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BLEEDCAUTION, do not use HP GND air with APU bleedAVIONICS VENTILATIONCONFIGURATIONS: CLOSED, on GND (skin32°-35°C) then EXTRACT VLV partially opens OPEN, on GND (skin>9°-12°C) SMOKE CONFIG Air from avionics bay SKIN EXCH OUTLET BYPASS VLV AEVC [DC1] [DC ESS SHED] SKIN AIR INLET VLV SKIN HEAT EXCHANGER SKIN EXCH ISOL VLVCAUTION, do not use GND AIRCOND air with air from packs simultaneouslyPACK 1 FLOW CONTROL VALVE [DC ESS SHED] ZONE CTL CH1 [AC1/DC1
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FWD CARGOCOMP
WING ANTI ICE VLV[AC ESS SHED]
Valve closes if unpowered
OUTFLOWVALVE
SAFETYVALVES
only SLATS 3,4 & 5are heated
5th
9th
PACK 1FLOWCONTROLVALVE[DC ESSSHED]
PACK 2FLOWCONTROLVALVE [DC2]
HOT AIRPRESSREG VLV
TRIMAIR VALVES
TRIMAIR VALVES
OVERPRESSVALVE (85psi)
pressureindication
X-BLEED VLVAUTOCTL [DC2]MANCTL [DC ESS SHED]
HP GNDCONNECT
CAUTION, do not use HP GND air with APU bleed
AIRCONDGND
CONNECT
APUBLEEDVALVE
CABINAMBIENT
AIR
INLETISOLVALVE
OUTLET ISOLVALVE
EXTRACT FAN[AC1]
FUEL A319/A320
A321 FUEL
ENGINE
(ENG 1 only)
HYDRES
WATERTANK LOOP A
LOOP B
PACK2
PACK1
PACK 1 CTLCH1 [AC1/DC1]CH2 [AC2/DC2]
ZONE CTLCH1 [AC1/DC1]CH2 [AC2/DC2]
AEVC[DC1]
[DC ESSSHED]
BLEED MONITORINGCOMPUTER BMC 1 [DC ESS SHED]BMC 1 [DC2]
MIXINGUNIT
FLAPVALVE
COCKPIT
AFTCABIN
CABIN AIR(85% recycle air)
CABINAIR
CAUTION, do not use GND AIRCOND air with air from packs simultaneously
FWDCABIN
SATCOM
EMERRAM AIR[DC ESS]
SKIN AIRINLET VLV
FILTER
SKINEXCHISOLVLV
SKIN AIREXTRACTVLV
SKIN HEATEXCHANGER
HOT BLEEDCOLD FAN AIRCOLD AIR FROM PACKMIXED CONDITIONNED AIR
CAB FAN 1[AC1]
CAB FAN 2[AC2]
FILTER
FILTER
ZONE CTLCH1 [AC1/DC1]CH2 [AC2/DC2]
CPC 1[DC ESS]
ELECTRICAL SUPPLYENG 1 loop A [DC ESS], loop B [DC2]ENG 2 loop A [DC2], loop B [DC ESS]APU loop A & B[DC BAT] ENG 1&2 BTL 1 squib A [HOT1] squib B [HOT2]ENG 1&2 BTL 2 squib A [DC2] squib B [DC2]APU BTL squib A [HOT1] squib B [DC BAT]APU auto extinguish [DC BAT]
CPC 2[DC2]
CARGOVENTILATION
CONTROL
SMOKE DETECTCONTROL UNIT
SDCUCH1 [DC ESS SHED]
CH2 [DC2]
ELECTRONICCONTROL BOX
[BAT]
FQICH1 [DC ESS SHED]
CH2 [DC2]
EIUENG1 [DC BAT]ENG2 [DC ESS]
MAN V/SSWITCH
BLEED AIRCONDAVIONICS VENTILATION
PRESSURIZATION
FIRE PROTECTION& CARGO VENT
APU
Regulated pressure 44 +/- 4 psi
HP VLVENG 1 [DC ESS SHED]ENG 2 [DC2]
BLEED VALVEENG 1 [DC ESS SHED]
ENG 2 [DC2]
STARTER VLV
FAN AIR VALVEENG 1 [DC ESS SHED]ENG 2 [DC2]regulates BLEED temp at 200°C
temperatureindication
Leak detection- single loop for APU and pylon ducts- double loop for wing ducts
Temperature control- HI TEMP if 290°C > 5sec or 270°C > 15sec or 257°C > 55sec- LO TEMP if < 150°C
Pressure control- HI PRESS if > 60psi - LO PRESS if < 4psi
MOT 1[DC ESS]
MANMOT
[DC BAT]
MOT 2[DC2]
- 2 safety valves (max 8.6psi or -.25psi)- if RAM AIR ON and ∂p<1psi, outflow vlvis 50% open (if not in MANUAL)
- EXCESS CAB ALT (>9550+/-350ft)
PACK 2 CTLCH1 [AC1/DC1]CH2 [AC2/DC2]
AVIONICSEQPMT
COCKPITPANELS
SKIN EXCHINLETBYPASSVLV
SKIN EXCHOUTLET
BYPASS VLV
Air from avionics bay
AFTCARGOCOMP
BULK
cargounder-floor
AIRCONDINLETVALVE
CLOSED, on GND (skin<9°-12°C), FLT(skin<32°-35°C)if (skin>32°-35°C) then EXTRACT VLV partially opensOPEN, on GND (skin>9°-12°C)
SMOKE CONFIG
ENG A/ICE VALVEENG 1 [DC1]ENG 2 [DC2]
valve opens if unpowered
1
1
APU PUMP[DC BAT][AC ESS
SHED]
APU LP VLV[DC BAT]
[HOT 1]
2
LH 1[AC1][DC1][DC ESS]
XFR VALVES1 [DC ESS SHED]
2 [DC2]
LP VALVEMOT 1 [DC ESS]
MOT 2 [DC2]
OUTER TANKS2 x 704kg
INNER TANKS2 x 5540kg
TOTAL TANKS CAPACITY (den 0.80kg/l)
19088kg
TOTAL CAPACITY(den 0.80kg/l)
18960kg
CENTER TANK6600kg
CENTER TANK6560kg
LH 2[AC2][DC2]
CTR1[AC1][DC1]
CTR2[AC2][DC2]
X-FEEDMOT 1 [DC ESS SHED]MOT 2 [DC1]
1 2
RH 1[AC1][DC1][DC ESS]
RH 2[AC2][DC2]
LP VALVEMOT 1 [DC ESS]MOT 2 [DC2]
jet pump
WING PUMPSTANK PUMPS
P
CTR XFRVLVL[DC1]R[DC2]
DEFUELXFRVLV
REFUELVALVE VENT TANK
~50kg
REFUEL VALVE[DC2] refueling on
batteries with [HOT1]
REFUELCOUPLING
REFUELCOUPLING
refueling / defueling linesfeeding lines
SQUIBS[DC BAT]
A321 only
A321 only
LIMITATIONSRPM min 95%, max 107% (auto shut down)running EGT max 682°C (5sec) or 700-742start EGT max 900°C > 25'000ftstart EGT max 982°C < 25'000ftLOW OIL LEVEL => 10 hrs APU ops start cycles: S 1min S 1min S 60minEnveloppe: START with AC pwr up to 39'000ftSTART with EMER ELEC pwr up to 25'000ftBLEED ON 2packs max 15'000ft, 1 pack max 20'000ftBLEED ON for engine start max 20'000ftBLEED for WING A/ICE not permittedAPU FUEL FLOW ~130 kg/hr
!!! NOT FOR OPERATIONAL USE !!! ©Pierre-Michel Gasser, 14.05.2007
APU
FUEL IMBALANCE A319/A320INNER TK Full, max 1500kgINNER TK 4300kg, max 1600kgINNER TK 2250kg, max 2250kgno limitations below 2250kgOUTER TK max 530kg, if OUTER+INNER same or INNER of empty OUTER equal or higher (up to 3t) of opposite INNER
A321 FUEL IMBALANCEWING TK Full, max 1350kg
WING TK 4000kg, max 1500kgWING TK 2350kg, max 2350kg
no limitations below 2350kg
FUEL TEMPERATUREJET A1 min -43°C max +54°CJET A min -36°C max +54°C
JET B, JP-4, JP-5, JP-8, RT, TS-1 see OM B 1.1.1
PACK CTLPrim fail => flow not optimized
Sec fail => ECAM sgnal lostBoth fail => 15°C by a/ice vlv
ZONE CTLPrim fail => 24°C by packs
Sec fail => no effectBoth fail => 20°C pack 1
10°C pack 2
SMOKE DETECTORS
FIRE DETECTORSF
FFFF
FF
FF
B
FIREX BOTTLESB
B
B1
B2
OUTER to INNER TRANSFER- XFR valves open when INNER have ~750kg- T/O only with Outer TK full- Automatic XFR after landing(to avoid, switch REFUEL panel PWR ON!)or transfer via DEFUEL/XFR valvesee OMB vol.2 1.4 / 28.4
BLOWERFAN[AC1]
EXTRACTFAN[AC2]
ENGPMP
FUEL METERING VLV
HP VLV [DC ESS]
FF
FUELNOZZLES
ENG cool-down time 3'or 1' if required by ops
A319: CFM56-5B6/2 23'500lbsA320: CFM56-5B4/2 27'000lbsA320E: CFM56-5B4/P 27'000lbsA321: CFM56-5B1/2 30'000lbsN1 100% = 5000 rpmN2 100% = 14460 rpm
FUEL/OIL HEAT
IDG OIL COOLER
SERVO FUELHEATER
CENTER to WING TRANSFER-Valve opens until wing tank is full then wait
until 250kg are used and re-opens- Gravity transfer from CTR TK
only possible if >2000kg in center tank these
are trapped
FADECENG1&2 CH A [DC ESS]
ENG1 CHB [DC BAT]ENG2 CHB [DC2]
IGNITIONENG1&2 A [AC ESS]
or [AC STAT INV]ENG1 B [AC1]ENG2 B [AC2]
WING TANKS2 x 6200kg
APUSTARTER
[BAT]
CONFIGURATIONS: