Note: Answer $5($Five$)$ questions only

Q$1$: write $($T$)$ for true statement or $($F$)$ for false statement for the following: $($FUEL$)$

$1-$ There are $6$ six operations fuel pumps which all operate during any trip for A$320$ airplane.

$2-$ The total fuel quantity in all tanks for $A320$ is $19000kg.$

$3-$ Never to contain a large amount of fuel without needs and to ensure consume all of it in a twin flight.

$4-$ There are three basic types of fuel tanks designed for use in aircraft.

$5-$ The basic of elementary fuel system is consists of tank$,$ drain cock, shut$-$off valve, fuel flow meter, high pressure pump, venting system, and fuel quantity gauge.

$6-$ The most popular one in our days of fuel is $($Jet A$)$ and it's also used with warplanes.

$7-$ There aren't live bacteria inside fuel tank.

$8-$ There are four abnormal flight problems occur in A$320$ fuel system.

$9-$ For abnormal fuel system case, the amber light can visualize on ECAM only for fuel pump frailer.

$10-$Fuel temperature inside fuel $-50C$ is the low limit in outer tank of A$320.$

Q$2$: write $($T$)$ for true statement or $($F$)$ for false statement for the following: $($APU$)$

$11-$APU GEN. produce $115V,400HZ$ Frequency, $3$ phases, $90$ KVA.

$12-$ The main instruments attached with APU gear box are flap motor, oil pump, and APU GEN.

$13-$ APU produce electric power and bleed air for anti$-$icing.

$14-$ To produce the sufficient thrust in APU, to produce electric power and air bleed, there are two compressors achieved.

$15-$ APU in not self$-$contained unit that makes the aircraft independent of external pneumatic and electrical power supplies.

$16-$Starting APU sequence start from press the MASTER s wpb and wait few second then press START pb$.$

$17-$APU ECAM contents of APU GEN indicators, number of revolution for APU shaft, EGT, BLEED pressure, and many indicators related with APU.

$18-$Statement $"$ FLAP OPEN" on ECAM displayed in green when APU air intake flap is fully open $($MASTER SW ON$).$

$19-$ Maximum EGT with APU running: $675C.$

$20-$ Maximum EGT with APU start: $1090C.$

Q$3$: Q$1$: write $(T)$ for true statement or $($F$)$ for false statement for the following: $($F$/$CTL$)$

$21-$ Flight control surfaces are all electrically activated and hydraulically controlled.

$22-$Pitch axis occurred by elevator and stabilizer.

$23-$Speed brakes controlled by electric.

$24-$ The pilots use a single switch on the center pedestal to set the rudder trim.

$25-$There is no manual switch for trimming the ailerons.

$26-$ Flight control surfaces computers are, $2$ ELACs, $3$ SECs, $2$ FACs, and $2$ FCDCs$.27-$L$.$ELEV moved using $B$ and $Y$ HYD systems.

$28-$ Spoiler #$5$ moved using G HYD system B$.29-$ SIDESTICKS is spring$-$loaded to neutral. $30-$The symbol $(-)$ mean the spoilers retracted $($WHITE$).$