Airbus A320 Series User Manual

A320 INSTRUCTOR SUPPORT
CONTENTS
DATE: JAN 2001 Page iii UDYXX02
B – ABNORMAL OPERATION
1 - ECAM PHILOSOPHY....................................................................................................... 175
2 - REJECTED TAKE-OFF (REFER FCOM 3-02-01) ............................................................ 181
3 - ENGINE FAILURE/FIRE AFTER V1................................................................................. 183
4 - FAILURE OF SOME ENGINE COMPONENTS ................................................................ 185
5 - EMERGENCY ELECTRICAL CONFIGURATION............................................................. 187
6 - DOUBLE HYDRAULIC FAILURE..................................................................................... 190
7 - ABNORMAL SLATS/FLAPS............................................................................................ 192
8 - ZFW ENTRY ERROR (PILOT’S ENTRY) ......................................................................... 194
9 - DOUBLE RADIO ALTIMETER FAILURE......................................................................... 197
10 - UNRELIABLE SPEED/ALTITUDE INDICATION .............................................................. 199

Airbus A320 Series Specifications

General

Manufacturer	Airbus
Engines	2
Variants	A318, A319, A320, A321
First Flight	22 February 1987
Passenger Capacity	150-180
Range	3, 300 nautical miles (6, 100 km)
Wingspan	34.1 m
Length	37.57 m
Height	11.76 m
Cruise Speed	828 km/h
Typical Seating	150 (2-class)
Cargo Volume	37.41 m³
Engines Model	CFM International CFM56 or IAE V2500
Service Ceiling	11, 900–12, 500 m
Thrust per Engine	111–120 kN