MD-11 Air Systems
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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| Trim Air provided by which systems | show 🗑
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| Trim Air Switch controls | show 🗑
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| Temp Control Knobs control | show 🗑
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| show | Avionics Bay
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| show | Systems 1 & 2 (Left Side)
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| show | Right side of AC
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| show | AC Power Application
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| show | 3 each (only one runs at a time)
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| show | Exhaust Fan ON, Venturi CLOSED for TO
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| show | Exhaust Fan OFF, Venturi OPEN @ 1.5 PSI differential
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| show | Cooling airflow insufficient, Pressurization airflow insufficient, Altitude (cabin) >10,000'
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| show | Exhaust Fan is ON, Venturi is CLOSED
(comes on for normal takeoff)
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| Air System Test is initiated by | show 🗑
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| show | Trim air shut-off
Engine 2 anti-ice duct
Manifold fail detect syst
Avionics Fan
CAC fans
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| "CAB ALT" light means | show 🗑
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| "NO MASKS" light means | show 🗑
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| Does the Trim Air switch work in auto or manual mode | show 🗑
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| "AVNCS OVHT" light in Trim Air Switch means and does what | show 🗑
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| CABIN AIR switch when pressed does what | show 🗑
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| Pack "FLOW" light illuminated means | show 🗑
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| 1-2 or 1-3 ISOL switch "DISAG" light means | show 🗑
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| show | Do not interconnect two or more active engine pneumatic supply systems
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| show | A/C is pressurized in flight and APU AIR is selected ON
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| "PRESS" light in PRV switch means | show 🗑
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| "TEMP HI" light in PRV switch means | show 🗑
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| "TEMP HI" in AUTO results in | show 🗑
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| "TEMP HI" in MANUAL results in | show 🗑
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| "MANF" light means | show 🗑
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| "MANF" light in AUTO results in | show 🗑
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| "MANF" light in MAN results in | show 🗑
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| # 1 "MANF" light alone, leak is _____ | show 🗑
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| #1 & 2 "MANF" lights, leak is _____ | show 🗑
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| show | Aft of CAC up to #2 engine
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| show | Right engine to fuselage, up FWD right tunnel to pack
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| show | Inside the CAC
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| show | Performs decay check to isolate problem
Turns good systems back on
Red "MANF" lights on until sys cools
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| show | Heated, vented, and cooled from SYS 3
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| show | Heated only from SYS 2
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| Aft Cargo compartment | show 🗑
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| show | 9.1 PSI
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| Normal Differential Pressure | show 🗑
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| show | 43,200'
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| Pressure Reliev Valves begin to open at __ fully open at __ | show 🗑
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| Max Differential Pressure on the ground | show 🗑
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| show | .55 PSI
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| show | 100' Below Field Elevation
Slats Extended (cleared to configure)
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| Bleeds and Packs come back on during normal takeoff profile at | show 🗑
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| show | 4500' AFE
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| show | 5000' AFE
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| Aircraft depressurizes on landing when | show 🗑
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| show | Closes holes, depressurizes, inhibits GPWS and some landing gear warnings
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| show | <100', 0.5, 0.55, Pwr Red, 4500', 5000', 8.6, 8.76, 9.1, 43,200'
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| "NO ICE DETECTED" light inhibited below | show 🗑
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| show | One lost system, pilot must determine when to turn on AI
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| EAI uses ___ stage air | show 🗑
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| show | The outer 5 slats
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| Rule of 4s | show 🗑
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| If you lose 2 bleed sources, one source may power __ points while ___ | show 🗑
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| Eng 2 Anti Ice Duct DUAL shroud leak produces | show 🗑
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| show | Level 1 alert SEL ENG 2 AI OFF
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| If SINGLE shroud w/leak and valve does not close then | show 🗑
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Created by:
cakorps