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Airbus

A350-1000

WIDE-BODY


Family:
Airbus A350
Type:
Turbofan airplane

Origin:
Country FlagEuropean Union
Manufacturer:
2010–present

Related:
Airbus A350-800
Airbus A350-900

Updated March 8, 2024
Aircraft picture
A350-1000 - Alan Wilson. CC-BY-SA-2.0

General characteristics (19)

  • Role
    Wide-body airliner
  • Crew
    2 pilots
  • Wing
    Fixed wing
  • Wing position
    Low wing (winglets)
  • Engine count
    2
  • ICAO type designator
    A35K
  • Body
    Wide
  • Tail
    Regular tail, low set
  • WTC
    H
  • APC
    D
  • Type code
    L2J
  • RFF Category
    9
  • Landing gear
    Tricycle retractable
  • Engine position
    Underwing mounted
  • Aerodrome ref. code
    4E
  • ADG
    VI
  • TDG
    6
  • SRS
    III
  • LAHSO
    9

Structural data (14)

  • Length
    66.8 m (219.2 ft)
  • Height (fuselage)
    6.09 m (19.98 ft)
  • Height (to fin)
    17.05 m (55 ft 11 in)
  • Width (fuselage)
    5.96 m (19.6 ft)
  • Width (cabin)
    5.61 m (18 ft 5 in) or 5.71 m (18 ft 9 in)
  • Wing area
    443 m² (4,768.45 sq ft)
  • Wingspan
    64.75 m (212.43 ft)
  • Sweep angle
    31.9°
  • Aspect ratio
    9.49
  • Parking area
    5,105.3 m2 (54,952.8 ft2)
  • Main gear config
    3D
  • Cockpit to main gear
    34.1 m (111.8 ft)
  • Main gear width
    12.8 m (42.1 ft)
  • Wheelbase
    32.5 m (106.6 ft)

Performance & capabilities (9)

  • Range
    8,300 nmi (15,372 km; 9,600 mi)
  • Fuel capacity
    140.8 m3 (37,200 US gal) or 110.5 t (244,000 lb)
  • Service ceiling
    43,100 ft (13,100 m)
  • Cargo capacity
    36 LD3 or 11 pallets
  • Maximum payload
    45.9–56.4 t (101,300–124,300 lb)
  • Seating (typical)
    315
  • Seating (maximum)
    440
  • Takeoff run
    2,600 m (8,500 ft)
  • Landing run
    2,000 m (6,600 ft)

Speeds (5)

  • Cruise (VCR)
    488 kt (903 km/h)
  • Cruise Mach
    0.85
  • Maximum (VMAX)
    513 kt (950 km/h)
  • Maximum Mach
    0.89
  • FAA approach
    154 kt (285 km/h)

Indicative Flight Profile data (23)
Source:SKYbrary logoSKYbrary [1]

  • Takeoff
    V2: -
    Distance: -
    Weight: 308000 kg
  • Initial climb (to 5000 ft)
    IAS: -
    ROC: -
  • Initial climb (to 15,000 ft)
    IAS: -
    ROC: -
  • Initial climb (to 24,000 ft)
    IAS: -
    ROC: -
  • Mach climb
    Mach: -
    ROC: -
  • Cruise
    TAS: 487 kts
    Mach: 0,85
    Ceiling: FL431
    Range: 7990 NM
  • Initial descent (to 24,000 ft)
    IAS: -
    ROD: -
  • Descent (to 10,000 ft)
    IAS: -
    ROD: -
  • Descent (below 10,000 ft)
    IAS: -
    MCS: -
    ROD: -
  • Approach
    VAPP (IAS): -
    Distance: -

Weights (7)

  • OEW
    142,400 kg (314,000 lb) typical
  • MEW
    115,000 kg (255,075 lb)
  • MLW
    233,000 kg (513,680 lb)
  • MTOW
    308,000 kg (679,020 lb)
  • MZFW
    220,000 kg (485,020 lb)
  • MTW
    308,900 kg (681,010 lb)
  • FAA weight class
    Heavy

Engine options (1)

Option 1:

  • Model
  • Manufacturer
    Country FlagRolls-Royce
  • Type
    Turbofan
  • Fan blades
    18
  • Fan stages
    1
  • IP compressor stages
    8
  • HP compressor stages
    6
  • LP turbine stages
    6
  • IP turbine stages
    2
  • HP turbine stages
    1
  • Control system
    Dual channel FADEC
  • Length
    5.81 m (19.06 ft)
  • Fan diameter
    3.00 m (9.84 ft)
  • Max continuous thrust
    369.60 kN (83,089.37 lbf)
  • Max takeoff thrust
    431.50 kN (97,005.04 lbf)
  • Bypass ratio
    9.6:1
  • ISA sea level pressure ratio
    50:1 (at take-off thrust)
  • Nominal 1st shaft RPM
    2,700
  • Nominal 2nd shaft RPM
    8,200
  • Nominal 3rd shaft RPM
    12,600
  • Dry weight
    7,549.00 kg (16,645.55 lb)

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