Rodina Final 2208
Quiz yourself by thinking what should be in
each of the black spaces below before clicking
on it to display the answer.
Help!
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| show | High Pressure Compressor
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| show | Bleed air
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| The cabin pressure of an aircraft in flight is maintained at the selected altitude by | show 🗑
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| show | all positive pressure from cabin
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| How is the cabin pressure of the pressurized aircraft usually controlled | show 🗑
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| show | main landing gear operating switch
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| the cabin pressure control setting has a direct influence upon the | show 🗑
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| show | negative pressure relief valve
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| if the cabin rate of climb is too great, the control should be adjusted to cause the | show 🗑
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| show | delivery air duct check valve
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| the primary function of the cabin pressurization system outflow valve is to | show 🗑
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| an aircraft pressurization cycle is normally considered to be | show 🗑
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| which statement best describes cabin differential pressure | show 🗑
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| the cabin pressurization modes of operation are | show 🗑
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| show | barometric pressure, cabin altitude, and cabin rate of change
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| the purpose of pressurizing aircraft cabin is to | show 🗑
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| show | SOV
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| show | unpressurized
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| show | isobaric
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| if the aircraft takes off from 1200 feet and climbs to and alt of 35k ft with a desired cabin altitude of 6500 ft, what operation is the psi system at 35k ft? | show 🗑
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| A/C takes of from a field elevation of 1k feet & climbs to 35kft with a desired cabin altitude of 6 ft. Outside atmospheric psi at 1kft is at 14.2psi at 6k ft is 11.8psi & at 35k is 3.46. what would be the required differential prssure at cruise altitude | show 🗑
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| if the aircraft takes off from a field elevation of 1k ft with a desired cabin altitude of 6k ft. has a max cabin differential of 5.4 psi what is the max cruising altitude of the aircraft | show 🗑
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| show | 7.44
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| Usually bleed air from a gas-turbine engine compressor can be safely used for cabin pressurization. Independent cabin condition air machine can be powered by bleed air from an aircraft turbine compressor | show 🗑
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| show | WOW (weight on wheels)
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| show | Cabin altitude instead of pressure
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| show | put aircraft in "air mode"
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| At what maximum altitude do we maintain the cabin of transport category aircraft? | show 🗑
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| show | dizziness, abnormal speech, and unconsciousness
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| What ATA chapter will you find pressurization? | show 🗑
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| Where would you find the regulating governing certification of transport category aircraft? | show 🗑
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| show | False
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| show | True
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| Turbine Bypass | show 🗑
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| show | Hottest air in the mixing chamber
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| 35 Degree sensor | show 🗑
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| show | extracts any condensation from the air
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| Expansion Turbine | show 🗑
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| show | First stage of cooling
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| show | cools air with RAM air before the turbine
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| ACM Compressor | show 🗑
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| Bleed Air valve | show 🗑
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| show | combines air inputs for proper temp into cabin
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| show | coldest air input into the mixing chamber
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| show | Air Cycle MAchine
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| show | Servicing the ACM
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| Zone temp controller | show 🗑
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| Coalescer Bag | show 🗑
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| show | Air conditioning/ pressurization
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| ATA Chapter 49 | show 🗑
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| ATA Chapter 36 | show 🗑
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| ATA Chapter 35 | show 🗑
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| show | 727 and L10-11
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| show | stabilize the pressure of the air before it enters the compressor
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| show | the airplane's main fuel supply
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| an APU is usually rotated during start by | show 🗑
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| when in operation, the speed of an APU occurs when | show 🗑
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| show | automatically by the APU fuel control system
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| usually, most of the load placed on an APU occurs when | show 🗑
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| show | is identical to the engine-driven generators
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| show | Provide bleed air for aircraft pneumatic systems
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| When necessary, APU engine cooling before shutdown may be accomplished by | show 🗑
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| show | pneumatic loading will be automatically modulated to maintain a safe EGT
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| show | 99.5%
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| uses a re-breather bag | show 🗑
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| show | 40-75 psi
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| demand type | show 🗑
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| show | high pressure cylinders
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| show | 1850 psi
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| stenciled on aircraft O2 bottle | show 🗑
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| show | 50 psi
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| show | Moisture
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| pressure test with water | show 🗑
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| show | Calibrated orifice
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| changes high psi cylinder psi to low system psi | show 🗑
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| the diluter is in a diluter demand system | show 🗑
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| show | green blowout plug on fuselage
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| DOT 3AA cylinder hydro test psi | show 🗑
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| show | Cylinder, Mask, and regulator
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| high pressure cylinder psi | show 🗑
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| portable O2 system used for | show 🗑
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| show | chemical O2 advantages
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| not used on commerical flights | show 🗑
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| show | pressure relief valve
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| show | continuous flow and pressure demand types
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| the purpose of the airflow metering aneroid assembly is O2 diluter demand regulator | show 🗑
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| what to do if the system has a leak | show 🗑
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| show | teflon
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| in the vapor cycle cooling system, what is the pressure and state of the refrigerant leaving the evaporator | show 🗑
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| show | low pressure, liquid
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| show | high pressure, liquid
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| in the vapor cycle cooling system, what is the pressure and state of the refrigerant leaving the compressor | show 🗑
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| which component in the vapor cycle system stores the refrigerant | show 🗑
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| show | evaporator
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| when servicing a vapor cooling system, evacuation is accomplished by using a vacuum. how is the water removed | show 🗑
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| show | False
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| show | the system needs to be charged
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| in which component of the vapor cooling system does the system give up heat and change the vapor into liquid | show 🗑
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| what is the ventilating air used for on a combustion heater | show 🗑
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| what is combustion air used for on a combustion heater | show 🗑
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| where does the exhaust from a combustion heater go | show 🗑
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| show | the aircraft fuel tank
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| the ignition system in a combustion heaters is continuous T/F? | show 🗑
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| show | False
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| show | the ignition will not be activated
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| show | the fuel is shut off to the heater
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| show | exhaust shroud heater
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| show | False
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Created by:
Bertttdavis