,180 m (7,152
ft)
Range fully
loaded
5,950 km or
3,250 nmi
(6,020 km)
6,800 km or
3,700 nmi
(6,900 km)
5,700 km or
3,000 nmi
(5,600 km)
5,600 km or
3,000 nmi
(5,600 km)
Max. fuel
capacity
23,860 litres or
6,300 US gal
29,840 litres or
7,885 US gal
29,680 litres or 7,842 US gal
Service Ceiling 39,000 ft (12,000 m)
Engines
2 × PW6122A
2 × CFM56-5
2 × IAE V2500
2 × CFM56-5
Source: Airbus
Airbus A330

10. Northwest Airlines A330-300
Role Wide-body jet airliner
Manufacturer Airbus
First flight 2 November 1992
Introduced January 1994 with Air Inter
Primary users Northwest Airlines
Qatar Airways
Emirates
Cathay Pacific
Number built 587 as of 31 December 2008 [1]
Unit cost A330-200: US$176.3 to $185.5m (2008)[2]
A330-300: $195.9 to $205.7m (2008)
A330-200F: $180.6 to $187.7m (2008)
Developed from Airbus A340
Variants Airbus A330 MRTT
Northrop Grumman KC-45
The Airbus A330 is a large-capacity, wide-body, twin-engine, medium-to-long-range commercial
passenger airliner. It was developed at the same time as the four-engined Airbus A340.
Airbus A340

11. A Cathay Pacific A340-600 landing at London Heathrow Airport
Role Airliner
Manufacturer Airbus
First flight 25 October 1991
Introduced March 1993 (delivery began in January 1993)
Status Active Service
Primary users Lufthansa
Iberia Airlines
Virgin Atlantic Airways
South African Airways
Number built 361 as of 31 October 2008 [1]
Unit cost A340-200: $87,000,000 (1989)
A340-300: $211.8 to $219.2m (2008)[2]
A340-500: $233.0 to $241.1m (2008)[2]
A340-600: $245.0 to $253.7m (2008)[2]
Variants Airbus A330
the Airbus A340 is a long-range four-engined wide-body commercial passenger airliner manufactured
by Airbus, a subsidiary ofEADS. It seats between 261 and 380 passengers, and has a range between 6,700
and 9,000 NM. It is similar in design to the twin-engined A330. Initial A340 versions share
the fuselage and wing of the A330 while later models are longer and have larger wings.
Measurement A340-200 A340-300
A340-500/-
500HGW
A340-600/-
600HGW
Cockpit crew Two
Seating
capacity
261 (3-class) 295 (3-class) 313 (3-class) 380 (3-class)
Length
59.39 m
194 ft 10 in
63.60 m
208 ft 8 in
67.90 m
222 ft 9 in
75.30 m
247 ft 0 in
Wingspan
60.30 m
197 ft 10 in
63.45 m
208 ft 2 in
Wing
Sweepback
30° 31.1°
Height
16.70 m
54 ft 9 in
16.85 m
55 ft 3 in
17.10 m
56 ft 1 in
17.30 m
56 ft 9 in

12. Cabin Width 5.28 m (17.3 ft)
Wheelbase
23.24 m
76 ft 3 in
25.60 m
84 ft 0 in
27.59 m
90 ft 6 in
32.89 m
107 ft 11 in
Typical empty
weight
129,000 kg
284,396 lb
129,275 kg
295,503 lb
170,400 kg
375,668 lb
177,000 kg
390,218 lb
Maximum
take-off
weight
275,000 kg
606,300 lb
276,500 kg
609,600 lb
372,000/380,000 kg
820,100 /837,800 lb
368,000/380,000 kg
811,300/837,800 lb
Cruising speed
Mach 0.82 (896 km/h, 484 knots,
557 mph)
Mach 0.83 (907 km/h, 490 knots,
564 mph)
Take off run
at MTOW
2,990 m
9,810 ft
3,000 m
9,840 ft
3,050 m
10,000 ft
3,100 m
10,170 ft
Range fully
loaded
14,800 km
8,000 NM
13,700 km
7,400 NM
16,020/16,700 km
8,650/9,000 NM
14,360/14,630 km
7,750/7,900 NM
Max. fuel
capacity
155,040 L
40,957 gal
140,640 L
37,153 gal
214,810/222,000 L
56,750/58,646 gal
195,881/204,500 L
51,746/54,023 gal
Cargo capacity
18 LD3s/6
pallets
30 LD3s/10
pallets
32 LD3s/11 pallets 42 LD3s/14 pallets
Service
Ceiling
11,887 m (39,000 ft)
Engines (4x)
CFM56-5C2 (1
38.78kN)
CFM56-5C3
(144.57kN)
CFM56-5C4
(151.25kN)
CFM56-5C2 (1
38.78kN)
CFM56-5C3
(144.57kN)
CFM56-5C4
(151.25kN)
CFM56-5C4P
(149.9kN)
Rolls-Royce Trent
553/556
(236/249kN)
Trent 556/560
(249/260kN)
Airbus A350

13. Airbus A350 XWB concept
Role Wide-body jet airliner
Manufacturer Airbus
First flight 2011 (scheduled)
Introduction 2013 (scheduled)
Status Under development
Unit cost A350-800 - $208.7 million
A350-900 - $240.6 million
A350-1000 - $269.6 million[1]
The Airbus A350 is a long range, mid-sized, wide-body family of airliners currently under development.
The A350 will be the first Airbus with fuselage and wing structures made primarily of carbon fiber
reinforced plastic.[2]
The A350 is designed to compete with the Boeing 777 and the Boeing 787 and Airbus
claims that it will be more fuel-efficient and with up to 8% lower operating cost than the Boeing 787.[2][3]
It
is scheduled to enter into airline service in 2013.
Model A350-800 A350-900 A350-1000
Cockpit
crew
Two
Passengers
270 3-class
312 2-class
314 3-class
366 2-class
350 3-class
412 2-class
Length 60.7 m (199 ft) 67 m (220 ft) 74 m (240 ft)
Wingspan 64.8 m (213 ft)
Wing area 443 m2
(4,770 sq ft)
Wing
sweepback
31.9°
Height 16.9 m (55 ft)
Fuselage
width
5.96 m (19.6 ft)
Cabin
width
5.59 m (220 in)
Cargo
capacity
28 LD3 36 LD3 44 LD3
Maximum
takeoff
weight
248 t (547,000 lb) 268 t (590,838.9 lb) 298 t (656,977.5 lb)

14. Cruise
speed
Mach 0.85 (903 km/h, 561 mph, 487 knots, at 40,000 ft/12.19 km)
Maximum
cruise
speed
Mach 0.89 (945 km/h, 587 mph, 510 knots, at 40,000 ft/12.19 km)
Range,
loaded
15,400 km (8,320 nmi) 15,000 km (8,099 nmi) 14,800 km (7,990 nmi)
Maximum
fuel
capacity
129,000 l (34,100 US gal
)
138,000 l (36,456 US gal
)
156,000 l (41,200 US gal)
Service
ceiling
43,100 ft (13.1 km) 41,450 ft (12.6 km)
Engines
(2×)
RR Trent XWB
Maximum
thrust
capability
74,000 lbf (329 kN) 83,000 lbf (369 kN) 92,000 lbf (409 kN)
Airbus A380
An Airbus 380 in Emirates Airline colors at the Dubai Air Show
Role Airliner
Manufacturer Airbus
First flight 27 April 2005
Introduced 25 October 2007 with Singapore Airlines

15. Primary users Singapore Airlines
Emirates Airline
Qantas
Produced 2004 – present
Number built 23 as of January 2009[1]
Unit cost US$317.2-337.5 million[2]
The Airbus A380 is a double-deck, wide-body, four-
engine airliner manufactured by the European corporation Airbus,
an EADSsubsidiary. The largest passenger airliner in the world, the A380
made its maiden flight on 27 April 2005 from Toulouse, France,[3]
and made
its first commercial flight on 25 October 2007
from Singapore to Sydney with Singapore Airlines. The aircraft was known
as the Airbus A3XX during much of its development phase, but
the nickname Superjumbo has since become associated with it.
The A380's upper deck extends along almost the entire length of
the fuselage, and its width is equivalent to that of a widebody aircraft. This
allows for a cabin with 50% more floor space than the next-largest airliner,
the Boeing 747-400.[4]
and provides seating for 525 people in standard three-
class configuration[5][6]
or up to 853 people in all economy
class configurations.[7]
The A380 is offered in passenger and freighter
versions. The A380-800, the passenger model, is the largest passenger
airliner in the world, but has a shorter fuselage than the Airbus A340-600,
which is Airbus's next-biggest passenger aeroplane. The A380-800F, the
freighter model, is offered as one of the largest freight aircraft, with a listed
payload capacity exceeded only by the Antonov An-225.[8]
The A380-800
has a design range of 15,200 km (8,200 nmi), sufficient to fly
from Boston to Hong Kong for example, and a cruising speed of Mach 0.85
(about 900 km/h or 560 mph at cruising altitude).[5]
It is the first commercial
jet capable of using GTL-based fuel.
Specifications

16. Measurement A380-800 A380-800F
Cockpit crew Two
Seating capacity
525 (3-class)[5]
644 (2-class)
853 (1-class)
12 couriers
Length 73 m (240 ft)
Span 79.8 m (262 ft)
Height 24.1 m (79 ft)
Wheelbase 30.4 m (100 ft)
Outside fuselage width 7.14 m (23.4 ft)
Cabin width
6.58 m (21.6 ft) for Main deck
5.92 m (19.4 ft) for Upper deck
Wing area 845 m2
(9,100 sq ft)
Wing sweep 33.5°
Operating empty
weight
276,800 kg (610,000 lb) 252,200 kg (556,000 lb)
Maximum take-off
weight
560,000 kg (1,200,000 lb) 590,000 kg (1,300,000 lb)

17. Maximum payload 90,800 kg (200,000 lb) 152,400 kg (336,000 lb)
Cruising speed
Mach 0.85
(1041 km/h, 647 mph, 562 knots)
Maximum cruising
speed
Mach 0.89
(1090 km/h, 677 mph, 588 knots)
Maximum speed
Mach 0.96[113]
(1176 km/h, 731 mph, 635 knots)
Take off run at MTOW 2,750 m (9,000 ft)[87]
2,900 m (9,500 ft)[87]
Range at design load
15,200 km (8,200 nmi,
9,400 mi)
10,400 km (5,600 nmi, 6,400 mi)
Service ceiling 13,115 m (43,030 ft)[114]
Maximum fuel capacity
310,000 l
(81,890 US gal,
68,200 imp gal)
310,000 l
(81,890 US gal, 68,200 imp gal),
356,000 l
(94,000 US gal, 78,300 imp gal)
option
Engines (4 x)
GP7270 (A380-861)
Trent 970/B (A380-841)
Trent 972/B (A380-842)
GP7277 (A380-863F)
Trent 977/B (A380-843F)
Thrust (4 x) 311 kN (70,000 lbf)