Aldis Paragraph

Multiple Choice

You lift the start lever 51) ........................... an engine start sequence. You lower the start lever to shut down the engine. The start lever sends signals to interfacing systems. There are two start levers, one for 52) ........................... engine. The start lever has two 53) ..........................., IDLE and CUTOFF. A detent locks the lever in each position. You must pull the lever out to move it from one detent to the other. The lever connects mechanically to a brake

54) ........................... gives a friction force. Each start lever operates 6 switches. Two of the switches send signals to the EEC (Electronic Engine Control).Two of the switches interface 55) ........................... the engine ignition system. The other two switches send signals to valves in the engine fuel feed

system.

• during

• when

• that

• as

Multiple Choice

You lift the start lever 51) ........................... an engine start sequence. You lower the start lever to shut down the engine. The start lever sends signals to interfacing systems. There are two start levers, one for 52) ........................... engine. The start lever has two 53) ..........................., IDLE and CUTOFF. A detent locks the lever in each position. You must pull the lever out to move it from one detent to the other. The lever connects mechanically to a brake 54) ........................... gives a friction force. Each start lever operates 6 switches. Two of the switches send signals to the EEC (Electronic Engine Control). Two of the switches interface 55) ........................... the engine ignition system. The other two switches send signals to valves in the engine fuel feed

system.

• one

• both

• two

• each

Multiple Choice

You lift the start lever 51) ........................... an engine start sequence. You lower the start lever to shut down the engine. The start lever sends signals to interfacing systems. There are two start levers, one for 52) ........................... engine. The start lever has two 53) ..........................., IDLE and CUTOFF. A detent locks the lever in each position. You must pull the lever out to move it from one detent to the other. The lever connects mechanically to a brake 54) ........................... gives a friction force. Each start lever operates 6 switches. Two of the switches send signals to the EEC (Electronic Engine Control). Two of the switches interface 55) ........................... the engine ignition system. The other two switches send signals to valves in the engine fuel feed

system.

• positions

• postures

• locations

• landings

Multiple Choice

You lift the start lever 51) ........................... an engine start sequence. You lower the start lever to shut down the engine. The start lever sends signals to interfacing systems. There are two start levers, one for 52) ........................... engine. The start lever has two 53) ..........................., IDLE and CUTOFF. A detent locks the lever in each position. You must pull the lever out to move it from one detent to the other. The lever connects mechanically to a brake 54) ........................... gives a friction force. Each start lever operates 6 switches. Two of the switches send signals to the EEC (Electronic Engine Control). Two of the switches interface 55) ........................... the engine ignition system. The other two switches send signals to valves in the engine fuel feed system.

• what

• where

• which

• whose

Multiple Choice

You lift the start lever 51) ........................... an engine start sequence. You lower the start lever to shut down the engine. The start lever sends signals to interfacing systems. There are two start levers, one for 52) ........................... engine. The start lever has two 53) ..........................., IDLE and CUTOFF. A detent locks the lever in each position. You must pull the lever out to move it from one detent to the other. The lever connects mechanically to a brake 54) ........................... gives a friction force. Each start lever operates 6 switches. Two of the switches send signals to the EEC (Electronic Engine Control). Two of the switches interface 55) ........................... the engine ignition system. The other two switches send signals to valves in the engine fuel feed system.

• with

• and

• as

• so

Multiple Choice

Position the new lockout ................... on the translating

sleeve.

• assemble

• assembly

• assemblies

• assembling

Multiple Choice

Protect the floor and sidewall panels with the ...........................

material.

• protected

• protector

• protecting

• protective

Multiple Choice

After the ............................ of new wires or harnesses do a continuity

test.

• installers

• installments

• installing

• installation

Multiple Choice

The .............................. is made with an external power unit connected.

• refueling

• refueled

• refuels

• refilled

Multiple Choice

An integrated drive generator (IDG) 61) ........................... on the aft face of the accessory gearbox at the 7 o’clock position. The IDG 62) ........................... of a constant speed drive and a generator mounted side by side in a 63) ........................... housing. Other parts integral or mounted to the IDG are the scavenge filter, thermal relief valve, and pressure relief valve. The IDG 64) ...........................the varying input speed of the engine into 115/200- volt, 3- Form No: AAA-DT-F 004, Rev. No: 00 Sayfa 16 / 21 phase, 90 KVA, 400 ±5 Hz power. The IDG weighs 65)........................... 120 pounds (54 kilograms).

• is mounted

• was mounting

• are mounted

• were mounted

Multiple Choice

An integrated drive generator (IDG) 61) ........................... on the aft face of the accessory gearbox at the 7 o’clock position. The IDG 62) ........................... of a constant speed drive and a generator mounted side by side in a 63) ........................... housing. Other parts integral or mounted to the IDG are the scavenge filter, thermal relief valve, and pressure relief valve. The IDG 64) ...........................the varying input speed of the engine into 115/200- volt, 3- Form No: AAA-DT-F 004, Rev. No: 00 Sayfa 16 / 21 phase, 90 KVA, 400 ±5 Hz power. The IDG weighs 65)........................... 120 pounds (54 kilograms).

• consistory

• consistent

• consisting

• consists

Multiple Choice

An integrated drive generator (IDG) 61) ........................... on the aft face of the accessory gearbox at the 7 o’clock position. The IDG 62) ........................... of a constant speed drive and a generator mounted side by side in a 63) ........................... housing. Other parts integral or mounted to the IDG are the scavenge filter, thermal relief valve, and pressure relief valve. The IDG 64) ...........................the varying input speed of the engine into 115/200- volt, 3- Form No: AAA-DT-F 004, Rev. No: 00 Sayfa 16 / 21 phase, 90 KVA, 400 ±5 Hz power. The IDG weighs 65)........................... 120 pounds (54 kilograms).

• commotion

• common

• commoner

• commute

Multiple Choice

An integrated drive generator (IDG) 61) ........................... on the aft face of the accessory gearbox at the 7 o’clock position. The IDG 62) ........................... of a constant speed drive and a generator mounted side by side in a 63) ........................... housing. Other parts integral or mounted to the IDG are the scavenge filter, thermal relief valve, and pressure relief valve. The IDG 64) ...........................the varying input speed of the engine into 115/200- volt, 3- Form No: AAA-DT-F 004, Rev. No: 00 Sayfa 16 / 21 phase, 90 KVA, 400 ±5 Hz power. The IDG weighs 65)........................... 120 pounds (54 kilograms).

• convents

• conveys

• convenes

• converts

Multiple Choice

An integrated drive generator (IDG) 61) ........................... on the aft face of the accessory gearbox at the 7 o’clock position. The IDG 62) ........................... of a constant speed drive and a generator mounted side by side in a 63) ........................... housing. Other parts integral or mounted to the IDG are the scavenge filter, thermal relief valve, and pressure relief valve. The IDG 64) ...........................the varying input speed of the engine into 115/200- volt, 3- Form No: AAA-DT-F 004, Rev. No: 00 Sayfa 16 / 21 phase, 90 KVA, 400 ±5 Hz power. The IDG weighs 65)........................... 120 pounds (54 kilograms).

• appropriately

• approximate

• approximately

• approvingly

Multiple Choice

The dust can cause................................. on all filter elements.

• contamined

• contamination

• contaminant

• contaminate

Multiple Choice

The pilot must report the.................................. encounter of this event.

• suspected

• suspect

• suspecting

• susceptible

Multiple Choice

The brake temperature.............................monitors the brake temperature.

• sensor

• sensory

• sense

• sensers

Multiple Choice

After 1 hour, use fog or foam on the wheel or tire to decrease the......................................

• temperature

• temperate

• temperament

• tempt

Multiple Choice

Look for bubbles at ................................. of those areas are to examine for leaks.

• once

• single

• each

• double

Multiple Choice

The number of passengers must be................................to 165 passengers.  

• limiting

•  limited

•  limitation

•  limitless

Multiple Choice

No electrical power will be .............................from the auxiliary power unit generator.

• availability

• allowable

• available

• allow

Multiple Choice

After you ............................the wiring, repair the wiring.

• exam

• examine

• exact

• extra

Multiple Choice

Put the seat unit................................position on the seat tracks. 

• in

• of

• as

• by

Multiple Choice

Count and.............................utilized tools. 

• verification

• verified

•  verify

• vivificated

Multiple Choice

The single aisle aircraft communication system has two sub-systems: radio communication, and on board communication. The radio communication systems are used for communications to and from  the aircraft. The on-board internal communication system is “divided” into 4 functions: service  interphone (on ground only) for maintenance technician communication with cockpit or cabin  thanks to several jack connectors around the aircraft. Flight interphone for cockpit internal  communication and also with the ground mechanic, Passenger Address (PA) from the cockpit or  from cabin crew stations for passenger announcements, cabin interphone for cabin crew or cabin  crew/pilots communication. 

The passage is mainly about ……………………………………………….

•  the details of the radio communication system

• the specific aircraft communication system

• the details of passenger address system

• the specific ground communication system

Multiple Choice

The single aisle aircraft communication system has two sub-systems: radio communication, and on board communication. The radio communication systems are used for communications to and from  the aircraft. The on-board internal communication system is “divided” into 4 functions: service  interphone (on ground only) for maintenance technician communication with cockpit or cabin  thanks to several jack connectors around the aircraft. Flight interphone for cockpit internal  communication and also with the ground mechanic, Passenger Address (PA) from the cockpit or  from cabin crew stations for passenger announcements, cabin interphone for cabin crew or cabin  crew/pilots communication. 

Radia communication system is used for..................

• to communicate with the cabin crew

•  to communicate with the ground mechanic 

•  to communicate between the aircrafts

•  to communicate with the passengers 

Multiple Choice

The single aisle aircraft communication system has two sub-systems: radio communication, and on board communication. The radio communication systems are used for communications to and from  the aircraft. The on-board internal communication system is “divided” into 4 functions: service  interphone (on ground only) for maintenance technician communication with cockpit or cabin  thanks to several jack connectors around the aircraft. Flight interphone for cockpit internal  communication and also with the ground mechanic, Passenger Address (PA) from the cockpit or  from cabin crew stations for passenger announcements, cabin interphone for cabin crew or cabin  crew/pilots communication. 

According to the passage it cannot be said that ………………………………………

• Passenger Address can be used for ground mechanic communication

•  radio communication is used to communicate outside of the aircraft

•  service interphone cannot be used on air to communicate with maintenance  technician

• there are multiple connection points for the maintenance technician 

Multiple Choice

The single aisle aircraft communication system has two sub-systems: radio communication, and on board communication. The radio communication systems are used for communications to and from  the aircraft. The on-board internal communication system is “divided” into 4 functions: service  interphone (on ground only) for maintenance technician communication with cockpit or cabin  thanks to several jack connectors around the aircraft. Flight interphone for cockpit internal  communication and also with the ground mechanic, Passenger Address (PA) from the cockpit or  from cabin crew stations for passenger announcements, cabin interphone for cabin crew or cabin  crew/pilots communication. 

69. “Divided” can be replaced with………………………………………. 

• combine

• contrive

• semantics

• separated

Multiple Choice

The single aisle aircraft communication system has two sub-systems: radio communication, and on board communication. The radio communication systems are used for communications to and from  the aircraft. The on-board internal communication system is “divided” into 4 functions: service  interphone (on ground only) for maintenance technician communication with cockpit or cabin  thanks to several jack connectors around the aircraft. Flight interphone for cockpit internal  communication and also with the ground mechanic, Passenger Address (PA) from the cockpit or  from cabin crew stations for passenger announcements, cabin interphone for cabin crew or cabin  crew/pilots communication. 

Communication with the maintenance technician is achieved using 

……………………………………………

•  radio communication

• Passenger Address

• cockpit radio

• service interphone 

Multiple Choice

The heart of the audio system is the Audio Management Unit (AMU). The AMU routes the signals  generated by the crew and directs the signals to and from the appropriate radio or interphone  system. The AMU has a decoding unit called Selective Calling (SELCAL). “It” lets aural and visual  indications on the audio control panel with an amber CALL indication to alert the flight crew for calls  from ground stations. When the Passenger Address function is used from cockpit, the audio signal is  routed via the AMU to the cabin intercommunication data system director and from the director to  

the Decoder Encoder Units (DEUs) for distribution in the cabin.

71. The passage is mainly about ………………………………………………………

• the passenger address system 

• selective calling unit

• audio management unit

• interphone system

Multiple Choice

The heart of the audio system is the Audio Management Unit (AMU). The AMU routes the signals  generated by the crew and directs the signals to and from the appropriate radio or interphone  system. The AMU has a decoding unit called Selective Calling (SELCAL). “It” lets aural and visual  indications on the audio control panel with an amber CALL indication to alert the flight crew for calls  from ground stations. When the Passenger Address function is used from cockpit, the audio signal is  routed via the AMU to the cabin intercommunication data system director and from the director to  

the Decoder Encoder Units (DEUs) for distribution in the cabin

...................is stated in the passage

• The purpose of the AMU

• The power requirements of the AMU

•  The location of the AMU

• The backup of the AMU

Multiple Choice

The heart of the audio system is the Audio Management Unit (AMU). The AMU routes the signals  generated by the crew and directs the signals to and from the appropriate radio or interphone  system. The AMU has a decoding unit called Selective Calling (SELCAL). “It” lets aural and visual  indications on the audio control panel with an amber CALL indication to alert the flight crew for calls  from ground stations. When the Passenger Address function is used from cockpit, the audio signal is  routed via the AMU to the cabin intercommunication data system director and from the director to  

the Decoder Encoder Units (DEUs) for distribution in the cabin.

“It” refers to ……………………………………..

• the AMU

• the SELCAL

• the radio

• the interphone

Multiple Choice

The heart of the audio system is the Audio Management Unit (AMU). The AMU routes the signals  generated by the crew and directs the signals to and from the appropriate radio or interphone  system. The AMU has a decoding unit called Selective Calling (SELCAL). “It” lets aural and visual  indications on the audio control panel with an amber CALL indication to alert the flight crew for calls  from ground stations. When the Passenger Address function is used from cockpit, the audio signal is  routed via the AMU to the cabin intercommunication data system director and from the director to  

the Decoder Encoder Units (DEUs) for distribution in the cabin.

Selective Calling unit is used …………………………………………

• to route the signals

• to address the passengers from the cockpit

• to decode signals and display indicators for crew

Multiple Choice

The heart of the audio system is the Audio Management Unit (AMU). The AMU routes the signals  generated by the crew and directs the signals to and from the appropriate radio or interphone  system. The AMU has a decoding unit called Selective Calling (SELCAL). “It” lets aural and visual  indications on the audio control panel with an amber CALL indication to alert the flight crew for calls  from ground stations. When the Passenger Address function is used from cockpit, the audio signal is  routed via the AMU to the cabin intercommunication data system director and from the director to  

the Decoder Encoder Units (DEUs) for distribution in the cabin.

According to the passage, which one is not true? 

• SELCAL has both audio and visual warnings

•  The route the signal takes from cockpit to cabin is stated in the passage

• The AMU distributes the signals to the correct radio or system

• SELCAL has different color coded indications 

Multiple Choice

The pitot probe measures pitot air pressure. The pitot probe port points forward to measure pitot  pressure. The probe is located several inches from the airplane skin to “decrease” airflow turbulence  effects. A base plate contains the electrical and pressure connectors. A gasket is between the probe  base and the airplane structure to form a pressure seal. An anti-icing heater is in the probe to  prevent ice. The heater is attached to the electrical connector in the base plate.

The passage is about ………………………………………………..

• the ice prevention

• turbulence

• pressure seal

• the function of pitot probe

Multiple Choice

The pitot probe measures pitot air pressure. The pitot probe port points forward to measure pitot  pressure. The probe is located several inches from the airplane skin to “decrease” airflow turbulence  effects. A base plate contains the electrical and pressure connectors. A gasket is between the probe  base and the airplane structure to form a pressure seal. An anti-icing heater is in the probe to  prevent ice. The heater is attached to the electrical connector in the base plate.

...........is not stated in the in the passage.

•  The purpose of the pitot probe

• The purpose of the anti-icing heater

•  The purpose of the gasket

• The purpose of the pressure seal

Multiple Choice

The pitot probe measures pitot air pressure. The pitot probe port points forward to measure pitot  pressure. The probe is located several inches from the airplane skin to “decrease” airflow turbulence  effects. A base plate contains the electrical and pressure connectors. A gasket is between the probe  base and the airplane structure to form a pressure seal. An anti-icing heater is in the probe to  prevent ice. The heater is attached to the electrical connector in the base plate.

The synonym of “decrease” is …………………………………………….

• increase

• rise

• lower

• give

Multiple Choice

The pitot probe measures pitot air pressure. The pitot probe port points forward to measure pitot  pressure. The probe is located several inches from the airplane skin to “decrease” airflow turbulence  effects. A base plate contains the electrical and pressure connectors. A gasket is between the probe  base and the airplane structure to form a pressure seal. An anti-icing heater is in the probe to  prevent ice. The heater is attached to the electrical connector in the base plate.

. It can be inferred from the passage ……….……………………………………. 

• the components of the pitot probe

•  the measurements of the probe

•  the limits of the anti-ice heater

• the maximum movement range of the pitot

Multiple Choice

The pitot probe measures pitot air pressure. The pitot probe port points forward to measure pitot  pressure. The probe is located several inches from the airplane skin to “decrease” airflow turbulence  effects. A base plate contains the electrical and pressure connectors. A gasket is between the probe  base and the airplane structure to form a pressure seal. An anti-icing heater is in the probe to  prevent ice. The heater is attached to the electrical connector in the base .

What cannot be said about the pitot probe?

•  It is flush with the aircraft skin.

• It measures air pressure.

•  It is located beneath the aircraft.

• It has a built-in heater unit against ice.