Air Systems Flashcards

1
Q

ZONE TEMP

A

-Overtemperature
-For CONT CAB also means both temperature controllers failed

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2
Q

PACK Switch AUTO

A

-With Flaps Up and other switch OFF, regulates to high flow
-When supplied by APU, regulates to high flow

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3
Q

Engine Bleed System

A

-From 5th and 9th stages of compressor (4 / 9 for MAX)
-Valves DC operated and pressure activated

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4
Q

Duct Pressure

A

-Min 18psi
-Max 60psi
-If shows 0, try to press Trip Reset

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5
Q

Unbalanced PACK Temperature Control

A

-When trim air supply not available
-If CONT trim air not available: Left PACK supplies selected CONT temperature
-If cabin or all trim air not available: FWD / AFT average

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6
Q

AC Distribution

A

-Left PACK to cockpit, rest to mix manifold
-Right PACK to mix manifold
-Recirculation Fans and Ground Air to mix manifold

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7
Q

Zone Temperature Controllers

A

-Left Electronic Controller: Aft Cabin and Backup for Flight Deck
-Right Electronic Controller: Forward Cabin and Primary for Flight Deck

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8
Q

Overboard Exhaust Valve Open

A

-On the ground and inflight <2psi differential pressure
-Either PACK Switch HIGH AND R Recirculation Fan Switch OFF

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9
Q

Differential Pressure Limits

A

-8.35psid >37000ft
-7.80psid 28000-37000ft
-7.45psid <28000ft
-8.45psid when climbing above FLT ALT

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10
Q

Maximum Cabin Altitude

A

8000ft

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11
Q

AUTOFAIL Light Reasons

A

-Cabin pressure change >2000fpm *
-Differential pressure >8.75psid *
-Cabin Altitude >15800ft *
-Outflow Valve control fault
-Controller fault (*)
-Loss of DC power

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12
Q

Cargo Compartment Minimum Temperatures

A

-FWD +5 degrees
-AFT 0 degrees

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13
Q

Engine and APU Bleed for PACK Operation

A

-APU is capable for 2 PACKs on the ground
-Don’t operate 2 PACKs from one engine on the ground
-Engine is capable of 1 PACK inflight (MAX 2 PACKs)

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