11.3 E Nacelles And Pylons Flashcards

(30 cards)

1
Q

What is the housing unit that typically encloses an aircraft engine called?
A. Turret
B. Nacelle
C. Podium

A

B. Nacelle

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2
Q

What isolates the aircraft engine from the wing or fuselage to enhance safety?
A. Insulation foam
B. Firewalls or fire shields
C. Cooling fans

A

B. Firewalls or fire shields

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3
Q

What is the main structural component of a pylon called that contains the engine attachment fittings?
A. Firewall
B. Torque box
C. Fairing

A

B. Torque box

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4
Q

What types of loads do the forward pylon attachment fittings primarily transmit?
A. Longitudinal and aerodynamic
B. Weight and lateral
C. Electrical and hydraulic

A

B. Weight and lateral

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5
Q

What is the primary purpose of a nacelle on an aircraft?
A. To carry passengers
B. To house the engine and accessories
C. To store fuel

A

B. To house the engine and accessories

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6
Q

What are the large panels called that surround and streamline the engine?
A. Skids
B. Cowls
C. Pods

A

B. Cowls

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7
Q

What type of metal is typically used on nacelle surfaces near exhaust exits due to high temperatures?
A. Copper
B. Stainless steel or titanium alloys
C. Lead

A

B. Stainless steel or titanium alloys

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8
Q

What is another common name for a nacelle?
A. Canopy
B. Pod
C. Shell

A

B. Pod

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9
Q

What feature is often added to modern nacelles to help reduce engine noise?
A. Air vents
B. Acoustic lining and serrated edges
C. Extra insulation foam

A

B. Acoustic lining and serrated edges

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10
Q

What does the fan cowl support beam do?
A. Stores fuel for the engine
B. Supports the fan cowl and distributes loads to the torque box
C. Controls airflow into the engine

A

B. Supports the fan cowl and distributes loads to the torque box

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11
Q

How is the fan cowl attached to the fan cowl support beam?
A. Welded
B. Bolted
C. Hinged with quick-release pins

A

C. Hinged with quick-release pins

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12
Q

What is the purpose of the wing-to-nacelle fairings?
A. To reduce engine noise
B. To provide a low-drag aerodynamic profile between the engine nacelle and the wing
C. To support the engine

A

B. To provide a low-drag aerodynamic profile between the engine nacelle and the wing

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13
Q

How long must firewall materials resist flame penetration according to regulations?
A. 5 minutes
B. 10 minutes
C. 15 minutes

A

C. 15 minutes

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14
Q

What is the purpose of a flameproof bulkhead (firewall) in an aircraft?
A. To support the engine
B. To separate the engine compartment from the rest of the aircraft and prevent flame penetration
C. To reduce fuel consumption

A

B. To separate the engine compartment from the rest of the aircraft and prevent flame penetration

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15
Q

What must the firewall prevent from passing through to other parts of the aircraft?
A. Oxygen and any fuel from leaking from the tank

What must the firewall prevent from passing through to other parts of the aircraft?
A. Oxygen
B. Hazardous quantity of liquid, gas, or flame
C. Carbon dioxide

C. Carbon dioxide from getting to the fire and making it worst

A

B. Hazardous quantity of liquid, gas, or flame

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16
Q

What must all aircraft firewalls and shrouds be?
A. Waterproof
B. Fireproof
C. Shockproof

17
Q

What must firewalls prevent from passing to other parts of the aircraft?
A. Air
B. Electrical signals
C. Hazardous liquid, gas, or flame

A

C. Hazardous liquid, gas, or flame

18
Q

How must openings in firewalls be sealed?
A. With glue
B. With close-fitting, fireproof grommets or fittings
C. With foam seals

A

B. With close-fitting, fireproof grommets or fittings

19
Q

What protection must firewalls have in addition to fire resistance?
A. Paint coating
B. Anti-vibration
C. Corrosion protection

A

C. Corrosion protection

20
Q

What are firewalls made from to resist high engine temperatures?
A. Aluminium and plastic
B. Stainless steel, Inconel, or titanium
C. Wood and copper

A

B. Stainless steel, Inconel, or titanium

21
Q

What do flameproof panels and diaphragms help prevent?
A. Engine noise
B. Vibration
C. Spread of flames through the engine

A

C. Spread of flames through the engine

22
Q

What should be inspected when checking a firewall?
A. Only the top edge
B. Paint color
C. Condition, security, cracking, grommets, and sealant

A

C. Condition, security, cracking, grommets, and sealant

23
Q

What must be done if a fire shield or heat blanket is worn or damaged?
A. Leave it until next inspection
B. Patch it with tape
C. Replace it

A

C. Replace it

24
Q

What is the main purpose of an engine mount?
A. Store fuel
B. Connect the engine to the aircraft and manage vibrations
C. Increase engine speed

A

B. Connect the engine to the aircraft and manage vibrations

25
What is the main purpose of shock mounts (flexible engine suspension units)? A. Increase engine power B. Prevent overheating C. Absorb engine vibrations
C. Absorb engine vibrations
26
What additional stress affects the entire engine mount bolts when the aircraft is airborne? A. Compressive stress B. Torsional stress C. Thermal stress
B. Torsional stress
27
How is the engine typically attached to the mount in aircraft using dynafocal mounts? A. By bolts placed at the rear of the engine B. Using dynafocal mounts at the engine’s centre of gravity, forward of the mounting ring C. With rigid brackets directly to the fuselage
B. Using dynafocal mounts at the engine’s centre of gravity, forward of the mounting ring
28
What is the purpose of the mounting pad angle in dynafocal engine mounts? A. To align the mount with the aircraft fuselage B. To reduce engine vibrations during flight C. To point to the Centre of Gravity (CG) of the engine’s mass
C. To point to the Centre of Gravity (CG) of the engine’s mass
29
How do engine mounts for turbofan engines function? A. They only support the rear end of the engine B. They transmit loads from the engine to the aircraft structure C. They are only used to isolate engine vibrations
B. They transmit loads from the engine to the aircraft structure
30
What is the primary function of the forward turbine vibration isolator engine mounts? A. To support only vertical loads B. To support vertical, side, and axial (thrust) loads while allowing thermal expansion C. To only accommodate thermal expansion without supporting any loads
B. To support vertical, side, and axial (thrust) loads while allowing thermal expansion