STL 472.502/90 Issue 6
A340 Fuel System
7.4
• In normal operation, each engine is independently
supplied by a continuously operating booster pump,
located in a dedicated collector box.
In the event of a pump failure, each engine is
automatically fed by a standby pump.
Collector boxes are maintained full by a jet pump
transfer action using booster pump pressure.
In cruise conditions, a single booster pump is able to
supply flow to all four engines.
• A crossfeed valve is associated with each engine. It
connects the engine and its associated pumps to the
X-FEED line. This allows any pump to supply any
engine.
All crossfeed valves open automatically in electrical
emergency configuration and during jettison operation.
• Supply of fuel to each engine may be shut off by an
engine LP valve driven by a double motor actuator. It
is controlled by either the ENG FIRE pushbutton or
the ENG master lever.
• Automatic control of transfer from center to inner
tanks is initiated, provided either center tank pump
pushbutton is selected on.
With fuel in the center tank and CTR TK pumps
running, both inner inlet valves are used
independently to cycle the inner tank contents
between underful and high level. (Underful is set at
approximately 2000 kg below high level).
When the center tank is empty, the pumps are
automatically controlled off, and both inner inlet
valves lose.
• Automatic transfer of fuel from the outer tanks is
performed by gravity. This occurs when center and
trim tanks have been emptied and when either inner
tank reaches 4000 kg.
Outer tank fuel transfer valves are used to cycle the
inner tanks contents between 4000 and 4500 kg.
These valves are closed when outer tanks are empty
for 5 minutes.
• Transfer to inner tanks can be manually selected
through the OUTR TK XFR pushbutton.
When selected ON, all inner tank fuel transfer, outer
inlet and inner inlet valves are controlled OPEN.
• Automatic control of transfer from ACT to center tank
occurs after takeoff slats restriction, provided the
center tank contains less than 23000 kg.
Engine feed
Summary of Contents for A340 Series
Page 2: ...STL 472 502 90 Issue 6...
Page 4: ...STL 472 502 90 Issue 6...
Page 5: ...STL 472 502 90 Issue 6 1 General 1 1...
Page 18: ...STL 472 502 90 Issue 6...
Page 19: ...STL 472 502 90 Issue 6 2 Flight Deck Layout 2 1...
Page 24: ...STL 472 502 90 Issue 6 A340 Flight Deck Layout 2 6 Pilots field of vision...
Page 26: ...STL 472 502 90 Issue 6 A340 Flight Deck Layout Control and indication panels shaded 2 8...
Page 30: ...STL 472 502 90 Issue 6 A340 Flight Deck Layout 2 12 Main instrument panels...
Page 32: ...STL 472 502 90 Issue 6 A340 Flight Deck Layout 2 14...
Page 37: ...STL 472 502 90 Issue 6 3 Electrical System 3 1...
Page 41: ...STL 472 502 90 Issue 6 A340 Electrical System 3 5 Control and display Overhead panel ECAM...
Page 43: ...STL 472 502 90 Issue 6 4 Hydraulic System 4 1...
Page 44: ...STL 472 502 90 Issue 6 A340 Hydraulic System 4 2 Architecture...
Page 46: ...STL 472 502 90 Issue 6...
Page 47: ...STL 472 502 90 Issue 6 5 Flight Controls EFCS 5 1...
Page 56: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 10 Schematic diagram...
Page 58: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 12 Pitch control...
Page 60: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 14 Roll control...
Page 62: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 16 Yaw control...
Page 64: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 18 Left intentionally blank...
Page 66: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 20 Slats flaps controls...
Page 68: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 22 Slats flaps control...
Page 70: ...STL 472 502 90 Issue 6 A340 Flight Controls EFCS 5 24 ECAM system page...
Page 86: ...STL 472 502 90 Issue 6...
Page 87: ...STL 472 502 90 Issue 6 6 Landing Gear 6 1...
Page 88: ...STL 472 502 90 Issue 6 A340 Landing Gear 6 2 Left intentionally blank...
Page 90: ...STL 472 502 90 Issue 6 A340 Landing Gear 6 4...
Page 96: ...STL 472 502 90 Issue 6 6 10 A340 Landing Gear ECAM system page...
Page 97: ...STL 472 502 90 Issue 6 7 Fuel System 7 1...
Page 104: ...STL 472 502 90 Issue 6 A340 Fuel System 7 8 Controls and displays...
Page 106: ...STL 472 502 90 Issue 6 A340 Fuel System 7 10 Refueling system...
Page 108: ...STL 472 502 90 Issue 6...
Page 109: ...STL 472 502 90 Issue 6 8 Engine Controls 8 1...
Page 111: ...STL 472 502 90 Issue 6 A340 Engine Controls CFM56 8 3 FADEC architecture...
Page 114: ...STL 472 502 90 Issue 6 A340 Engine Controls 8 6 Thrust control operations...
Page 117: ...STL 472 502 90 Issue 6 9 Auxiliary Power Unit APU 9 1...
Page 119: ...STL 472 502 90 Issue 6 A340 Auxiliary Power Unit 9 3 Controls and display...
Page 120: ...STL 472 502 90 Issue 6...
Page 121: ...STL 472 502 90 Issue 6 10 Automatic Flight System 10 1...
Page 144: ...STL 472 502 90 Issue 6 A340 Automatic Flight System Flight Management 10 24 MCDU ND...
Page 152: ...STL 472 502 90 Issue 6...
Page 153: ...STL 472 502 90 Issue 6 11 Environmental Control System 11 1...
Page 154: ...STL 472 502 90 Issue 6 A340 Environmental Control System 11 2 Air conditioning schematic...
Page 156: ...STL 472 502 90 Issue 6 A340 Environmental Control System 11 4 Air conditioning Air bleed...
Page 158: ...STL 472 502 90 Issue 6 A340 Environmental Control System 11 6 Avionics ventilation...
Page 160: ...STL 472 502 90 Issue 6 A340 Environmental Control System 11 8 Cabin pressure control...
Page 162: ...STL 472 502 90 Issue 6...
Page 163: ...STL 472 502 90 Issue 6 12 Electronic Instrument System EIS 12 1...
Page 166: ...STL 472 502 90 Issue 6 A340 Electronic Instrument System 12 4 EFIS ECAM architecture...
Page 170: ...STL 472 502 90 Issue 6 A340 Electronic Instrument System 12 8 Reconfiguration F O on EFIS DMC3...
Page 172: ...STL 472 502 90 Issue 6 A340 Electronic Instrument System 12 10 DU reconfiguration...
Page 174: ...STL 472 502 90 Issue 6 12 12 A340 Electronic Instrument System EFIS Control panels...
Page 177: ...STL 472 502 90 Issue 6 12 15 A340 Electronic Instrument System EFIS ND ROSE NAV mode...
Page 179: ...STL 472 502 90 Issue 6 12 17 A340 Electronic Instrument System EFIS ND ROSE ILS mode...
Page 185: ...STL 472 502 90 Issue 6 12 23 A340 Electronic Instrument System ECAM Display unit...
Page 191: ...STL 472 502 90 Issue 6 12 29 A340 Electronic Instrument System ECAM Failure related mode...
Page 194: ...STL 472 502 90 Issue 6...
Page 195: ...STL 472 502 90 Issue 6 13 1 13 Radio Management and Communication...
Page 196: ...STL 472 502 90 Issue 6 A340 Radio Management and Communication 13 2 Radio Management Panel RMP...
Page 198: ...STL 472 502 90 Issue 6 A340 Radio Management and Communication 13 4 RMP architecture...
Page 202: ...STL 472 502 90 Issue 6...
Page 203: ...STL 472 502 90 Issue 6 14 A340 Central Maintenance System CMS 14 1...
Page 204: ...STL 472 502 90 Issue 6 A340 Central Maintenance System 14 2 Left intentionally blank...
Page 208: ...STL 472 502 90 Issue 6 A340 Central Maintenance System 14 6 Examples of use...
Page 210: ...STL 472 502 90 Issue 6...