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SEP 13/07 K8419 COMMUNICATION - CIDS - DEFINE
INTERCOMMUNICATION DATA SYSTEM
(CIDS) FOR ANZ01 VERSION
33069
.. ....
ALL
SEP 13/07 K8413 EQUIPMENT/FURNISHINGS-PAX
COMPT.SEATS - INTRODUCE AN IN SEAT
POWER SUPPLY SYST. (ISPSS)110VAC,
VENDOR GENERAL DYNAMICS
33085
.. ....
ALL
SEP 13/07 K9150 E/F-PAX COMPARTMENT-INSTALL A TWO
CLASS 114 PAX CABIN LAYOUT
CONFIGURATION FOR DRK01 VERSION
34062
.. ....
ALL
TR1 A318/A319/A320/A321 FLEET CCOM Page 3 of 3
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
TABLE OF CONTENTS
01.000
JAN 08/08
01.010 AIRCRAFT PRESENTATION
-- GENERALITES 1
01.020 AIRCRAFT DIMENSIONS
-- DIMENSIONS 1
01.030 PERFORMANCE
-- PERFORMANCE 1
01.040 PRESSURIZATION
-- UNPRESSURIZED COMPARTMENTS 1
01.050 FLIGHT CONTROLS
-- GENERAL 1
01.060 LANDING GEARS
-- LANDING GEARS 1
01.070 CARGO COMPARTMENTS
-- CARGO COMPARTMENTS 1
-- CARGO DOORS 2
01.080 CABIN DOORS
-- CABIN DOORS 1
TR1 A318/A319/A320/A321 FLEET CCOM Page 1 of 1
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
AIRCRAFT PRESENTATION
01.010
SEP 13/07
GENERALITES
ALL
-- General : The A320 is a short to medium range, single-aisle, subsonic, civil
transport aircraft.
-- Engines : The aircraft has two high bypass, turbofan engines, mounted
underneath the wings.
-- Cockpit : The cockpit is arranged for a two-member crew. It also has a place
for one observer (plus optionally an additional one).
-- Cabin :
. The passenger seating layout may be varied to suit operating
requirements, up to a certified maximum of 180 seats.
. Any combination of cabin crew seats may be provided, with a minimum of
4 imperative seats.
CAUTION
-- AS WITH THE FLIGHT CREW PROCEDURES, A TRIPPED CIRCUIT
BREAKER MUST NOT BE RE-ENGAGED IN FLIGHT.
-- ON GROUND, THE CABIN CREW MAY RE-ENGAGE THE CIRCUIT
BREAKER, IF THE ACTION IS COORDINATED WITH MAINTENANCE
AND THE CAUSE OF THE TRIPPING IS IDENTIFIED.
TR1 A318/A319/A320/A321 FLEET CCOM Page 1 of 1
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
AIRCRAFT DIMENSIONS
01.020
SEP 13/07
DIMENSIONS
ALL
The overall cabin length of the A320 is 27,51 meters (90 feet, 3 inches).
TR1 A318/A319/A320/A321 FLEET CCOM Page 1 of 2
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
AIRCRAFT DIMENSIONS
01.020
SEP 13/07
AIRCRAFT DIMENSIONS
12,45m
34,1m
111ft 10in
40ft 10in
24ft 11in
37ft 9in
11,51m
7,59m
3,95m
12ft 11in
5,75m
5,07m
16ft 7in
18ft 10in
NOC 01020 02243 0001
37,57m
123ft 3in
12,64m
41ft 6in
11.76m
38ft 7in
TR1 A318/A319/A320/A321 FLEET CCOM Page 2 of 2
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
PERFORMANCE
01.030
SEP 13/07
PERFORMANCE
ALL
The design weights of the A320 are as follows :
- MAX operating altitude: between 39 000 feet and 41 100 feet depending on
aircraft certification
- MAX design speeds (VMO/MMO): 350 kt ; 0.82 M
TR1 A318/A319/A320/A321 FLEET CCOM Page 1 of 1
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
PRESSURIZATION
01.040
SEP 13/07
UNPRESSURIZED COMPARTMENTS
ALL
UNPRESSURIZED COMPARTMENTS
MAIN GEAR
BAY
NOSE GEAR TAIL CONE
BAY
UNPRESSURIZED AREAS
NOC 01040 00205 0001
TR1 A318/A319/A320/A321 FLEET CCOM Page 1 of 1
CABIN CREW OPERATING MANUAL
AIRCRAFT GENERAL
FLIGHT CONTROLS
01.050
SEP 13/07
GENERAL
ALL
The fly-by-wire control system was designed and certificated to render the new
generation of aircraft safer, more cost effective, and more pleasant to fly, or ride
in, than a conventional aircraft.
BASIC PRINCIPLE
All flight control surfaces are :
-- Electrically controlled,
-- Hydraulically activated.
The stabilizer and rudder can also be controlled mechanically.
The pilots use the sidesticks to fly the aircraft in pitch and roll (and in yaw,
indirectly, through turn coordination).
Computers interpret pilot inputs and move the flight control surfaces, as
necessary, to carry out these orders.
However, regardless of the pilot’s inputs, computers prevent :
-- Excessive maneuvers,
-- Flight outside the safe-flight envelope.
FLIGHT CONTROL BASIC PRINCIPLE
A/P
COMPUTER
SIDE
STICK
SURFACE
FEEDBACK
FEEDBACK
COMPUTER
ORDER
RESPONSE
F/CTL
　
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