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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.

The right pedal controls the right main landing gear brakes, and the rear wheel brakes of the center landing gear FLIGHT OPERATIONS SUPPORT & LINE ASSISTANCE 57 © Training & Flight Operations Support Division Autobrake The autobrake is still comprised of three modes on the A340-200/300 family, but has been extended to six modes on the A340-500/600. On the A340-200/300 aircraft, autobrake control is achieved via a deceleration target, based on a target speed / aircraft speed comparison. It is, therefore, dependent on tachometer wheel speed acquisition.

The modification of the two inner tanks has also led to a change in the collector cell arrangement, which may be seen in the opposite diagram. 551lbs/US Gal FLIGHT OPERATIONS SUPPORT & LINE ASSISTANCE 34 © Training & Flight Operations Support Division A340-600 Despite the lack of a rear center tank, the A340-600’s larger wing means that significantly more fuel may be stored than on the A340-200/300. 551lbs/US Gal FLIGHT OPERATIONS SUPPORT & LINE ASSISTANCE 35 © Training & Flight Operations Support Division APU FEED A340-200/300 A340-500/600 On the A340-200/300 aircraft, the APU is fed from the trim tank transfer line and is independent of the FCMC.

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