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.
What do various states have to do?
All aircraft manufacturing workers in various states must be reminded they are state workers with the affiliation of World Aviation Administration. Boeing, Airbus, and some others have to merge and identity with individual state and the World Aviation Administration.
Aircraft specifications
Aircraft Specifications
Intercontinental aircraft
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Aspect ratio: 8.5
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Cabin width: 20.1 ft (6.13 m)
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Cabin length: 49.9 m (163 ft 9 in) main deck
44.93 m (147 ft 5 in) upper deck
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Cargo capacity: 5,705 cu ft (162 m3)/30,177 cu ft (855 m3)
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Cockpit crew: 2
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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)
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Engines/Powerplant (4×):
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Height: 19.4 m (63 ft 8 in)
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Interior cabin width: 20 feet (6.1 m)
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Landing speed: 130-135 kn (240–250 km/h)
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Length: 250 ft 2 in (76.3 m)
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Long-distance cruising speed: Mach 0.85 (289m/s)
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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)
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Maximum landing weight: 688,000 lb (312,000 kg)/ 757,000 lb (343,000 kg)
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Maximum speed,advised operating: Mach 0.9
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Maximum structural payload: 169,100 lb (76,700 kg)/ 295,800 lb (134,000 kg)
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Maximum Zero-fuel weight: 651,000 lb (295,000 kg) / 727,000 lb (330,000 kg)
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Overall length: 250 ft 2 in (76.3 m)
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Passengers: (three-class arrangement): 605 (maximum)
467 (3-class)
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Powerplant: 4 Engine
(82,000 lb thrust)
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Range: 7, 260 nm
(13,450 km)
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Seating capacity: (three-class arrangement): 605 (maximum) 467 (3-class)
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Seating configuration: Two decks,
two aisles main deck
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Service ceiling: 41,000 ft
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Thrust/Powerplant (4×): (82,000 lb thrust)
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Top cruising speed: Mach 0.92 (313 m/s)
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Top Speed: 614 mph
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Weight: Empty: 393,263 lbs (178,756 kg)
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Weight: Max Takeoff: 875,000 lbs (397,000 kg)
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Wing area: 554 m2 (5,960 sq ft)
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Wing sweep: 37.5
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Wingspan: 224 ft 7 in (68.5 m)
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Airbus 380 |
Boeing 747-400
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001
Coming Soon |
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| Measurements |
| Wingspan |
79.8 m (261 ft 10 in) |
64.4 m (211 ft 5 in) |
68.5 m (224 ft 7 in) |
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| Length |
73.0 m (239 ft 6 in) |
70.7 m (231 ft 10 in) |
105.22 m (or ft - in) |
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| Height |
24.1 m (79 ft) |
19.4 m (63 ft 8 in) |
19.4 m (63 ft 8 in)
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| Weight: Empty |
610,700 lbs
(277,000 kg) |
393,263 lbs
(178,756 kg) |
393,263 lbs
(178,756 kg)
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| Weight: Max Takeoff |
1,234,600 lbs
(560,000 kg) |
875,000 lbs
(397,000 kg) |
875,000 lbs
(397,000 kg)
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| Capacity/Layout |
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| Crew |
2 |
2 |
2 |
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| Passengers (three-class arrangement) |
555 |
416 |
800 (Two types, single and two storeyed
Jumbo) |
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| Seating configuration |
Two decks,
two aisles per deck |
Two decks,
two aisles main deck
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Two decks,
two aisles main deck
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| Miscellaneous |
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| Range |
8,000 nm (14,800 km) |
7, 260 nm
(13,450 km)
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7, 260 nm
(13,450 km)
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| Service ceiling |
43,000 ft (13,100 m) |
41,000 ft
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41,000 ft
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| Top cruising speed |
Mach 0.88 (299 m/s) |
Mach 0.92 (313 m/s)
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Mach 0.92 (313 m/s)
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| Long-distance cruising speed |
Mach 0.85 (289 m/s) |
Mach 0.85 (289m/s) |
Mach 0.85 (289m/s)
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| 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
Engine/Thrust: Four General Electric CF6-80s/44,700 lbs each
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4 Engine
(82,000 lb thrust)
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