Air Systems Flashcards

1
Q

What sources supply air to the bleed air system?

A

-Engines
-APU
-ground external pneumatic air cart/source

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2
Q

What causes the engine bleed valve to automatically close? Which lights indicate this has occurred?

A

-Excessively high bleed air temp (254*C) or pressure (220 psi)
-BLEED TRIP OFF, AIR COND annunciator, and MASTER CAUTION

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3
Q

Which conditions will the TRIP RESET switch reset?

A

When pressed, will reset the bleed trip condition (BLEED TRIP OFF [amber]) if the exceedance no longer exists. With the engine bleed air switch ON, the valve will auto open with successful reset.

-TRIP RESET switch also used to reset ZONE TEMP and PACK lights

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4
Q

What will cause the automatic closure of the APU bleed valve?

A

-The valve closes automatically when the APU is shut down, regardless of switch position.

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5
Q

Normally, what is the position of the isolation valve with the isolation switch in AUTO?

A

-In AUTO, the isolation valve is closed when
—both engine bleed air switches are ON, and
—both pack switches are ON (auto/high)
-placing one switch to off (any bleed/pack) will auto open the ISOL valve.
-ISOL valve position not affected by APU BLEED air switch.

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6
Q

What does the DUAL BLEED (amber) light indicate?

A

-illuminates when the APU bleed air valve is open, and
—Engine 1 bleed switch is on and/or
—Engine 2 bleed switch is on with isolation valve open

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7
Q

What is the primary source of conditioned air in the flight deck?

A

-A portion of the conditioned air from the left pack flows directly to the flight deck.
-Excess air from the left pack, the right pack, and the air recirculating system is combined in the mix manifold, then distributed through the left/right sidewall risers in the pax cabin.
—if left pack not operating, mix manifold will provide air to flight deck.

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8
Q

A single pack on high flow mode can maintain pressurization up to what altitude?

A

-A single pack can maintain pressurization/acceptable temp up to max certified ceiling

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9
Q

What conditions would cause a pack to change to high air flow with both PACK switches in AUTO?

A

-When plane is airborne, flaps up, pack switches AUTO, ENG bleeds on, if one pack/engine fails or PACK switch selected off, the remaining pack switches to high air flow

—auto pack switching inhibited on ground or in flight with flaps extended (for single engine perf)

-auto switching to “high flow” occurs if both engine bleed switches OFF and APU bleed switch ON, regardless of flap position, air/ground status, or number of packs operating.

-High airflow mode=pack switch in “high”

-“APU high air flow” avail:
—aircraft on ground
—ENG Bleed switches OFF
—APU operating
—APU Bleed air Switch on, and
—either/both PACK switches to High

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10
Q

What is indicated by the PACK (amber) light on the bleed air panel?

A

-Indicates failure of both primary and standby pack controls for the same pack. The pack will continue to operate without control unless excessive temps cause the pack to trip off.

-or, indicates overheat condition. Pack valve closes. Terminates operation of associated pack

-during master caution recall, indicates a primary or standby pack control failure exists. Extinguishes with Master caution system reset.

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11
Q

What will cause the Isolation valve to open automatically with the Isolation Valve switch in auto?

A

-In AUTO, the Isolation Valve will be CLOSED when: (corner switches)
—both Engine BLEED Air switches on, and
—both Pack switches in AUTO or HIGH

*placing any one of these switches to OFF will automatically open the Isolation Valve

  • not affected by the APU BLEED switch
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12
Q

What provides cooling air for the heat exchangers in the PACK system?

A

The ram air system.

-Automatically controlled by the packs
-full open
—on ground
—slow flight with flaps extended

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13
Q

What is indicated by the bright blue RAM DOOR FULL OPEN light?

A

-RAM DOOR FULL OPEN (blue light) illuminates when fully open
-doors modulate between open/closed in normal cruise
-deflector doors prevent FOD prior to liftoff/after touchdown. Connected mechanically to ram air inlet door

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14
Q

What is the purpose of the recirculation fans?

A

-Increase airflow to passenger cabin through main distribution system
-2 fans (left, right) either side of mix manifold
-pull air from electronics bay and and cabin floor grilles towards lining of forward cargo compartment, then into the mix manifold
-only recirc air passes through HEPA filters

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15
Q

What does the illumination of the ZONE TEMP (amber) lights indicate?

A

ANY ZONE TEMP
-supply duct overheat and associated Trim Air Modulating Valve closes
—may be reopened with TRIP RESET switch after duct cooled

CONT CAB ZONE TEMP (Amber)
-failure of both primary and standby temp controls
-during master caution recall, CONT CAB indicates failure of primary or standby flight deck temp control. Auto switch to backup control

FWD or AFT CAB ZONE TEMP (Amber)
-during master caution recall, FWD or AFT indicates failure of forward or aft temp control, and associated trim valve closes
—Temp Selectors operate normally but average the two passenger cabin zones

Left electronic controller
-controls aft cabin zone
-provides backup control to flight deck

Right electronic controller
-controls forward cabin zone
-provides primary control to flight deck

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16
Q

What limitations, if any, are there when using external conditioned air?

A

-Pack Switches should be OFF
—packs ON reduce efficiency of external air
—flight deck temp controls don’t change external air temp

17
Q

What is the propose of the Equipment Cooling System?

A

-cools electronics in flight deck and E/E bay
-2 ducts, supply and exhaust
—each duct has normal and alternating fan

-exhaust collects warm air from all electronics
—overboard exhaust valve normally open on ground, closed in flight (pressurized)
—when closed, warm air diffused in lining of forward cargo compartment for added heating

18
Q

Which, if any, of the cargo compartments are heated by the Equipment Cooling System exhaust fans?

A

-forward cargo compartment for added in flight heating

19
Q

What does the Equip Cooling OFF (amber) light indicate?

A

-indicates loss of airflow due to the failure of the respective Equipment Cooling Fan

-selecting the alternate fam should restore airflow and extinguish light within 5 seconds

-if over temp on ground, crew call horn in nose wheel well sounds

20
Q

How is the Alternate Cabin Pressurization selected?

A

-when manually selected. ALTN (green) light

-or, when auto fail has occurred (AUTO FAIL amber light also illuminated)

21
Q

What are the indications that the active Cabin Pressurization Controller has failed?

A

AUTO FAIL (Amber) light with ALTN (green) light

-AUTO FAIL (amber) light
—loss of DC power
—controller fault
—Outflow Valve control fault
—excessive diff press >8.75psi
—excessive cabin press change >2000 ft/min
—high cabin alt >15,800 ft

*AUTO FAIL light without ALTN light
—dual controller failure
—FLT ALT and LAND ALT windows show 5 dashes

22
Q

What causes the illumination of the OFF SCHED DESCENT (amber) light?

A

-if the aircraft begins to descend without reaching preset cruise altitude.

-controller automatically programs cabin to departure field elevation.
*if the FLT ALT indicator changed, auto abort capability to takeoff field elevation is lost

23
Q

At approximately what altitude will the CABIN ALTITUDE (red) light and the Cabin Altitude Horn activate? Can the horn be silenced?

A

-10,000 ft +/- 1000 ft
-sensed by either of the 2 cabin altitude pressure switches in E/E compartment

-can be silenced with ALT HORN CUTOUT switch on Cabin Altitude Panel

-same aural tone as Takeoff Config Warnings