STL 945.7136/97
AIRBUS
A319/A320/A321
Flight deck and systems
briefing for pilots
THIS BROCHURE IS PROVIDED
FOR INFORMATION PURPOSES ONLY
AND ITS CONTENTS
WILL NOT BE UPDATED.
IT MUST NOT BE USED AS AN OFFICIAL REFERENCE.
FOR TECHNICAL DATA OR OPERATIONAL PROCEDURES,
PLEASE REFER TO THE
RELEVANT AIRBUS DOCUMENTATION
STL 945.7136/97 Issue September 1998
STL 945.7136/97
STL 945.7136/97
Contents
1. General
2. Flight deck layout
3. Electrical system
4. Hydraulic system
5. Flight controls
6. Landing gear
7. Fuel system
8. Engine controls
9. Auxiliary power unit
10. Automatic flight system
11. Environmental flight system
12. Electronic instrument system
13. Radio management and communication
14. Maintenance centralized fault display system
1
STL 945.7136/97
STL 945.7136/97
1. General
1.1
STL 945.7136/97
A319/A320/A321 General
1.2
A319 A320 A321
STL 945.7136/97
A319/A320/A321 general
1.3
A319-100 A320-100 A320-200 A321-100
Span
Length
Height
Fuselage
Diameter
Track
Max. pax
Max. FL
34.10m
111ft 10in
33.84m
111ft
33.91m
111ft 3in
34.10m
111ft 10in
37.57m
123ft 3in
44.51m
146ft
11.76m
38ft 7in
3.95m
12ft 11in
7.59m
24ft 11in
145 180
390
220
STL 945.7136/97
A319/A320/A3210 general
1.4
Engine Maximum weights (kg) Operation limits
Model Manuf. Type Mmo Vmo
A319-111
A319-112
A319-113
A319-114
A319-115
A319-131
A319-132
A319-133
A319
Corporate Jet
A320-111
A320-211
A320-212
A320-214
A320-231
A320-232
A320-233
A321-111
A321-112
A321-131
A321-211
A321-231
CFM
CFM
CFM
CFM
CFM
IAE
IAE
IAE
CFM
IAE
CFM
CFM
CFM
CFM
IAE
IAE
IAE
CFM
CFM
IAE
CFM
IAE
CFM56-5B5
CFM56-5B6
CFM565A4
CFM56-5A5
CFM56-5B7
V2522-A5
V2524-A5
V2527-M-A5
CFM56-5-B6/5B7
V2524-A5/V2527-M-A5
CFM56-5-A1
CFM56-5A1/5A3
CFM56-5A3
CFM56-5B4
V2500-A1
V2527-A5
V2527E-A5
CFM56-5B1
CFM56-5B2
V2530-A5
CFM56-5B3
V2533-A5
64 000
(options :
68 000 or
70 000)
75 500
68 000
73 500
(options : from
68 000 up to
77 000)
83 000
(options :
78 000 or
85 000)
89 000
61 000
62 500
63 000
64 500
73 500
(option :
74 500)
75 000
57 000
58 000
59 000
60 500
(option :
61 000)
69 500
(option :
70 500
71 500
MTOW MLW MZFW
0.82 350kt
STL 945.7136/97
A319/A320/A321 introduction
1.5
The A319/A320/A321 are narrow body, twin-engined,
short / medium-range aircraft, the A319 being the
shortened version of the A320, and the A321 being the
stretched version of the A320.
They both offer an increased fuselage cross-section
leading to an increased revenue potential through :
- greater passenger comfort with wider seats and
aisle
- greater overhead baggage volume
- greater cargo capacity
- wide-body compatible container capability
- quicker turnrounds.
Advanced technology applied to aerodynamics,
structure, systems and powerplant offer reduced costs
through :
- unmatched fuel efficiency
- more accurate flight path control
- reduced maintenance costs
- increased reliability
- reduced trouble-shooting time.
Introduced for airline service in March 1988, the A320
represents the largest single advance in civil aircraft
technology since the introduction of the jet engine and
results in a major stride forward in airline profitability.
A computer-managed system gives complete
protection against excursions outside the normal flight
envelope and greatly improves the man / machine
interface.
STL 945.7136/97 2.1
2. A319/A320/A321 flight deck layout
STL 945.7136/97 2.3
A319/A320/A321 flight deck – plan view
Capt. sidestick F / O sidestick
F / O nav. bag
3rd occupant seat
Capt. nav. bag
4th occupant
seat (optional)
Coat
stowage
An observer seat aft of the pedestal offers maximum
visibility over all panels.
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