3_AIR CONDITIONING Flashcards

1
Q

How does the ac system provide temp controlled air

A

it processes bleed air from the engines, apu or ground air source in air cond packs

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2
Q

Describe the flow, in general of the system

A

conditioned air from the left pack, upstream of the mix manifold, goes to the flt deck

excess air from left pack, air from rt pack and air from recirc system is combined in the mix manifold

this then goes to the left and right sidewall risers and to the pax cabin

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3
Q

What controls the flow of bleed air to the pack?

A

the pack valve

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4
Q

Describe the normal bleed air sources for the packs

A

normally the left pack uses bleed air from Eng 1

right pack from eng 2

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5
Q

Can a single pack provide adequate pressure

A

Yes - a single pack in HIGH FLOW is capable to sustain both Press and Temp up to 41k

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6
Q

Can APU provide adequate bleed air?

A

yes - the APU can supply bleed air for

2 - packs on the ground

1 pack in flight

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7
Q

Are there any pack operating concerns when it comes to bleed air?

A

Do not operate MORE THAN ONE PACK from ONE ENGINE

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8
Q

if everything is operating normally, 2 engines, packs to auto and both eng bleed switches ON what is the pack flow rate

A

Normal flow

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9
Q

Describe Pack Auto logic

A
  • AIR - and flaps are UP (pack auto and eng bleed are ON)
    • if one pack fails - 1 engine fails - or 1 pack switch is turned OFF
      • the other automatically switches to HIGH FLOW
  • GROUND or FLAPS ARE DOWN (pack auto both eng bleed ON)
    • if one pack fails - 1 engine fails - or 1 pack switch is turned OFF
      • the remaining pack will NOT automatically switch to HIGH FLOW
    • auto switch is inhibited to ensure adequate eng power or sgl eng operation

APU PACK LOGIC.

  • if APU bleed ON (both eng bleeds OFF) w/ both packs in AUTO
    • auto switch to high flow occurs with a single pack failure
      • regardless of flaps or air/ground status
    • NOTE - in this configuration the flt crew can FORCE and APU HIGH AIR FLOW rate when either or BOTH packs are in HIGH (give max airflow) when APU is sole source
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10
Q

Describe and state purpose of the RAM air system

A
  • to provide cooling for the PACKS
  • automatically controlled by the packs (through the ram air doors)
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11
Q

When do the RAM air doors open and close

A
  • FULL OPEN
    • on the ground
    • during slow flight with flaps not fully retracted

Normal Cruise

  • door modulate between open and closed
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12
Q

Describe purpose and operation of the deflector doors

A
  • installed forward of the ram air inlet doors
  • prevent slush ingestion prior to liftoff and after touchdown
  • they extend electrically by the air/ground switch
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13
Q

How is overheat protection provided for the PACK

A

there are temp sensors in the cooling cycle

an overheat causes PACK VALVE to CLOSE and PACK light illuminate

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14
Q

How is pack temp output controlled?

A
  • Electronic controllers command the temperature control valve (to open or closed)
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15
Q

Describe what happens with a single or dual pack temp controller failure

A
  • if a primary pack control fails ( SINGLE PACK CONTROLLER FAIL )
    • the affected pack is controlled by the standby controller (opposite controller)
    • causes PACK, MC and AIR COND lights during RECALL

  • if BOTH controllers fail - FOR THE SAME PACK
    • PACK, MC and AIR COND lights illuminate immediately
    • the pack will continue to operate WITHOUT TEMP CONTROL unless excessive temps cause the pack to trip off
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16
Q

How many ‘zones’ are in the aircraft - how are they controlled (temp) - and what is the temp range?

A
  • 3 zones
  • temps are controlled with individual temp selectors
  • temp range: 65 - 85
17
Q

How is air temp determined with pack output

A

packs produce an air temp that satisfies the zone that requires the MOST cooling

zone temp is controlled by introducing trim air to the other zones

the AMOUNT of trim air is controlled by the individual trim air modulating valves

18
Q

Describe single pack ops -

with TRIM AIR ON -

with TRIM AIR OFF -

A
  • ON: zone temps are controlled the same as 2 pack operation
  • OFF: the pack attempts to produce an average temp of ALL 3 ZONES
19
Q

Describe the zone temp controllers and their areas of responsibilites

which controller controls what zones?

Describe the failure modes of the PRI FLT DECK TEMP CONTROLLER and what happens

A
  • Left controller
    • controls AFT zone (primary)
    • Flight Deck (backup controller)
  • Right controller
    • forward & flight deck (primary)
    • aft zone (backup)

FAILURE OF THE PRIMARY FLT DECK TEMP CONTROL (i.e. Right electronic controller)

  • causes an AUTO switch to backup controller
  • illuminates ZONE TEMP light (CONT CAB)
    • ON RECALL if its just the primary controller
  • failure of BOTH controllers will illuminate those lights AUTOMATICALLY
20
Q

What happens to the trim air modulating valves when you have a failure of the FWD or AFT CABIN temp controller.

A
  • causes the associated trim air modulating valve to close
  • the TEMP SELECTORS operate normally
    • BUT - the temp selector settings of the 2 pax cabin zones will be averaged.
  • ZONE TEMP light will illuminate ON RECALL which indicate failure of the associated zone control
    *
21
Q

Any failure affecting the supply of trim air will cause the temp control syst

A