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CPL Test Series
Question Bank
Questions for FIRE EXTINGUISHER 1002 -1050
Answer the following questions
Test Mode
Training Mode
1.
A gaseous sensor/responder tube fire sensor is tested by
checking the continuity of the system with a test switch
checking the wiring harness for faults but not the sensor
heating up the sensor with test power connection
checking the sensor with pressurized gas.
2.
In accordance with JAR-OPS 1, during and following an emergency descent, each occupant of the cockpit seats on duty must have access to a minimum amount of oxygen in:1. order to maintain a supply throughout the entire flight time where the cabin altitude pressure is greater than 13000 ft.2. order to maintain a supply throughout the entire flight time where the cabin altitude pressure is greater than 10000 ft and smaller than 13000 ft minus 30 minutes.3. no case less than 30 minutes for airplanes certified to fly up to 25000 ft.4. no case less than 2 hours for airplanes certified to fly at over 25000 ft.The combination regrouping all the correct statements is
1, 2.
1, 2, 3 et 4.
1,4.
1, 2, 4.
3.
The purpose of the proximity of the emergency evacuation path marking system is to
to be used only at night.
replace the overhead emergency lighting during an emergency evacuation with a thick smoke
replace the overhead emergency lighting in case of failure
mark only the exits at the floor level
4.
An airplane whose maximum approved passenger seating configuration is 7 to 30 seats must be equipped with at least
3 hand fire-extinguishers conveniently located in the passenger compartment
1 hand fire-extinguisher conveniently located in the passenger compartment.
4 hand fire-extinguishers conveniently located in the passenger compartment
2 hand fire-extinguishers conveniently located in the passenger compartment
5.
When a wire type fire system is tested
a part of the wire is totally heated
Only the warning function is tested.
the wire is totally heated.
the wiring and the warning are tested.
6.
Some emergency exits must be equipped with devices so as to help the occupants to get out and reach the ground if their threshold is at a height above the ground greater than:
8 ft, aeroplane on the ground, landing gear extended
6 ft, aeroplane on the ground, one main gear or nose gear collapse
8 ft, aeroplane on the ground, one main gear or nose gear collapse.
6 ft, aeroplane on the ground, landing gear extended.
7.
A Continuous-Loop-Detector-System is a
Carbon dioxide warning system
Fire fighting system
Smoke detection system
Fire detection system
8.
An airplane whose maximum approved passenger seating configuration is 401 to 500 seats must be equipped with at least
7 hand fire-extinguishers conveniently located in the passenger compartment
8 hand fire-extinguishers conveniently located in the passenger compartment
5 hand fire-extinguishers conveniently located in the passenger compartment.
6 hand fire-extinguishers conveniently located in the passenger compartment
9.
When a bimetallic strip is used as a switch in a fire detection loop, a fire alarm is triggered after a delay. The purpose of this delay is to
delay the triggering of the fire extinguinshers and increase their efficiency
avoid false alarms in case of vibrations
wait for the triggering of the second fire detection loop in order to confirm the fire
allow temperatures to equalise
10.
In accordance with JAR-OPS 1, an airplane must be equipped with equipment or systems at each emergency exit that allow to reach the ground safely in the case of an emergency when the sill height of the passenger emergency exit is higher than
1,83 m.
1,80 m.
1,86 m.
1,89 m.
11.
The most common extinguishing agent used in gas turbine engine fire protection system is
Freon
Powder.
CO2.
Water
12.
In order to enable a fire to be controlled as quickly as possible, the fire detectors are located in the highest risk compartments. Theses compartments are :1. the main landing gear wheel wells2. the fuel tanks3. the oil tanks4. the auxiliary power unit5. around the enginesThe combination regrouping all the correct statements is
2,5
1,2,3,4,5
1,4,5
2,3
13.
When quick donning masks are in use, the pilot is
only able to receive
able to radiotelephone.
only able to transmit
not able to do any radio communication.
14.
An airplane whose maximum approved passenger seating configuration is greater than 60 seats must be equipped with at least
4 HALON 1211 fire-extinguishers
2 HALON 1211 fire-extinguishers
1 HALON 1211 fire-extinguisher
3 HALON 1211 fire-extinguishers
15.
Smoke detectors fitted on transport aircraft are of the following type
electrical
magnetic
optical or ionization
chemical
16.
An airplane whose maximum approved passenger seating configuration is greater than 600 seats must be equipped with at least
9 hand fire-extinguishers conveniently located in the passenger compartment
8 hand fire-extinguishers conveniently located in the passenger compartment.
6 hand fire-extinguishers conveniently located in the passenger compartment
7 hand fire-extinguishers conveniently located in the passenger compartment
17.
A manual inflation handle
operates a hand pump for manual inflation of a slide
is generally not applied on slides
serves to inflate a life jacket when the normal inflation function fails
serves to actuate inflation of a slide when automatic inflation fails
18.
Ion detectors are devices used in aircraft for systems protection. They detect
overtemperature and fire.
fire.
smoke.
overtemperature.
19.
An airplane whose maximum approved passenger seating configuration is 501 to 600 seats must be equipped with at least
5 hand fire-extinguishers conveniently located in the passenger compartment
7 hand fire-extinguishers conveniently located in the passenger compartment
6 hand fire-extinguishers conveniently located in the passenger compartment
8 hand fire-extinguishers conveniently located in the passenger compartment
20.
When a continuous element of a fire detection system is heated:1. its resistance decreases.2. its resistance increases.3. the leakage current increases.4. the leakage current decreases.The combination regrouping all the correct statements is
1, 4
2, 3
2, 4
1, 3
21.
Continuous loop fire detector systems operate on the principle that an increase in temperature produces
a decrease in pressure
a decrease in resistance
a decrease in the reference current
an increase in resistance
22.
An airplane whose maximum approved passenger seating configuration is 301 to 400 seats must be equipped with at least
5 hand fire-extinguishers conveniently located in the passenger compartment
4 hand fire-extinguishers conveniently located in the passenger compartment
6 hand fire-extinguishers conveniently located in the passenger compartment
3 hand fire-extinguishers conveniently located in the passenger compartment
23.
Generally, when the fire handle of the fire-extinguishing system on an aircraft is pulled, the effects are :1. closing of the LP valve of the fuel system2. opening of the air bleed valves and HP valves on the engine concerned3. setting of extinguishing systems4. closing of the isolation and de-icing valves5. isolation of the associated electric current generators6. immediate discharge of extinguishing agentThe combination regrouping all the correct statements is
1,3,4,5
2,3,4,5
1,2,5,6
1,3,4
24.
In accordance with JAR-OPS 1, an airplane whose maximum take-off mass exceeds 5 700 kg or whose maximum approved passenger seating configuration is greater than 9 seats and smaller than 200 seats must be equipped with a
crash axe and a crow-bar in the passenger compartment
crash axe in the cockpit and a crow-bar in the passenger compartment.
crow-bar in the cockpit and a crash axe in the passenger compartment
crash axe or a crow-bar in the pilot compartment.
25.
Evacuation slide inflation is ensured by
pressurized air from the air conditioning system
a pressurized gas canister combined with the slide itself.
the aircraft's general pneumatic circuit
a manual pump, used when needed by the cabin crew.
26.
In transport aeroplanes overheat detection systems are installed in the
landing gear bays / wheel wells
cabin.
tyres.
fuel tanks
27.
The most suitable means for extinguishing a magnesium fire on the ground is
carbon dioxide
freon.
water.
sand.
28.
With engine fire alarm activated, the extinguisher discharge
does not need the engine to be stopped
is the pilot's task
is automatic after a delay to allow the pilot to stop the engine
is automatic and immediate
29.
The indication of the fire detection systems is performed by a
warning light
gear warning
warning light and a warning bell (or aural alert).
warning bell
30.
If inflammable gaseous materials, like propane for example, are set on fire, the following extinguisher types should be used for fire fighting
CO2 and water type extinguishers
BCF and CO2 type extinguishers
Water type extinguishers
Dry and water type extinguishers
31.
On an aircraft provided with resistance and capacitance variation type fire detection loops, a fire alarm is initiated by a temperature increase detected
only in a uniform way along the loops
only at an isolated point of the loops
at any isolated point of the loops or else generally on all the loops
on at least one loop
32.
In accordance with JAR-OPS 1, the minimum requirement for the survival oxygen needed to supply 100 % of the passengers during and following an emergency descend is
30 minutes
the entire flight time where the cabin pressure altitude is above 13000 ft.
10 minutes or the entire flight time where the cabin pressure altitude is above 15000 ft, whichever is the greater
the entire flight time where the cabin pressure altitude is above 10000 ft minus 30 minutes.
33.
In the cockpit of a transport airplane, at least one manual fire-extinguisher must be conveniently located containing
halon.
powder.
water.
special fluids
34.
On a multi-engined aircraft a fire detection system includes
a single warning light but a separate alarm bell for each engine
a warning light for each engine and a single alarm bell common to all engines
both a warning light and an alarm bell unique to each engine
a single warning light and a single alarm bell
35.
Smoke detector systems are installed in the
upper cargo compartments (class E).
wheel wells.
fuel tanks.
engine nacelles
36.
An airplane whose maximum approved passenger seating configuration is 201 to 300 seats must be equipped with at least
4 hand fire-extinguishers conveniently located in the passenger compartment.
3 hand fire-extinguishers conveniently located in the passenger compartment
6 hand fire-extinguishers conveniently located in the passenger compartment
5 hand fire-extinguishers conveniently located in the passenger compartment
37.
A public transport jet aeroplane may be operated up to FL 450. The cabin includes 180 passenger seats, made up of 30 rows (3 seats from each side of central aisle). The minimum number of cabin oxygen masks for this aeroplane must be
210 (one additional mask per seat row).
198 (110% of the seating capacity).
240 (one additional mask per seat block).
270 (150% of the seating capacity).
38.
In a fire detection system with single-loop continuous components (with no fault protection), if the line is accidently grounded
there will be no effect on the system
the power supply is cut off automatically.
the fire alarm is triggered
the engine fire extinguisher striker is automatically activated
39.
An airplane whose maximum approved passenger seating configuration is 31 to 60 seats must be equipped with at least
2 hand fire-extinguishers conveniently located in the passenger compartment.
5 hand fire-extinguishers conveniently located in the passenger compartment
3 hand fire-extinguishers conveniently located in the passenger compartment.
4 hand fire-extinguishers conveniently located in the passenger compartment
40.
An exit is considered to be out of service when the following elements are inoperative the:1. external door opening mechanism2. internal door opening mechanism3. door opening aid device4. open door locking system5. auxiliary means of evacuation6. emergency lightingThe combination regrouping all the correct statements is
1, 2, 5, 6
1, 2, 3, 4, 5, 6
1, 3, 4, 5
2, 3, 4, 6
41.
An aircraft is scheduled to fly from PARIS to MARSEILLE at FL 390 and has the following characteristics:Maximum permissible number of passenger specified by the certificate of airworthiness= 230Number of seats on board= 200Scheduled number of passengers on board= 180The minimum number of inhaler systems provided in the aircraft cabin should be
220
200.
180.
230.
42.
The number of emergency exits in transport aeroplanes
must be in accordance with the number of passengers on board
depends on the decision of the manufacturer in agreement with the operator
must be arranged to allow at least 50 % of all passengers to leave the aeroplane within 2 minutes
must be arranged to allow all passengers and all crew members to leave the aeroplane within 90 sec. through 50 % of the available emergency exits
43.
An airplane whose maximum approved passenger seating configuration is 61 to 200 seats must be equipped with at least
2 hand fire-extinguishers conveniently located in the passenger compartment
4 hand fire-extinguishers conveniently located in the passenger compartment
3 hand fire-extinguishers conveniently located in the passenger compartment
5 hand fire-extinguishers conveniently located in the passenger compartment
44.
In a pressurized aircraft, the first-aid (therapeutic) oxygen is designed to
protect the flight crew and cabin attendants against fumes and noxious gases
protect all the occupants against the effects of accidental depressurisation
protect certain passengers, and is only carried on board for these people
give medical assistance to passengers with pathological respiratory disorders
45.
The oxygen masks have dropped down from the passengers service units. The oxygen flow starts
After the system has been switched on by a crew member
after pulling the oxygen mask downwards
immediately
only above FL200
46.
The main feature of BCF fire extinguishers is that they
use the cooling effect created by the venturi during discharge.
are highly corrosive particularly for aluminium alloys
act as flame inhibitors by absorbing the air's oxygen.
are electrical conductors.
47.
In a pressurized aircraft, the first-aid (therapeutic) oxygen is designed to
protect all the occupants against the effects of accidental depressurisation
protect the flight crew and cabin attendants against fumes and noxious gases
give medical assistance to passengers with pathological respiratory disorders
protect certain passengers, and is only carried on board for these people
48.
A fault protection circuit in a fire detection system will
activate an alarm in the cockpit and in the landing gear bay for ground crew
inhibit the fire detector when the detection line is connected to ground
automatically initiate APU shutdown and fire extinguisher striker activation in the event of fire
activate the fire detection system when the detection line is connected to ground
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