Reading...
Play button
Play button
Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
18 Cards in this Set
- Front
- Back
|
Which T-6A environmental system is an engine-driven vapor cycle system?
|
air conditioning
|
|
|
The control which determines how much hot engine bleed air is provided to the environmental system.
|
Bleed air inflow switch
|
|
|
the control which determines the amount of warm bleed air to be mixed with cooled air supplied by the heat exchanger for ducting to the cockpit.
|
temperature control switch knob
|
|
|
In order for the air conditioner compressor to be engaged, both the AIR COND and DEFOG switches must be in the ON position. T/F?
|
TRUE
|
|
|
The ____ controls provide power to the front and rear cockpit blowers which supply airflow through the air conditioning vents.
|
evaporator blower
|
|
|
On the ground, the fresh air blower is activated by the ______
|
weight-on-wheels switch on the landing gear
|
|
|
Fresh air is distributed to the main cockpit duct and then output through the _____.
|
footwarmers or defog vents
|
|
|
While in flight, cool air from the ____ passes through the heat exchanger, draws heat from the bleed air, and is then exhausted through a vent in the lower right cowling.
|
ram air inlet
|
|
|
As the temperature control is turned toward COLD, the heat exchanger bypass valve opens up and more cool air from the heat exchanger passes into the cockpit.
|
FALSE
|
|
|
Which control, when activated, prevents engine compartment fumes from entering the cockpit through the environmental system after an engine shutdown situation?
|
Firewall shutoff handle.
|
|
|
Cockpit air temperature is automatically adjusted between _____ Fahrenheit with the TEMP CONTROL switch set to AUTO.
|
60 and 90*
|
|
|
When the DEFOG switch is ON and the vent control lever is set to CANOPY, a higher volume of bleed air in the system causes ambient cockpit air to be drawn into the heating system ejector, mixed with bleed air in the main cockpit duct and flow downstream to the windshield and canopy defog ducts. T/F?
|
TRUE
|
|
|
Placing the vent lever in the ___ position causes the valve at the front cockpit assembly to direct the warm air into the windshield defog duct
|
CANOPY
|
|
|
The control which opens the bi-level flow control bypass valve and provides a higher volume of bleed air flow to the heating system ejector.
|
Defog switch
|
|
|
The air conditioning system only operates when the engine is on and functioning with the ___ and the ____
|
generator on-line; AIR COND or DEFOG switch ON
|
|
|
The air conditioner component which converts vaporized refrigerant to a liquid.
|
Condenser
|
|
|
A panel in the ____ side of the fuselage allows access for maintenance personnel to recharge the system refrigerant when necessary.
|
forward right
|
|
|
The ___ will produce airflow at up to 350 cu ft per minute at the HI setting.
|
evaporator blowers.
|
