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Aircraft manufacturers
Make/Model/Series 1

Do mergers of aircraft manufacturers hurt or help? What should the world look forward to in aircraft manufacturing? What recommendations are there for aircraft manufacturing? Who all must merge in aircraft manufacturing? What resources are required to manufacture the types of aircraft displayed here? How is an aircraft built? Why are these resources essential for all states around the world? What is the main purpose of these aircrafts? Is it possible to manufacture these planet/global aircraft with specifications displayed at this resource? How should you ideally go ahead with manufacture of large aircraft? What is aerospace engineering? What is aerospace electronics? What are examples of common electronic components? How are electronic components categorized? How many aerospace engineers are required to manufacture a large aircraft within 18 months? What will the aircraft look like? Do you manufacture these resources within the state? What do you have to do to manufacture these resources within the state? What do you understand by open source manufacturing of products?

Do mergers of aircraft manufacturers hurt or help? Aircraft manufacturers’ mergers help the aviation services. What should the world look forward to in aircraft manufacturing? Aircraft manufacturers’ mergers will result in one world aircraft manufacturing entity worldwide, a public service aircraft manufacturing entity. What recommendations are there for aircraft manufacturing? There should be a merger of aircraft manufacturers worldwide to one world entity of aircraft manufacturing. Who all must merge in aircraft manufacturing? Airbus Antonov ATR AVIC I/II BAE Systems Boeing Bombardier Britten-Norman Cessna Dornier Embraer Fairchild Aerospace Fokker Hawker Beechcraft Indonesian Aerospace Lockheed Martin LZ Auronautical McDonnell Douglas NAMC Pilatus Aircraft Piper Aircraft Saab Shorts Sukhoi Tupolev Yakovlev These entities existed up to January 17, 2014. New tail numbers will be given to all aircraft worldwide. What are the specifications of aircraft you manufactured that are in service now? Aircraft manufacture What resources are required to manufacture the types of aircraft displayed here? Engineering resources: Devices, machines, materials, processes, structures, and systems. Human resources for aircrafts manufacturing. Methods and services. Locations to build and assemble various parts and data centers. Data centers with proper human resources are the most important resources for the manufacture of these aircrafts. How is an aircraft built? Data centers with proper human resources are the most important resources for the manufacture of these aircrafts. Design offices and engineering centres Aircraft Specifications Aircraft Parts and Auxiliary Equipment Aircraft Engines and Engine Parts Transport of major aircraft sections Final Assembly and tests Test program Flight test Here are further guidelines.

Aircraft Specifications

F/A-18 Hornet	JF-17 Thunder	F-16 fighter plane.	F-18 HARV (High Alpha Research Vehicle).
F-35 fighter plane.	Flying a MiG-30 fighter	F-22 Raptor.	The Xiaolong/FC-4 fighter plane.
MIG-29 fighter plane.	Sukhoi-30 fighter plane.	Sukhoi-27 fighter plane.	A-4 SkyHawk Firing.

Airplanes
Military Aircraft

Aircraft Manufacturing-Project Report

Intercontinental aircraft

Fighters : F-4 , F-14 , F-15 , F-16 , F-18 , F-22 , Etc.

Bombers, Attack : Stealth , Bombers , Attack

Aerobatic teams : Blue Angels , Thunderbirds

Helicopters : Helicopters

Special aircraft : SR-71 Blackbird , Electronic Warfare and Control

Transport , Other Aircraft

Aircraft carriers

RC Airplanes

Intercontinental aircraft

Aspect ratio: 8.5 Cabin width: 20.1 ft (6.13 m) Cabin length: 49.9 m (163 ft 9 in) main deck 44.93 m (147 ft 5 in) upper deck Cargo capacity: 5,705 cu ft (162 m3)/30,177 cu ft (855 m3) Cockpit crew: 2 Cruising speed: at 35,000 ft (10,700 m): Mach 0.855 (570 mph or 917 km/h or 495 kn)/Mach 0.845 (564 mph or 908 km/h or 490 kn) Engines/Powerplant (4×): Height: 19.4 m (63 ft 8 in) Interior cabin width: 20 feet (6.1 m) Landing speed: 130-135 kn (240–250 km/h) Length: 250 ft 2 in (76.3 m) Long-distance cruising speed: Mach 0.85 (289m/s) Maximum fuel capacity: 63,034 US gal (239,000 L; 52,500 imp gal)/60,211 US gal (228,000 L; 50,100 imp gal) Maximum landing weight: 688,000 lb (312,000 kg)/ 757,000 lb (343,000 kg) Maximum speed,advised operating: Mach 0.9 Maximum structural payload: 169,100 lb (76,700 kg)/ 295,800 lb (134,000 kg) Maximum Zero-fuel weight: 651,000 lb (295,000 kg) / 727,000 lb (330,000 kg) Overall length: 250 ft 2 in (76.3 m) Passengers: (three-class arrangement): 605 (maximum) 467 (3-class) Powerplant: 4 Engine (82,000 lb thrust) Range: 7, 260 nm (13,450 km) Seating capacity: (three-class arrangement): 605 (maximum) 467 (3-class) Seating configuration: Two decks, two aisles main deck Service ceiling: 41,000 ft Thrust/Powerplant (4×): (82,000 lb thrust) Top cruising speed: Mach 0.92 (313 m/s) Top Speed: 614 mph Weight: Empty: 393,263 lbs (178,756 kg) Weight: Max Takeoff: 875,000 lbs (397,000 kg) Wing area: 554 m2 (5,960 sq ft) Wing sweep: 37.5 Wingspan: 224 ft 7 in (68.5 m)

	Airbus 380	Boeing 747-400	001 Coming Soon
Measurements
Wingspan	79.8 m (261 ft 10 in)	64.4 m (211 ft 5 in)	68.5 m (224 ft 7 in)
Length	73.0 m (239 ft 6 in)	70.7 m (231 ft 10 in)	105.22 m (or ft - in)
Height	24.1 m (79 ft)	19.4 m (63 ft 8 in)	19.4 m (63 ft 8 in)
Weight: Empty	610,700 lbs (277,000 kg)	393,263 lbs (178,756 kg)	393,263 lbs (178,756 kg)
Weight: Max Takeoff	1,234,600 lbs (560,000 kg)	875,000 lbs (397,000 kg)	875,000 lbs (397,000 kg)
Capacity/Layout
Crew	2	2	2
Passengers (three-class arrangement)	555	416	800 (Two types, single and two storeyed Jumbo)
Seating configuration	Two decks, two aisles per deck	Two decks, two aisles main deck	Two decks, two aisles main deck
Miscellaneous
Range	8,000 nm (14,800 km)	7, 260 nm (13,450 km)	7, 260 nm (13,450 km)
Service ceiling	43,000 ft (13,100 m)	41,000 ft	41,000 ft
Top cruising speed	Mach 0.88 (299 m/s)	Mach 0.92 (313 m/s)	Mach 0.92 (313 m/s)
Long-distance cruising speed	Mach 0.85 (289 m/s)	Mach 0.85 (289m/s)	Mach 0.85 (289m/s)
Powerplant	4 Rolls-Royce Trent 900 turbofans (initially 70,000 lb thrust; cleared at 80,000 lb thrust) or 4 Engine Alliance GP7200 turbofans (approx. 82,000 lb thrust)	4 Pratt & Whitney PW4062 turbofans (63,300 lb thrust) or 4 Rolls-Royce RB211-524 H2-T (59,500 lb thrust) or General Electric CF6-80C2B5F (62,000 lb thrust)	4 Engine (82,000 lb thrust)

http://www.qureshiuniversity.org/aircraftspecifications.htm
http://www.qureshiuniversity.com/aircraftmanufactureworld.html

Why are these resources essential for all states around the world? See the difference. Take a look at existing values of various aircraft around the world. As of November 4, 2014, these are the facts. Boeing 747 Jumbo Jets and Airbus A-340 The current list price of Boeing's long-range jets goes from Rs 2,282 crore for a brand new B-747-8 to Rs 1,352 crore for a B 787-8. Airbus long-range jets' current list price goes from Rs 2,112 crore for A-350-1000 to Rs 1,375 crore for A-330-200. (Calculations at Rs 62 to a dollar). Aircraft specifications Here are further guidelines. http://www.qureshiuniversity.org/aircraftspecifications.htm Is it possible to manufacture these planet/global aircraft with specifications displayed at this resource? Yes. Here are further guidelines. http://www.qureshiuniversity.com/aircraftmanufactureworld.html

How should you ideally go ahead with manufacture of large aircraft?

Aerospace electronics

Aircraft hydraulics

Aerospace engineering

What is aerospace engineering?
Aerospace engineering focuses on airframe, engines, structures, and composites.

What is aerospace electronics?
Aerospace electronics focuses on aircraft (space craft) electronics (avionics) systems, aircraft navigation, and flight control systems.

What are examples of common electronic components?
Capacitors, inductors, resistors, diodes, transistors, etc.

How are electronic components categorized?
Components often are categorized as active (e.g., transistors and thyristors) or passive (e.g., resistors and capacitors).

Aerospace electronics is also called avionics.

How many aerospace engineers are required to manufacture a large aircraft within 18 months?
Here are further guidelines.

What will the aircraft look like?

Do you manufacture these resources within the state? What do you have to do to manufacture these resources within the state? Here are further guidelines.

Open Source manufacturing of products. What do you understand by open source manufacturing of products? Here are further guidelines.

Intercontinental What is the main purpose of these aircrafts? Intercontinental aircrafts. Cargo, military, passenger intercontinental Jumbo Jets. Others listed. Sample Passengers Typical 3-class configuration 467 Cargo Intercontinental -- Total cargo capacity 161.5 cu m (5,705 cu ft) including 7 pallets and 16 LD-1 containers plus bulk storage of 18.1 cu m (640 cu ft); revenue volume 110.3 cu m (3,895 cu ft). Freighter -- Total cargo capacity 30,288 cu ft (857.7 cu m); total main-deck volume capacity 24,462 cu ft (692.7 cu m), consisting of 34 2.4 m x 3.2 m (96 in x 125 in) pallets of which 27 are 3-m (10-ft) high units; total lower-hold volume capacity 165.7 cu m (5,850 cu ft), consisting of 12 2.4 m x 3.2 m (96 in x 125 in) pallets, 2 LD-1 containers and bulk storage of 14.0 cu m (496 cu ft). Engines (Maximum thrust) GEnx-2B67 (x4) 66,500 lb (296 kn) Maximum Fuel Capacity Intercontinental: 64,055 U.S. gallons (242,470 L) Freighter: 60,755 U.S. gallons (229,980 L) Maximum Takeoff Weight 987,000 lb (447,696 kg) Maximum Range Intercontinental -- 14,815 km (8,000 nmi) Typical city/state/continent pairs: Chicago/Illinois/North America - Srinagar/kashmir/Asia Freighter -- 8,130 km (4,390 nmi) Typical Cruise Speed (at 35,000 feet) Mach 0.855 (Intercontinental) Mach 0.845 (Freighter) Basic Dimensions Wing Span Overall Length Tail Height 68.5 m (224 ft 7 in) Overall length 76.3 m (250 ft 2 in) Tail Height 19.4 m (63 ft 6 in) Interior Cabin Width 6.1 m (20.1 ft) 747-8 Passengers Typical 3-class configuration 467 Cargo Intercontinental -- Total cargo capacity 161.5 cu m (5,705 cu ft) including 7 pallets and 16 LD-1 containers plus bulk storage of 18.1 cu m (640 cu ft); revenue volume 110.3 cu m (3,895 cu ft). Freighter -- Total cargo capacity 30,288 cu ft (857.7 cu m); total main-deck volume capacity 24,462 cu ft (692.7 cu m), consisting of 34 2.4 m x 3.2 m (96 in x 125 in) pallets of which 27 are 3-m (10-ft) high units; total lower-hold volume capacity 165.7 cu m (5,850 cu ft), consisting of 12 2.4 m x 3.2 m (96 in x 125 in) pallets, 2 LD-1 containers and bulk storage of 14.0 cu m (496 cu ft). Engines (Maximum thrust) GEnx-2B67 (x4) 66,500 lb (296 kn) Maximum Fuel Capacity Intercontinental: 64,055 U.S. gallons (242,470 L) Freighter: 60,755 U.S. gallons (229,980 L) Maximum Takeoff Weight 987,000 lb (447,696 kg) Maximum Range Intercontinental -- 14,815 km (8,000 nmi) Typical ______ pairs: New York - Hong Kong Los Angeles - _____ ______ - Singapore Freighter -- 8,130 km (4,390 nmi) Typical Cruise Speed (at 35,000 feet) Mach 0.855 (Intercontinental) Mach 0.845 (Freighter) Basic Dimensions Wing Span Overall Length Tail Height 68.5 m (224 ft 7 in) Overall length 76.3 m (250 ft 2 in) Tail Height 19.4 m (63 ft 6 in) Interior Cabin Width 6.1 m (20.1 ft) M-4 performance characteristics Wing span: 50.53 meters Length: 48.70 meters Height: 14.10 meters Wing area: 326.35 square meters Maximum speed: 947 kilometers per hour Operational range: 8,100 kilometers Service ceiling: 11,000 kilometers Crew: eight persons Operational load: 9,000 kilograms standard, 24,000 kilograms maximum B-52 Role Strategic bomber First flight 15 April 1952 Introduction February 1955 Status In service Air Combat Command's B-52 is a long-range, heavy bomber that can perform a variety of missions. The bomber is capable of flying at high subsonic speeds at altitudes up to 50,000 feet (15,166.6 meters). It can carry nuclear or conventional ordnance with worldwide precision navigation capability. Specifications (B-52H) General characteristics Crew: 5 (pilot, copilot, Weapon Systems Officer, navigator, Electronic Warfare Officer, and tail gunner until the removal of the tail gun in 1991) Length: 159?ft 4 in (48.5?m) Wingspan: 185?ft 0?in (56.4?m) Height: 40?ft 8?in (12.4?m) Wing area: 4,000?sq?ft (370 m²) Airfoil: NACA 63A219.3 mod root, NACA 65A209.5 tip Empty weight: 185,000 lb (83,250 kg) Loaded weight: 265,000 lb (120,000 kg) Max. takeoff weight: 488,000 lb (220,000 kg) Powerplant: 8 × Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) each Fuel capacity: 47,975 U.S. gal (39,948 imp gal; 181,610 L) Zero-lift drag coefficient: 0.0119 (estimated) Drag area: 47.60 sq?ft (4.42 m²) Aspect ratio: 8.56 Performance Maximum speed: 560 kt (650 mph, 1,047 km/h) Cruise speed: 442 kt (525 mph, 844 km/h) Combat radius: 4,480 mi (3,890 nmi, 7,210 km) Ferry range: 10,145 mi (8,764 nmi, 16,232 km) Service ceiling: 50,000 ft (15,000 m) Rate of climb: 6,270 ft/min (31.85 m/s) Wing loading: 120 lb/ft² (586 kg/m²) Thrust/weight: 0.31 Lift-to-drag ratio: 21.5 (estimated) Armament Guns: 1× 20 mm (0.787 in) M61 Vulcan cannon originally mounted in a remote controlled tail turret on the H-model, removed from all current operational aircraft in 1991 Bombs: Approximately 70,000 lb (31,500 kg) mixed ordnance; bombs, mines, missiles, in various configurations Avionics Electro-optical viewing system that uses platinum silicide forward-looking infrared and high resolution low-light-level television sensors ADR-8 chaff rocket (1965-1970) LITENING Advanced Targeting System Sniper Advanced Targeting Pod IBM AP-101 computer Aircraft Parts and Auxiliary Equipment Adapter assemblies, hydromatic propeller Ailerons, aircraft Aircraft armament, except guns Aircraft arresting device system Aircraft assemblies, subÄassemblies, and parts, except engines Aircraft body assemblies and parts Aircraft power transmission equipment Aircraft propeller parts Airframe assemblies, except for guided missiles Airplane brake expanders Alighting assemblies (landing gear), aircraft Beaching gear, aircraft Blades, aircraft propeller: metal or wood Bomb racks, aircraft Brakes, aircraft Chaffing dispensers, aircraft Countermeasure dispensers, aircraft Deicing equipment, aircraft Dive brakes, aircraft Dusting and spraying equipment, aircraft Dynetric balancing stands, aircraft Elevators, aircraft Empennage (tail) assemblies and parts aircraft Fins, aircraft Flaps, aircraft wing Fuel tanks, aircraft: including self-sealing Fuselage assemblies, aircraft Gears, power transmission: aircraft Governors, aircraft propeller feathering Hubs, aircraft propeller Instrument panel mockups: aircraft training units Landing gear, aircraft Landing skis and tracks, aircraft Link trainers (aircraft training mechanisms) Nacelles, aircraft Oleo struts, aircraft Oxygen systems for aircraft Panel assemblies (hydromatic propeller test stands), aircraft Pontoons, aircraft Propeller alining tables Propellers, variable and fixed pitch and parts-aircraft Pumps, propeller feathering Refueling equipment, airplane: for use in night Research and development on aircraft parts and auxiliary equipment Roto-blades for helicopters Rudders, aircraft Seat ejector devices, aircraft Spinners, aircraft propeller Stabilizers, aircraft Target drones, aircraft Targets, trailer type: aircraft Tow targets, aircraft Training aids, aircraft: except electronic Transmissions, aircraft Turret test fixtures, aircraft Turrets and turret drives, aircraft Wheels, aircraft Wing assemblies and parts, aircraft Aircraft Engines and Engine Parts Air scoops, aircraft Aircraft engines and engine parts, internal combustion and jet Airfoils, aircraft engine Cooling systems, aircraft engine Engine heaters, aircraft Engine mount parts, aircraft Exhaust systems, aircraft External power units, aircraft: for hand-inertia starters Jet assisted takeoff devices (JATO) Lubricating systems, aircraft Pumps, aircraft engine Research and development on aircraft engines and engine parts Rocket motors, aircraft Starters, aircraft: nonelectric Turbines, aircraft type Turbo-superchargers, aircraft