Airbus A320neo (320)

Only representative arrangements are listed.
Please note that scheduled aircrafts are subject to change without prior notice.
*For seat details, please select the class/aircraft type from In-flight Service and click here.

146 seats

  • Galley
  • Bar
  • Multi-purpose Room
  • Monitor
  • Emergency Exit
  • Stairs
  • Lavatory
  • Wheelchair Accessible Lavatory
  • Lavatory with a table for diaper change
  • Lavatory with a multi-function bidet
  • Emergency exit row seat
  • No Window Seat
  • Reclining Not Available
  • Armrest Non-movable seat
  • ANA COUCHii
  • Table
  • Movable Partition
  • *Only typical seat configurations are shown.

This is the seat map for the 146-seat Airbus A320neo.
There are 8 Business Class and 138 Economy Class seats. Seat rows are numbered from 1 to 27.
Emergency exits are located on both sides at the front of the cabin, both sides at row 11, both sides at row 12, and both sides at the back of the cabin. 

Business Class seats are in rows 1 and 2.
The seat layout from left to right is A, C, aisle, H, K. Armrests are non-movable for all of these seats. Monitors are installed in front of row 1. 

Economy Class seats are in rows 5 to 27.
The seat layout from left to right is A, B, C, aisle, H, J, K. All seats in rows 11 and 12 are emergency exit row seats. Seats 10A, 10K, 11A, and 11K do not recline. Armrests are non-movable for all seats in row 5. Monitors are installed in front of row 5. 

A wheelchair-accessible lavatory equipped with a diaper changing table is located on the seat A side at the back of the cabin. Lavatories equipped with a diaper changing table are located in front of seats 1A and C and behind seats 27A, B, and C. A lavatory is located at the back center of the cabin.
Galleys are located at the front and back of the cabin.

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Spec

Seats 146 seats
Overall Length 37.6 m
Wing Span 35.8 m
Tail Height 11.8 m
Typical Cruise Speed 840 km/h
Cruising range 6,280 km
Maximum operation altitude 12,100 m
Maximumtake off weight 79.0 ton
Engines PW1127G-JM
Thrust of engine 12,160 kg (26,800 lbf) X 2
Maximum Fuel Capacity 23.7 kl

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