Auto Credit Based on GalacticaAsia's (Updated)A320[CFM]
No description.
Specifications
General Characteristics
- Predecessor (Updated)A320[CFM]
- Created On iOS
- Wingspan 107.5ft (32.8m)
- Length 123.3ft (37.6m)
- Height 40.4ft (12.3m)
- Empty Weight 34,550lbs (15,671kg)
- Loaded Weight 45,949lbs (20,842kg)
Performance
- Power/Weight Ratio 0.548
- Horse Power/Weight Ratio 0.065
- Wing Loading 29.2lbs/ft2 (142.8kg/m2)
- Wing Area 1,571.5ft2 (146.0m2)
- Drag Points 6124
Parts
- Number of Parts 467
- Control Surfaces 9
- Performance Cost 2,995
@AviationLover12345 np
@CaptainBrayden um tbh i think ill pass but at least ty for tryna help!
@AviationLover12345 only the excerpt on the a320– you know what? Just copy this: The programme was launched on 2 March 1984.[16] At the time, Airbus had 96 orders.[17]: 48 Air France was its first customer to sign a "letter of intent" for 25 A320s and options for 25 more at the 1981 Paris Air Show.[18] In October 1983, British Caledonian placed seven firm orders, bringing total orders to more than 80.[19] Cyprus Airways became the first customer to place an order for V2500-powered A320s in November 1984, followed by Pan Am with 16 firm orders and 34 options in January 1985, and then Inex Adria.[17]: 49 One of the most significant orders occurred when Northwest Airlines placed an order for 100 A320s in October 1986, powered by CFM56 engines, later confirmed at the 1990 Farnborough Airshow.[17]: 49–50
During A320 development, Airbus considered propfan technology, which was backed by Lufthansa.[13] At the time unproven, the technology essentially consisted of a fan placed outside the engine nacelle, offering turbofan speeds and turboprop economics; ultimately, Airbus stuck with turbofans.
Power on the A320 was to be supplied by two CFM56-5-A1s rated at 111 kN (25,000 pounds-force).[14] It was the only engine available until the arrival of the IAE V2500, offered by International Aero Engines, a group composed of Rolls-Royce plc, Pratt & Whitney, Japanese Aero Engine Corporation, Fiat and MTU. The first V2500 variant, the V2500-A1, has a thrust output of 110 kN (25,000 pounds-force),[20] hence the name. It is 4% more efficient than the CFM56, with cruise thrust-specific fuel consumption for the -A5 at 16.3 and 16.9 g/kN/s (0.58 and 0.60 lb/lbf/h) for the CFM56-5A1.[21]
@CaptainBrayden only the what?
@AviationLover12345 there is no page with only the a320, you could use only the excerpt on the a320
@CaptainBrayden ty but what i mean is a wiki page that only has info on the a320, that page is the entire family & the variants options dont include the a320.
@AviationLover12345 here is wiki: ! here ya go
I just noticed i forgot the lights on the top & bottom for this plane, i apologise.
Before any of yall tell me i forgot the description, i didnt, I couldn’t find info on the wiki (where i find info abt all planes) page for the a320.