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normal backup operation
A321 stretched version
132’0" with 8 FWD and 5 AFT doors
Z = 0
vertical stabilizer
A320 X = 0
2.54 m forward of radome
X axis
fuselage
Y axis
wings
Caution
procedures to avoid damage
Zone 404
nacelles and pylons
Electrical clock
UTC, elapsed time, chrono
DMC
processes data and images for displays
ECAM
Electronic Centralized Aircraft Monitoring System
EIS
6 displays (2 PFD, 2 ND, Upper ECAM/EWD, Lower ECAM/SD)
CFDS
centralizes and memorizes system failure info
SSFDR and CVR
rear fuselage, THS compartment
FWC
red warnings, SDAC
RAT activation
pressurizes blue hydraulic system
RAT manual deploy
false
On ground AC/DC bus without full aircraft
true
ISIS
replaces standby horizon, altimeter, airspeed
ISIS power
battery
MMR
GPS + ILS
Flight director symbol
PFD
ADIRU
ADR + IR, independent channels
ILS ground facility
marker beacons, glide slope, localizer
Autothrust disengage
instinctive disconnect push button
Autoflight side stick/levers
no movement
AFS FG
autopilot, flight director, autothrust
ACP
transmit/receive audio signals
ACP blue light
passenger call
DEU B
crew functions
DEU A
passenger functions
RMP
tunes comm/nav receivers
ATSU
manages communication message exchange
ATSU
heart of ATIS
ATA 33 exterior lights
taxi, runway turnoff, takeoff/landing, wing/engine scan, nav lights, strobes, beacon, logo
Nose landing gear lights
runway turnoff, taxi, takeoff
FAP
purser station, forward cabin
Crossfeed valve
connects L/H and R/H fuel
A321 fuel pumps
4 booster, 2 jet
Outer wing tank
cannot directly supply engine/APU
FDU
3 (engine, engine, APU)
Fire detector location
pylon, fan, core
Auto extinguishing
lav waste bin, APU
AEVC
avionics cooling/smoke controller
APU
supplies electrical + pneumatic (AC, engine start)
APU ground-only
auto shutdown + auto extinguish
Engine HP compressor
9 stages
HP turbine
1 stage
LP compressor
5 stages (incl. fan)
LP turbine
4 stages
Starter drives
N2
N2
HP spool
Engine blades
36 hollow titanium, 80% thrust
Auto relight
engine anti-ice on
Air bleed
APU, GPU, engine
Crossbleed valve
connects pneumatic systems
Crossbleed control
BMC
Pneumatic system
HP air, AC, engine start, anti-ice, water pressurization, hydraulic reservoir pressurization
Pack bypass valve
modulates temp, prevents icing
Cabin recirc air
mixer unit
Pressurization valve
outflow valve
Probe not heated on ground with one engine
TAT probe
WHC 1
left windshield, left side windows
Windshield wiper >200 kts
false
Yellow hydraulic pressurization
EDP, electric pump, PTU
PTU auto start
500 psi differential
Green system EDP
1
RAT automatic deploy
100 kts + loss of all AC power
A318/A319 gear
anti-skid, auto brake, brake fans, tire monitoring
BSCU
braking, anti-skid, auto brake, brake temp
Normal gear operation
green hydraulic
Mechanical backup
THS, rudder
Hydraulic/manual control
THS, rudder
Speedbrake
spoilers 2, 3, 4
Ground spoilers
spoilers 1, 2, 3, 4, 5
Windows
ATA 56
A320 to A318
4.5 FWD, 7 AFT
Radome
quartz fiber reinforced plastic
A320 emergency exits
8 (no overwing, type 1 doors)
Pax door armed
lever up, pin installed
Cabin systems
controlled/tested/monitored by CIDS
Pax doors
single lane
Overwing exits
dual lane slides
Cabin oxygen
automatic (rapid decompression ≥14,000 ft) + manual MRT
Oxygen masks
one pulled deploys all
Crew oxygen
fixed cylinder + mask + PBE hood
Potable/lav servicing
restricted to avoid cross-contamination
Enhanced vacuum
controlled by CIDS via VSCF
Vacuum generator stops
16,000 ft
Lavatory waste/sink water
heated drain mast
Portable oxygen bottles and PBE location
cabin and cockpit
Green HYD reservoir location
MLG bay aft side
PTU description
transfers hydraulic power but not hydraulic fluid
Ground system for maintenance and cargo doors
Yellow HYD Elec pump
Potable water servicing
with or without electrical power supply
Optional navigational system
Heads Up Display (HUD)
A320 overwing emergency exits
4
Manual radio navigation tuning
Multipurpose Control Display Unit (MCDU)
Transmit/receive audio signals
Audio Control Panel (ACP)
Pilot oxygen tank location
LH Avionics compartment