A320 Final Exam 1Aexam with complete
SOLUTIONS
On the approach with all the exterior lights selected ON, which lights will not illuminate
until the landing gear is extended?
a. Turn off only
b. Nose (takeoff only)
c. Nose (Takeoff and Taxy) and turn off only
d. Nose (Takeoff and Taxy) only - ANSc. Nose (Takeoff and Taxy) and turn off only
What is the difference between the cockpit and the passenger oxygen systems?
a. There is no difference, both are served by oxygen cylinders
b. Crew is supplied from an oxygen bottle, passengers are supplied by chemical oxygen
generators
c. Both crew and passengers are supplied with oxygen from chemical oxygen
generators
d. The crew has an oxygen bottle for an emergency back-up supply - ANSb. Crew is
supplied from an oxygen bottle, passengers are supplied by chemical oxygen
generators
If both lanes of ACSC 2 are failed...
a. PACK 1 is inoperative and Pack 2 goes to High Flow
b. PACK 2 is inoperative and there is no effect on PACK 1
c. Both Cabin (FWD & AFT) Trim Air Valves and inoperative
d. ACSC 1 will take over, resulting in normal operation - ANSc. Both Cabin (FWD &
AFT) Trim Air Valves and inoperative
With the FLOW controller set to LO, what could cause the actual flow to be normal?
a. The APU supplying bleed air.
b. The engines supplying bleed air.
c. The cross-bleed valve being OPEN.
d. Temperature demands not being satisfied. - ANSd. Temperature demands not being
satisfied.
When the RAM air is selected on, which of the following statements regarding the Ram
Air Value is true?
a. It should not be opened at a pressure differential of > 1.0 psi.
b. It directs ambient air to the PACKS.
c. It should not be opened above 10,000 ft aircraft altitude.
,It should not be opened above 10,000 fit cabin altitude - ANSa. It should not be opened
at a pressure differential of > 1.0 psi.
What is the meaning of CAB PR LDG EVEL FAULT ECAM?
a. Landing elevation data from the FMGS is not available
b. Wrong selection of landing elevation is made
c. Landing elevation selector is moved out of auto inappropriately
d. Outflow valve is in manual control - ANSa. Landing elevation data from the FMGS is
not available
In flight, which valve will not close if the DITCHING switch is pushed?
a. The RAM AIR VALVE.
b. The OUTFLOW VALVE (if it is selected to MANUAL).
c. The pack FLOW CONTROL VALVE.
d. The Avionics Vent. EXTRACT VALVE. - ANSb. The OUTFLOW VALVE (if it is
selected to MANUAL).
When the EXTRACT pushbutton switch is set at the OVRD position, the system goes
to?
a. Close circuit configuration
b. Open circuit configuration
c. Intermediate circuit configuration
d. No configuration change - ANSa. Close circuit configuration
In flight, if the SKIN AIR temperature is 38°C, in which configuration will the AVIONICS
VENT be?
a. INTERMEDIATE
b. OPEN
c. CLOSED
d. SMOKE - ANSa. INTERMEDIATE
Auto flight. Yaw Bar - ANSa. Below 30ft RA, is LOC signal available, During takeoff in
RWY mode, On landing in FARE/ROLL OUT mode
FAC - control rudder limiter, Both FAC fails? - ANSa. Rudder freezes in current POSN,
Flap down, full range resumed
Inflight, autopilot can be engaged when?
a. At an altitude of 400ft
b. At least 5 seconds after V1 speed
c. At least 5 seconds after takeoff or above 100ft
d. Below 100ft - ANSc. At least 5 seconds after takeoff or above 100ft
After setting the APU MASTER SW to ON, and the START switch is pushed what
happens?
a. The AVAIL light illuminates.
, b. The FAULT light illuminates.
c. The AIR INTAKE FLAP starts to open and the starter engages when the flap is fully
open.
d. The AIR INTAKE FLAP starts to open and the starter engages simultaneously. -
ANSc. The AIR INTAKE FLAP starts to open and the starter engages when the flap is
fully open.
Regarding limitations, which of the following statements is true?
a. The APU may be started at any point in the flight envelope.
b. The waiting time, after three failed start attempts, is 30 minutes.
c. When the LOW OIL LEVEL message appears on the SD the APU must not be
started.
d. The maximum altitude for APU start, when in the ELEC EMER CONFIG, is 30,000 ft.
- ANSa. The APU may be started at any point in the flight envelope.
When should the AUDIO SWITCHING switch be moved from the NORM position?
a. After a failure of the Capt's or F/O's loudspeaker
b. After a failure of RMP 1 and RMP 2
c. After a failure of ACP1 or ACP2
d. After a failure of any RMP - ANSc. After a failure of ACP1 or ACP2
RMP2, if you select VHF1, selected an amber SEL light illuminates...
a. On RMP1
b. On RMP 2
c. On RMP 2 & 3
d. On RMP 1 & 2 - ANSd. On RMP 1 & 2
What alert will trigger in the cockpit when an emergency call is made by the cabin crew?
a. 2 buzzer and ATT light on all 3 ACPs
b. 3 buzzer and ATT light on all 3 ACPs
c. 3 clicks, chine with ATT light on CAPTs ACP
d. 3 buzzer, chine with ATT light on CAPTs ACP - ANSb. 3 buzzer and ATT light on all
3 ACPs
After first engine start (ENG 1) and APU running, which source is supplying AC BUS 1
and AC BUS 2?
a. ENG GEN 2 will supply both buses
b. APU GEN will supply both buses
c. APU GEN to AC BUS 2 & ENG GEN 1 to AC BUS 1
d. APU GEN to AC BUS 1 & ENG GEN 1 to AC BUS 2 - ANSc. APU GEN to AC BUS 2
& ENG GEN 1 to AC BUS 1
Apart from the EMRG GEN, what can supply the AC ESS bus?
a. AC BUS 1, AC BUS 2, AC ESS SHED
b. AC BUS 1, AC BUS 2, BAT 1 (static Inverter)
c. AC BUS 1, AC BUS 2, BAT 2 (static Inverter)
SOLUTIONS
On the approach with all the exterior lights selected ON, which lights will not illuminate
until the landing gear is extended?
a. Turn off only
b. Nose (takeoff only)
c. Nose (Takeoff and Taxy) and turn off only
d. Nose (Takeoff and Taxy) only - ANSc. Nose (Takeoff and Taxy) and turn off only
What is the difference between the cockpit and the passenger oxygen systems?
a. There is no difference, both are served by oxygen cylinders
b. Crew is supplied from an oxygen bottle, passengers are supplied by chemical oxygen
generators
c. Both crew and passengers are supplied with oxygen from chemical oxygen
generators
d. The crew has an oxygen bottle for an emergency back-up supply - ANSb. Crew is
supplied from an oxygen bottle, passengers are supplied by chemical oxygen
generators
If both lanes of ACSC 2 are failed...
a. PACK 1 is inoperative and Pack 2 goes to High Flow
b. PACK 2 is inoperative and there is no effect on PACK 1
c. Both Cabin (FWD & AFT) Trim Air Valves and inoperative
d. ACSC 1 will take over, resulting in normal operation - ANSc. Both Cabin (FWD &
AFT) Trim Air Valves and inoperative
With the FLOW controller set to LO, what could cause the actual flow to be normal?
a. The APU supplying bleed air.
b. The engines supplying bleed air.
c. The cross-bleed valve being OPEN.
d. Temperature demands not being satisfied. - ANSd. Temperature demands not being
satisfied.
When the RAM air is selected on, which of the following statements regarding the Ram
Air Value is true?
a. It should not be opened at a pressure differential of > 1.0 psi.
b. It directs ambient air to the PACKS.
c. It should not be opened above 10,000 ft aircraft altitude.
,It should not be opened above 10,000 fit cabin altitude - ANSa. It should not be opened
at a pressure differential of > 1.0 psi.
What is the meaning of CAB PR LDG EVEL FAULT ECAM?
a. Landing elevation data from the FMGS is not available
b. Wrong selection of landing elevation is made
c. Landing elevation selector is moved out of auto inappropriately
d. Outflow valve is in manual control - ANSa. Landing elevation data from the FMGS is
not available
In flight, which valve will not close if the DITCHING switch is pushed?
a. The RAM AIR VALVE.
b. The OUTFLOW VALVE (if it is selected to MANUAL).
c. The pack FLOW CONTROL VALVE.
d. The Avionics Vent. EXTRACT VALVE. - ANSb. The OUTFLOW VALVE (if it is
selected to MANUAL).
When the EXTRACT pushbutton switch is set at the OVRD position, the system goes
to?
a. Close circuit configuration
b. Open circuit configuration
c. Intermediate circuit configuration
d. No configuration change - ANSa. Close circuit configuration
In flight, if the SKIN AIR temperature is 38°C, in which configuration will the AVIONICS
VENT be?
a. INTERMEDIATE
b. OPEN
c. CLOSED
d. SMOKE - ANSa. INTERMEDIATE
Auto flight. Yaw Bar - ANSa. Below 30ft RA, is LOC signal available, During takeoff in
RWY mode, On landing in FARE/ROLL OUT mode
FAC - control rudder limiter, Both FAC fails? - ANSa. Rudder freezes in current POSN,
Flap down, full range resumed
Inflight, autopilot can be engaged when?
a. At an altitude of 400ft
b. At least 5 seconds after V1 speed
c. At least 5 seconds after takeoff or above 100ft
d. Below 100ft - ANSc. At least 5 seconds after takeoff or above 100ft
After setting the APU MASTER SW to ON, and the START switch is pushed what
happens?
a. The AVAIL light illuminates.
, b. The FAULT light illuminates.
c. The AIR INTAKE FLAP starts to open and the starter engages when the flap is fully
open.
d. The AIR INTAKE FLAP starts to open and the starter engages simultaneously. -
ANSc. The AIR INTAKE FLAP starts to open and the starter engages when the flap is
fully open.
Regarding limitations, which of the following statements is true?
a. The APU may be started at any point in the flight envelope.
b. The waiting time, after three failed start attempts, is 30 minutes.
c. When the LOW OIL LEVEL message appears on the SD the APU must not be
started.
d. The maximum altitude for APU start, when in the ELEC EMER CONFIG, is 30,000 ft.
- ANSa. The APU may be started at any point in the flight envelope.
When should the AUDIO SWITCHING switch be moved from the NORM position?
a. After a failure of the Capt's or F/O's loudspeaker
b. After a failure of RMP 1 and RMP 2
c. After a failure of ACP1 or ACP2
d. After a failure of any RMP - ANSc. After a failure of ACP1 or ACP2
RMP2, if you select VHF1, selected an amber SEL light illuminates...
a. On RMP1
b. On RMP 2
c. On RMP 2 & 3
d. On RMP 1 & 2 - ANSd. On RMP 1 & 2
What alert will trigger in the cockpit when an emergency call is made by the cabin crew?
a. 2 buzzer and ATT light on all 3 ACPs
b. 3 buzzer and ATT light on all 3 ACPs
c. 3 clicks, chine with ATT light on CAPTs ACP
d. 3 buzzer, chine with ATT light on CAPTs ACP - ANSb. 3 buzzer and ATT light on all
3 ACPs
After first engine start (ENG 1) and APU running, which source is supplying AC BUS 1
and AC BUS 2?
a. ENG GEN 2 will supply both buses
b. APU GEN will supply both buses
c. APU GEN to AC BUS 2 & ENG GEN 1 to AC BUS 1
d. APU GEN to AC BUS 1 & ENG GEN 1 to AC BUS 2 - ANSc. APU GEN to AC BUS 2
& ENG GEN 1 to AC BUS 1
Apart from the EMRG GEN, what can supply the AC ESS bus?
a. AC BUS 1, AC BUS 2, AC ESS SHED
b. AC BUS 1, AC BUS 2, BAT 1 (static Inverter)
c. AC BUS 1, AC BUS 2, BAT 2 (static Inverter)
