| Term 
 
        | Maximum Takeoff Weight\Taxi |  | Definition 
 
        | Taxi 144,000 (-500)=143,500 Max Takeoff |  | 
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        | Maximum Payload (Importance) |  | Definition 
 
        | 35,900. IF YOU ARE OVER THIS you fail test |  | 
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        | Term 
 
        | Seating Class and Total Passengers |  | Definition 
 
        | 8 First class + 138 Economy = 146 People |  | 
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        | Max Takeoff and Landing Altitude |  | Definition 
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        | Max Operating (Due to Compass Malfunction) |  | Definition 
 
        | 73 Degrees North and 60 Degrees South |  | 
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        | Max cabin differential pressure in flight |  | Definition 
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        | Max differential for takeoff and landing |  | Definition 
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        | Term 
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        | 1,000 lbs for taxi, takeoff, flight, or landing |  | 
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        | Term 
 
        | Main tanks must be full if center tank contains greater than |  | Definition 
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        | Term 
 
        | Scavenger Pump activates below ______lbs and dumps fuel into engine ___. |  | Definition 
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        | Term 
 | Definition 
 
        | 8 pumps, 2 engine driven, 6 electrical. Scavenger pump in center feeds into engine 1, can create lateral imbalance. Bypass valves are used for engine driven pump. |  | 
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        | Term 
 
        | Is there any fuel transfer capability? |  | Definition 
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        | Term 
 
        | When do you need to fuel the center tank? What is total fuel capacity? |  | Definition 
 
        | If your fuel capacity is over 20,236 (10,118 each wing) Then you can add up to 15,613 in the center. Total fuel capacity is 35,849. |  | 
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        | Term 
 | Definition 
 
        | The purpose is to prevent damage to the wings do to excess buildup of pressure inside the fuel tanks. |  | 
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        | Term 
 
        | Can fuel filter be bypassed? |  | Definition 
 
        | Yes, dirty fuel is better than no fuel |  | 
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        | Term 
 
        | Are the fuel pumps AC/DC powered? |  | Definition 
 
        | DC, one generator failure will not affect more than one fuel pump |  | 
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        | Term 
 
        | 3 Sources of pressure For A/C |  | Definition 
 
        | Main engine bleeds (2 engines one source), APU, ground pneumatic. |  | 
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        | Term 
 
        | Ground preconditioned air |  | Definition 
 
        | goes to mix manifold, almost straight into airplane |  | 
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        | Term 
 
        | Where does air go from mix manifold? |  | Definition 
 
        | Hot air goes into Pack Valves (2) (goes in hot comes out room temp.) goes to Mix Manifold to Cockpit, FWD Cabin, or AFT Cabin |  | 
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        | Term 
 
        | A/C Pack has how many radiators? |  | Definition 
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        | Term 
 | Definition 
 
        | Bleed air goes through primary heat exchange, compressor, secondary heat exchange, water separator, turbine, water separator, mix manifold |  | 
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        | Term 
 
        | You blow an A/C pack in the air, what do you do. |  | Definition 
 
        | Descend to 25,000 (eastbound) or 24,000 (westbound), only if you have enough fuel. |  | 
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        | Term 
 
        | How many generators and what voltage for electrical? |  | Definition 
 
        | 3 generators 115 volts ac |  | 
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        | Term 
 
        | What is the A/C D/C conversion rates? |  | Definition 
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        | Term 
 | Definition 
 
        | **(*edit me)3 Generators producing 115 v ac, 3 transformer rectifier (28 dc to 115 ac), |  | 
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        | Term 
 | Definition 
 
        | Ram air turbine, falls out of belly, spins in air stream. |  | 
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        | Term 
 
        | Hydraulic System A and B Operate |  | Definition 
 
        | Rudder, Ailerons, Elevators, landing gear, nose wheel |  | 
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        | Term 
 
        | Hydraulic system A operates only |  | Definition 
 
        | Inboard flight spoilers, aternate brakes, autopilot a, thrust reverser one |  | 
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        | Term 
 
        | Hydraulic system B Operates only |  | Definition 
 
        | Outboard flight spoiler, autopilot B, trailing edge flaps |  | 
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        | Term 
 | Definition 
 
        | Auto slats and leading edge flaps and slats and rudder |  | 
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        | Term 
 
        | What does the power transfer unit control? |  | Definition 
 
        | Auto slats and leading edge devices |  | 
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        | Term 
 | Definition 
 
        | They are staggered in order of importance so that if there is a leak, you won't use primary systems, it ensures there is always enough fluid to operate electric motor. |  | 
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        | Term 
 
        | Which wheel has no brakes? |  | Definition 
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        | Term 
 
        | Steering nose wheel can only be accomplished via what speed? |  | Definition 
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        | Term 
 
        | Autobrake is initiated upon... |  | Definition 
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        | Term 
 | Definition 
 
        | Skidding and reduces landing and stopping distance, as well as keeps all wheels spinning at same speed. |  | 
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        | Term 
 
        | Do distances for landing include thrust reversers? |  | Definition 
 
        | No, landing is brakes only |  | 
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        | Term 
 
        | Classes of fire extinguishers and usage |  | Definition 
 
        | A-Combustible B-Flammable
 C-Live electrical
 |  | 
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        | Term 
 
        | Only three have fire protection, which ones? |  | Definition 
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        | Term 
 
        | with a wheel well fire you do what? |  | Definition 
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        | Term 
 
        | Both fire bottles for main engines can be used on main engine, can the APU be satisfied the same way? |  | Definition 
 
        | No the APU has it's own freon tank |  | 
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        | Term 
 
        | The cargo area puts out fires how? |  | Definition 
 
        | It is sealed, so oxygen will be used up quickly. |  | 
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        | Term 
 
        | Two types of anti icing... |  | Definition 
 
        | Electrical and Thermal Anti Icing |  | 
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        | Term 
 
        | Electrical is located where? |  | Definition 
 
        | Windshields, pitot tubes, antennas |  | 
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        | Term 
 
        | Thermal covers what two areas |  | Definition 
 
        | Leading edge devices from engine outward and engine cowl lip |  | 
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        | Term 
 
        | Thermal bleed air comes from which stage and when |  | Definition 
 
        | 5th and 9th stages at idle, 5th stage in flight due to heat |  | 
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        | Term 
 
        | Thermal anti icing is required |  | Definition 
 
        | AT 8 Celsius and below due to water and skin of airplane. Ice blocks can cause a loss of lift, causing a failure in a missed approach procedure. |  | 
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