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Boeing 777 Boeing
777
Long-Range Jetliner

DESCRIPTION:
What eventually became the 777 project began when several airlines expressed a desire for an airliner with a capacity in between the 767-300 and 747-400. The 777 is designed for both intercontinental and transcontinental routes and is targeted primarily at the Pacific rim market. The overall design is typical of previous Boeing airliners except it is equipped with only two engines, unlike the transcontinental 707 and 747.
To achieve flight certification on such a design, Boeing had to ensure new levels of reliability in engines, avionics, and a fly-by-wire control system as well as the ability to maintain level flight for three hours even with one engine inoperative. Like the 747, the 777 includes three powerplant options depending on airline preference, and these air-breathing engines are the most powerful ever fitted to any aircraft. To give some idea of the size of the 777, the engine nacelles are nearly as wide as the fuselage of the 737. However, some airlines requested the large airliner be able to use the passenger gates designed for the DC-10 and smaller aircraft, so the outer wing panels are designed to fold upward on some models.
Five major variants of the 777 have been designed to date. Base models are the 727-200 and stretched 777-300, and serveral extended and long range models have also been developed. At least 700 aircraft had been built by early 2008.
Last modified 15 July 2008

HISTORY:

First Flight (777-200) 12 June 1994
(777-200ER) 7 October 1996
(777-200LR) 8 March 2005
(777-300) 16 October 1997
(777-300ER) 24 February 2003
(777F) 14 July 2008

Service Entry

(777-200) 7 June 1995 (with United Airlines)
(777-200ER) 9 February 1997 (with British Airways)
(777-200LR) February 2006 (with Pakistan International Airlines)
(777-300) 27 May 1998 (with Cathay Pacific Airways)
(777-300ER) 10 May 2004 (with Air France)

CREW: two flight crew: pilot, co-pilot

PASSENGERS: (777-200) 305 in three classes, 400 in two classes, 440 in one class
(777-200ER) 301 in three classes, 400 in two classes, 440 in one class
(777-200LR) 301 in three classes
(777-300) 386 in three classes, 451 in two classes, 550 in one class
(777-300ER) 365 in three classes

ESTIMATED COST:

(777-200LR) $231 to $256.5 million [2007$]
(777-300ER) $250 to $279 million [2007$]

AIRFOIL SECTIONS:

Wing Root unknown

Wing Tip

unknown

DIMENSIONS:

Length (777-200) 209.08 ft (63.73 m)
(777-200ER) 209.08 ft (63.73 m)
(777-200LR) 209.08 ft (63.73 m)
(777-300) 242.33 ft (73.93 m)
(777-300ER) 242.33 ft (73.93 m)

Wingspan (777-200) 199.92 ft (60.93 m)
(777-200ER) 199.92 ft (60.93 m)
(777-200LR) 212.58 ft (64.86 m)
(777-300) 199.92 ft (60.93 m)
(777-300ER) 212.58 ft (64.86 m)

Height (777-200) 60.75 ft (18.51 m)
(777-200ER) 60.75 ft (18.51 m)
(777-200LR) 60.92 ft (18.58 m)
(777-300) 60.75 ft (18.51 m)
(777-300ER) 60.92 ft (18.58 m)

Wing Area (777-200) 4,605 ft² (427.8 m²)

Canard Area

not applicable

WEIGHTS:

Empty (777-200) 298,900 lb (135,580 kg)

Normal Takeoff unknown

Max Takeoff (777-200) 545,000 lb (247,210 kg)
(777-200ER) 656,000 lb (297,824 kg)
(777-200LR) 750,000 lb (340,195 kg)
(777-300) 660,000 lb (299,370 kg)
(777-300ER) 750,000 lb (340,195 kg)

Fuel Capacity internal:
(777-200) 31,000 gal (117,340 L)
(777-200ER) 45,220 gal (171,170 L)
(777-200LR) 51,590 gal (195,285 L)
(777-300) 45,220 gal (171,170 L)
(777-300ER) 47,890 gal (181,280 L)
external: not applicable

Max Payload

unknown

PROPULSION:

Powerplant (777-200) two Pratt & Whitney PW4077 turbofans
or two Rolls-Royce Trent 877 turbofans
or two General Electric GE90-77B turbofans
(777-200ER) two Pratt & Whitney PW4084/PW4090 turbofans
or two Rolls-Royce Trent 884/892/895 turbofans
or two General Electric GE90-85B/92B/94B turbofans
(777-200LR) two General Electric GE90-110B1 turbofans
(777-300) two Pratt & Whitney PW4098 turbofans
or two Rolls-Royce Trent 892 turbofans
(777-300ER) two General Electric GE90-115B turbofans

Thrust (777-200) 77,200 lb (343 kN) [P&W]
(777-200) 76,000 lb (338 kN) [RR]
(777-200) 77,000 lb (342 kN) [GE]
(777-200ER) 90,200 lb (401 kN) [P&W]
(777-200ER) 93,400 lb (415 kN) [RR]
(777-200ER) 93,700 lb (417 kN) [GE]
(777-200LR) 110,000 lb (489 kN)
(777-300) 98,00 lb (435 kN) [P&W]
(777-300) 90,000 lb (400 kN) [RR]
(777-300ER) 115,000 lb (512 kN)

PERFORMANCE:

Max Level Speed at altitude: 575 mph (930 km/h) at 35,000 ft (10,675 m), Mach 0.87
at sea level: unknown
cruise speed: 560 mph (900 km/h) at 35,000 ft (10,675 m), Mach 0.84

Initial Climb Rate unknown

Service Ceiling 43,100 ft (13,135 m)

Range (777-200) 5,210 nm (9,650 km)
(777-200ER) 7,730 nm (14,315 km)
(777-200LR) 9,420 nm (17,445 km)
(777-300) 5,950 nm (11,030 km) (777-300ER) 7,175 nm (13,290 km)

g-Limits unknown

KNOWN VARIANTS:

777-200 First production model originally designated 777-200A; 76 built by 2001

777-200ER Extended range model originally designated 777-200B or 777-200IGW (Increased Gross Weight) with greater fuel capacity and uprated engines; 203 built by 2001

777-200LR Long range model based on the 777-200 with more powerful engines

777F Cargo freighter model based on the 777-200LR

777-300 Stretched model with a lengthened fuselage for greater passenger capacity, also features uprated engines and greater fuel capacity for improved range compared to the 777-200 model; 34 built by 2001

777-300ER Extended range 777-300 model with more powerful engines

KNOWN OPERATORS:

Aeroflot
Air Canada
Air China
Air France
Air Europe Italy
Air India
All Nippon Airways
American Airlines
Arik Air
Asiana Airlines
Babcock & Brown Aircraft Management
Biman Bangladesh Airlines
BOC Aviation
British Airways
Cathay Pacific Airways
China Southern Airlines
Continental Airlines
Delta Airlines
Egyptair
El Al
Emirates Airlines
Etihad Airways
Federal Express
Garuda Indonesia
GE Commercial Aviation Services (GECAS)
GMG Airlines
Japan Airlines
Japan Air Systems
Jet Airways
Kenya Airways
KLM - Royal Dutch Airlines
Korean Air Lines
Kuwait Airways
LAN Chile
Lauda Air
Malaysian Airline System (MAS)
Mid East Jet
OceanAir
Pakistan International Airlines
Philippine Air Lines
Qatar Airways
Royal Brunei Airlines
Saudia
Saudi Oger
Singapore International Airlines
South African
TAAG Angola Airlines
TAM Brazil
Thai Airways International
TransBrazil
United Airlines
Vietnam Airlines
Virgin Airways
Virgin Blue Airlines
Varig

3-VIEW SCHEMATIC:

Boeing 777

SOURCES:

Aboulafia, Richard. Jane's Civil Aircraft. Glasgow: Harper Collins Publishers, 1996, p. 54-55, Boeing 777.

Boeing 777 site

Donald, David, ed. The Complete Encyclopedia of World Aircraft. NY: Barnes & Noble, 1997, p. 174, Boeing Model 777.

Donald, David, ed. The Encyclopedia of Civil Aircraft. San Diego, CA: Thunder Bay Press, 1999, p. 216-223, Boeing 777.

Rendall, David. Jane's Aircraft Recognition Guide, 2nd ed. London: Harper Collins Publishers, 1999, p. 220, Boeing 777.

Taylor, Michael. Brassey's World Aircraft & Systems Directory 1996/1997. London: Brassey's, 1996, p. 270-271, Boeing 777.

Taylor, Michael J. H. Brassey's World Aircraft & Systems Directory 1999/2000. London: Brassey's, 1999, p. 255-257, Boeing 777.

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DESCRIPTION: What eventually became the 777 project began when several airlines expressed a desire for an airliner with a capacity in between the 767-300 and 747-400. The 777 is designed for both intercontinental and transcontinental routes and is targeted primarily at the Pacific rim market. The overall design is typical of previous Boeing airliners except it is equipped with only two engines, unlike the transcontinental 707 and 747. To achieve flight certification on such a design, Boeing had to ensure new levels of reliability in engines, avionics, and a fly-by-wire control system as well as the ability to maintain level flight for three hours even with one engine inoperative. Like the 747, the 777 includes three powerplant options depending on airline preference, and these air-breathing engines are the most powerful ever fitted to any aircraft. To give some idea of the size of the 777, the engine nacelles are nearly as wide as the fuselage of the 737. However, some airlines requested the large airliner be able to use the passenger gates designed for the DC-10 and smaller aircraft, so the outer wing panels are designed to fold upward on some models. Five major variants of the 777 have been designed to date. Base models are the 727-200 and stretched 777-300, and serveral extended and long range models have also been developed. At least 700 aircraft had been built by early 2008. Last modified 15 July 2008
HISTORY:
First Flight	(777-200) 12 June 1994 (777-200ER) 7 October 1996 (777-200LR) 8 March 2005 (777-300) 16 October 1997 (777-300ER) 24 February 2003 (777F) 14 July 2008
Service Entry	(777-200) 7 June 1995 (with United Airlines) (777-200ER) 9 February 1997 (with British Airways) (777-200LR) February 2006 (with Pakistan International Airlines) (777-300) 27 May 1998 (with Cathay Pacific Airways) (777-300ER) 10 May 2004 (with Air France)
CREW:	two flight crew: pilot, co-pilot
PASSENGERS:	(777-200) 305 in three classes, 400 in two classes, 440 in one class (777-200ER) 301 in three classes, 400 in two classes, 440 in one class (777-200LR) 301 in three classes (777-300) 386 in three classes, 451 in two classes, 550 in one class (777-300ER) 365 in three classes
ESTIMATED COST:	(777-200LR) $231 to $256.5 million [2007$] (777-300ER) $250 to $279 million [2007$]
AIRFOIL SECTIONS:
Wing Root	unknown
Wing Tip	unknown
DIMENSIONS:
Length	(777-200) 209.08 ft (63.73 m) (777-200ER) 209.08 ft (63.73 m) (777-200LR) 209.08 ft (63.73 m) (777-300) 242.33 ft (73.93 m) (777-300ER) 242.33 ft (73.93 m)
Wingspan	(777-200) 199.92 ft (60.93 m) (777-200ER) 199.92 ft (60.93 m) (777-200LR) 212.58 ft (64.86 m) (777-300) 199.92 ft (60.93 m) (777-300ER) 212.58 ft (64.86 m)
Height	(777-200) 60.75 ft (18.51 m) (777-200ER) 60.75 ft (18.51 m) (777-200LR) 60.92 ft (18.58 m) (777-300) 60.75 ft (18.51 m) (777-300ER) 60.92 ft (18.58 m)
Wing Area	(777-200) 4,605 ft² (427.8 m²)
Canard Area	not applicable
WEIGHTS:
Empty	(777-200) 298,900 lb (135,580 kg)
Normal Takeoff	unknown
Max Takeoff	(777-200) 545,000 lb (247,210 kg) (777-200ER) 656,000 lb (297,824 kg) (777-200LR) 750,000 lb (340,195 kg) (777-300) 660,000 lb (299,370 kg) (777-300ER) 750,000 lb (340,195 kg)
Fuel Capacity	internal: (777-200) 31,000 gal (117,340 L) (777-200ER) 45,220 gal (171,170 L) (777-200LR) 51,590 gal (195,285 L) (777-300) 45,220 gal (171,170 L) (777-300ER) 47,890 gal (181,280 L) external: not applicable
Max Payload	unknown
PROPULSION:
Powerplant	(777-200) two Pratt & Whitney PW4077 turbofans or two Rolls-Royce Trent 877 turbofans or two General Electric GE90-77B turbofans (777-200ER) two Pratt & Whitney PW4084/PW4090 turbofans or two Rolls-Royce Trent 884/892/895 turbofans or two General Electric GE90-85B/92B/94B turbofans (777-200LR) two General Electric GE90-110B1 turbofans (777-300) two Pratt & Whitney PW4098 turbofans or two Rolls-Royce Trent 892 turbofans (777-300ER) two General Electric GE90-115B turbofans
Thrust	(777-200) 77,200 lb (343 kN) [P&W] (777-200) 76,000 lb (338 kN) [RR] (777-200) 77,000 lb (342 kN) [GE] (777-200ER) 90,200 lb (401 kN) [P&W] (777-200ER) 93,400 lb (415 kN) [RR] (777-200ER) 93,700 lb (417 kN) [GE] (777-200LR) 110,000 lb (489 kN) (777-300) 98,00 lb (435 kN) [P&W] (777-300) 90,000 lb (400 kN) [RR] (777-300ER) 115,000 lb (512 kN)
PERFORMANCE:
Max Level Speed	at altitude: 575 mph (930 km/h) at 35,000 ft (10,675 m), Mach 0.87 at sea level: unknown cruise speed: 560 mph (900 km/h) at 35,000 ft (10,675 m), Mach 0.84
Initial Climb Rate	unknown
Service Ceiling	43,100 ft (13,135 m)
Range	(777-200) 5,210 nm (9,650 km) (777-200ER) 7,730 nm (14,315 km) (777-200LR) 9,420 nm (17,445 km) (777-300) 5,950 nm (11,030 km) (777-300ER) 7,175 nm (13,290 km)
g-Limits	unknown
KNOWN VARIANTS:
777-200	First production model originally designated 777-200A; 76 built by 2001
777-200ER	Extended range model originally designated 777-200B or 777-200IGW (Increased Gross Weight) with greater fuel capacity and uprated engines; 203 built by 2001
777-200LR	Long range model based on the 777-200 with more powerful engines
777F	Cargo freighter model based on the 777-200LR
777-300	Stretched model with a lengthened fuselage for greater passenger capacity, also features uprated engines and greater fuel capacity for improved range compared to the 777-200 model; 34 built by 2001
777-300ER	Extended range 777-300 model with more powerful engines
KNOWN OPERATORS:	Aeroflot Air Canada Air China Air France Air Europe Italy Air India All Nippon Airways American Airlines Arik Air Asiana Airlines Babcock & Brown Aircraft Management Biman Bangladesh Airlines BOC Aviation British Airways Cathay Pacific Airways China Southern Airlines Continental Airlines Delta Airlines Egyptair El Al Emirates Airlines Etihad Airways Federal Express Garuda Indonesia GE Commercial Aviation Services (GECAS) GMG Airlines Japan Airlines Japan Air Systems Jet Airways Kenya Airways KLM - Royal Dutch Airlines Korean Air Lines Kuwait Airways LAN Chile Lauda Air Malaysian Airline System (MAS) Mid East Jet OceanAir Pakistan International Airlines Philippine Air Lines Qatar Airways Royal Brunei Airlines Saudia Saudi Oger Singapore International Airlines South African TAAG Angola Airlines TAM Brazil Thai Airways International TransBrazil United Airlines Vietnam Airlines Virgin Airways Virgin Blue Airlines Varig
3-VIEW SCHEMATIC:
SOURCES: Aboulafia, Richard. Jane's Civil Aircraft. Glasgow: Harper Collins Publishers, 1996, p. 54-55, Boeing 777. Boeing 777 site Donald, David, ed. The Complete Encyclopedia of World Aircraft. NY: Barnes & Noble, 1997, p. 174, Boeing Model 777. Donald, David, ed. The Encyclopedia of Civil Aircraft. San Diego, CA: Thunder Bay Press, 1999, p. 216-223, Boeing 777. Rendall, David. Jane's Aircraft Recognition Guide, 2nd ed. London: Harper Collins Publishers, 1999, p. 220, Boeing 777. Taylor, Michael. Brassey's World Aircraft & Systems Directory 1996/1997. London: Brassey's, 1996, p. 270-271, Boeing 777. Taylor, Michael J. H. Brassey's World Aircraft & Systems Directory 1999/2000. London: Brassey's, 1999, p. 255-257, Boeing 777.