
ACJ350 XWB
BASE PRICE
ACJ350-900: $ 317,400,000
ACJ350-1000: $ 366,500,000
INTERIOR BUDGET: $ 100M - $ 190M
PASSENGERS
60
CABIN AREA
ft²
3000
RANGE
nm
10000
SPEED
Mach
0.79
MTOW
lb
600000
75 PAX
11,100 nm
M 0.89
696,200 lb

The A350XWB is a long-range wide-body aircraft developed by Europe based Aerospace conglomerate Airbus.
The A350 first version was launched in 2004, using A330 fuselage with a newly developed wing and 787 technology engines from General Electric. Following the failure to attract the market to this limited change version. Airbus decided to return to the drawing boards to develop a clean-sheet all-composite wider fuselage, able to compete against both Boeing 787 and the 777 product line.
The Bolder design version 2 was launched in 2006 bearing A350XWB (for Extra Wide Body) designation powered by the latest generation specifically developed Trent XWB engines from Rolls-Royce. This version quickly attracted worldwide leading airline orders.
The shorter version A350-900 completed its first flight on June 14, 2013, prior to entering service with premium middle east airline Qatar Airways in early 2015, followed in 2018 by the longer A350-1000 model with the same launch customer airline. A Shorter version designed A350-800 was marketed by airbus prior to cancelation as the newly developed A330NEO was able to offer similar capabilities. In 2018 Airbus introduced the A350-900ULR version with increased MTOW and fuel capacity allowing launch customer Singapore Airline to launch 18 hours non-stop flight between New York and Singapore opening a new market of ultra-long-haul flights.
ACJ350-900 ULR
25 Passengers Range | 11,100 nm |
Speed | |
Maximum Speed | M 0.89 |
Altitude | |
Maximum Cruise Altitude | 43,000 ft |
Maximum Takeoff | 606,200 lbs |
Maximum Landing | 451,900 lbs |
Maximum Zero Fuel | 423,300 lbs |
Basic Operating | – |
Interior Allowance | – |
Usable Fuel | 37,248 USG |
ACJ350-1000
Range | |
25 Passengers Range | 9,850 nm |
Speed | |
Maximum Speed | M 0.89 |
Altitude | |
Maximum Cruise Altitude | 43,000 ft |
Maximum Takeoff | 696,200 lbs |
Maximum Landing | 520,300 lbs |
Maximum Zero Fuel | 491,600 lbs |
Basic Operating | – |
Interior Allowance | – |
Usable Fuel | 41,210 USG |
INTERIOR
GREENPOINT TECHNOLOGIES
GREENPOINT TECHNOLOGIES
Previous slide
Next slide
The A350 wide cabin was designed to accommodate up to 10-abreast seats. Optional crew rest facilities are available to be installed above the passengers’ compartment ceiling.
Typical Floor Plans

Completion Centers




Previous image
Next image
Interior Designers




Previous image
Next image
ACJ350-900 ULR
Cabin Height | 8 ft |
Cabin Width | 18 ft 5 in |
Cabin Length | 167 ft 5 in |
Cabin Volume | 30,162 cu.ft |
Cabin Area | 2,905 ft2 |
ACJ350-1000
Cabin Height | 8 ft |
Cabin Width | 18 ft 5 in |
Cabin Length | 190 ft 5 in |
Cabin Volume | 32,030 cu.ft |
Cabin Area | 3,315 ft2 |
Flight Deck

The A350 cockpit features six large interchangeable LCD displays units, complemented by two keyboard and cursor control units. The two lateral screens act as an integrated Electronic Flight Bag system and allow for the display of Onboard Information System (OIS) with the ability to transfer the data to the lower centrally located display for better crew coordination. An optional dual Head-Up Display (HUD) system from Thales can be installed in the cockpit allowing for enhanced situation awareness and low visibility operations.