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Extra resources for Airbus A340200, 300, 500, 600) Differences Brochure
REFUEL / DEFUEL VALVES sel FAULT light 10 MODE SELECT switch (guarded at off) MODE SELECT sel Control of the refuel function is via two FCMCs and two FDCs. The operator interface is either through the standard refuel panel, fitted in the lower surface of the fuselage just aft of the undercarriage bay, or through the optional refuel panel and MCDU in the cockpit. A340-500 only FLIGHT OPERATIONS SUPPORT & LINE ASSISTANCE 43 © Training & Flight Operations Support Division Refuel – Defuel A340-200/300 A340-500/600 A340-200/300 A340-500/600 A340-500 only A different fuel tanks arrangement has also led to a different refuel architecture on the A340-500/600.
Fuel Quantity Indicator Fuel Quantity Indicator 2. HI LVL light HI LVL light 3. OVERFLOW light OVERFLOW light 4. INCREASE/DECREASE preselector rocker switch INCREASE/DECREASE preselector rocker switch 5. TRANSF VALVE switch (guarded in CLOSED) APU EMER pushbutton 6. APU EMER pushbutton (guarded) POWER SUPPLY switch (guarded in NORM) 7. POWER SUPPLY switch (guarded in NORM ) HIGH LEVEL TEST switch (guarded) 8. HI LEVEL TEST switch (guarded) REFUEL / DEFUEL VALVES sel 9. REFUEL / DEFUEL VALVES sel FAULT light 10 MODE SELECT switch (guarded at off) MODE SELECT sel Control of the refuel function is via two FCMCs and two FDCs.
Pump control is automatic and depends on trim tank transfer line’s status at the time of operation. On the A340-500/600, the APU is fed via a dedicated line from a tapping of the number one engine’s fuel feed line. The number one engine’s booster pumps normally supply the fuel pressure. However, if these pumps are not selected, then a dedicated APU pump is installed in the line to supply the fuel pressure. The new system removes the Fuel/Air separator, and associated water drainage system. FLIGHT OPERATIONS SUPPORT & LINE ASSISTANCE 36 © Training & Flight Operations Support Division Fuel Transfers Aft Fuel Transfer A340-200/300: Aft fuel transfer towards to trim tank comes: • from the center tank by means of two pumps, when the center tank is not empty • from the inner tanks by means of main 2/3 and standby 2/3 pumps, when the center tank is empty A340-500/600: Introduction of six Aft Transfer/ Jettison pumps: • Enables Aft Transfer and Jettison to be independent of the engine feed system.
Airbus A340200, 300, 500, 600) Differences Brochure