Term
| What power source is required to start the APU? 04.01.02.1 |
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Definition
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Term
| What fuel source(s) are available for APU start and operation? 04.01.03.01 |
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Definition
| Battery powered DC fuel pump prior to AC power being available then Left #2 aft tank AC main fuel pump |
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Term
| What system controller is responsible for APU start/stop operation? 04.01.03.01 |
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Definition
| Miscellaneous System Controller (MSC) |
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Term
| When the APU is started from the APU panel when does it provide electrical power? 04.01.05.01 |
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Definition
| When the APU Power switch on the electrical panel is selected ON |
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Term
| When the APU is started from the Electrical panel when does it provide electrical power? 04.01.05.01 |
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Definition
| Automatically after the APU is started |
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Term
| Where can the pre-flight oxygen quantity requirements be found? |
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Definition
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Term
| How many high pressure oxygen cylinders are carried onboard UPS MD-11 aircraft to provide oxygen to the crew, observers and supernumerary stations and positions? 07.01.01.01 |
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Definition
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Term
| Over pressurization (thermal discharge) of the high pressure oxygen cylinders is indicated by? 07.01.01.01 |
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Definition
| Green thermal discharge disc located in two places on the aircraft exterior |
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Term
| A red illuminated NO MASKS switch accompanied by a Level 3 Red Boxed Alert indicates? 07.01.01.02 |
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Definition
| Masks in the crew rest facility have not deployed automatically as required |
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Term
| After the oxygen mask is restowed into the box and doors are shut, what must you do to stop the flow of oxygen to the mask, reset the microphone from mask to boom and retract the OXY ON flag? 07.02.01.03 |
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Definition
| Push the PRESS TO TEST AND REST lever. |
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Term
| With the ENG FIRE handle pulled and the ENG FUEL switch on or off: 08.01.02.01.04 |
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Definition
| The ENG FUEL switch remains illuminated if the fire warning still exists |
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Term
| How many Fire Detection Control Units (FDCU) are installed on the MD-11? 08.01.02.01.03 |
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Definition
| One for each main engine and one for the APU |
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Term
| What happens to the APU when an APU fire is detected? 08.01.02.02 |
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Definition
| The APU will automatically shut down when a fire is detected |
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Term
| What is the electrical power source for engine and APU fire extinguishing? 08.01.02.02 |
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Definition
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Term
| The lower cargo compartment is a Class C compartment meaning: 08.01.03.01 |
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Definition
| Detection and extinguishing are provided |
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Term
| When heat or smoke is detected in a lower cargo compartment: 08.01.03.01 |
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Definition
| Heating and ventilation are automatically shut off |
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Term
| The main deck cargo compartment is a Class E compartment meaning? 08.01.04.01 |
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Definition
| Detection is available, protection is not required |
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Term
| The crew will be notified of smoke detected on the main cargo deck by. 08.01.04.01 |
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Definition
| Master warning lights, aural tone, and a CABIN AIR SMOKE light on the air control panel illuminated red |
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Term
| How is the cargo fire detection and extinguishing system tested? 08.01.04.01 & 08.01.03.01 |
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Definition
| System is automatically tested when the first IRU is turned on. |
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Term
| Why does the Level 3 CGR FIRE LWR ____ checklist direct you to turn the associated cargo flow switch to OFF? 08.01.03.01 |
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Definition
| To prevent restoration of ventilation to the compartment when the smoke or overheat condition is no longer detected |
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Term
| What does the flow DISAG light on the Cargo Fire panel indicate? 08.01.03.01 & 08.02.02.02 |
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Definition
| Ventilation has been automatically shut off, but the flow switch has not been selected to the “off” position |
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Term
| With the Air system in AUTO and smoke detected on the main cargo deck, pushing the Cabin Air Switch to OFF does what? |
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Definition
| Closes the main cargo deck conditioned air shutoff valve and reduces to single pack operation |
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Term
| If the Engine 1 Fire Detection Control Unit simultaneously receives a Fire signal from Loop A and a Fault signal from Loop B, what alert will be displayed? 08.01.02.01.03 |
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Definition
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Term
| If the Engine 1 Fire Detection Control Unit Receives a Fault signal from Loop A and a Fault signal from Loop B outside of 5 seconds from each other, what alert will be displayed? 08.01.02.01.03 |
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Definition
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Term
| If the Engine 1 Fire Detection Control Unit Receives a Fire signal from Loop A and a Normal signal from Loop B what alert will be displayed? 08.01.02.01.03 |
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Definition
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Term
| A list of Level 1 alerts and the required pilot action can only be found where? |
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Definition
| Aircraft Operating Manual (AOM) Chapter 2.3 |
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Term
| During takeoff, when are Level 3 alerts and associated Master Warning lights normally inhibited? 18.01.03.01 |
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Definition
| From V1 to 400’ RA, but no longer than 25 seconds in the air |
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Term
| During landing, when are Level 3 alerts and associated Master Warning lights normally inhibited? 18.01.03.02 |
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Definition
| Level 3 alerts are not inhibited during landing. |
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Term
| During takeoff, level 2 or level 1 alerts are inhibited, depending on alert significance at? 18.01.03.01 |
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Definition
| At throttle advance, 80 knots, or V1-20 knots |
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Term
| During landing, when are level 2 or level 1 alerts and associated Master Caution light inhibited? 18.01.03.02 |
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Definition
| 1000’ AGL to 80 knots ground speed not to exceed 120 seconds |
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Term
| Which item on the Takeoff Essential Items checklist does not produce an aural warning if it is NOT in the proper configuration? 18.01.04.01 |
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Definition
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Term
| The CAWS provides an aural warning, tone and voice, if any gear is not down and locked with the flaps in the landing configuration. To silence the warning: 18.01.05.02 |
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Definition
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Term
| The CAWS provides an aural warning, tone and voice, if any gear is not down and locked, any throttle(s) retarded to idle, airspeed less than 210 knots and flaps not in the landing configuration below 1200’AGL. To silence the warning: 18.01.05.02 |
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Definition
| Push the Gear Horn Off button |
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Term
| The Enhanced Ground Proximity Warning System (EGPWS) combines basic GPWS with? 18.01.07.01 |
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Definition
| Terrain clearance floor, terrain awareness, optional peaks and obstacles |
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Term
| How do the enhanced features of the EGPWS affect the other modes of the GPWS? 18.01.07.01 |
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Definition
| Enhanced features are independent and have no affect upon the other modes of the GPWS |
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Term
| When is the Terrain Clearance Floor feature of the EGPWS active? 18.01.07.01 |
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Definition
| Takeoff, cruise, and final approach |
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Term
| If the Terrain Clearance Floor feature of the EGPWS is penetrated: 18.01.07.01 |
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Definition
| A TOO LOW TERRAIN voice warning is generated twice and an amber GROUND PROX message is displayed on the PFD |
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Term
| When will selecting the ND switch on the System Display Control Panel cause the existing system display to become a Nav display? 18.02.02.01 |
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Definition
| When 1 or more DUs are inoperative |
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Term
| In order to eliminate false terrain alarms, the TERRAIN OVRD switch on the overhead panel should be selected: AOM 01.03.07.01 |
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Definition
| When landing at an airport not contained in the GPWS airport terrain data base |
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Term
| When is the FLAP OVRD position of the GPWS switch on the overhead panel used? 18.02.03.01 |
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Definition
| To prevent the GPWS from actuating during a landing with flaps not in the landing configuration |
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Term
| Which slats have anti-ice protection? 13.01.02.02 |
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Definition
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Term
| Which pneumatic system provides air for the tail anti-ice system? 13.01.02.02 |
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Definition
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Term
| Which of the following air data systems are heated? 13.01.04.01 |
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Definition
| All Pitot tubes, AOA sensors, TAT probe, static ports |
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Term
| Which of the cockpit windows have anti-ice systems? 13.01.04.02 |
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Definition
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Term
| Where are the ice detector(s) located? 13.01.06.01 |
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Definition
| One in each wing engine cowl |
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Term
| What is the function of the Fuel System Controller (FSC) during fuel dumping? 11.01.08.01 |
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Definition
| The FSC monitors the state of the fuel dump valves |
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Term
| Pushing the fuel DUMP switch to ON one time commands the system to dump to what value/quantity? 11.01.08.01 |
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Definition
| Pilot entered FMS DUMP to GW |
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Term
| Pushing the fuel DUMP switch to ON then OFF then ON again will result in the system dumping to what value/quantity? 11.01.08.01 |
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Definition
| Approximately 11,500 lbs per tank |
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Term
| What is the function of the wing fuel vent system? 11.01.10.01 |
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Definition
| Prevents tank pressure from exceeding structural limits |
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Term
| Which fuel pumps are turned ON from engine start until engine shutdown? 11.01.11.01 |
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Definition
| Tanks 1.2 and 3 aft pumps |
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Term
| What is the purpose of Tail Fuel Management? 11.01.11.03 |
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Definition
| Improves cruise performance by maintaining an aft CG |
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Term
| What fuel quantity is required for tail fuel management to take place? 11.01.11.03 |
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Definition
| 60,000 lbs at the termination of refueling |
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Term
| When does tail fuel management begin? 11.01.11.03 |
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Definition
| When the climb phase begins |
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Term
| Descending through what altitude will cause remaining tail fuel to be transferred forward? 11.01.11.03 |
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Definition
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Term
| Transfer of tail fuel forward will terminate when below 17,750’ under what conditions? 11.01.11.03 |
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Definition
| Slats or gear are extended |
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Term
| What is the minimum main tank fuel quantity for cold fuel recirculation to operate? 11.01.11.04 |
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Definition
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Term
| What happen when the fuel temperature in the tail tank drops to within 5º of the fuel freeze point? 11.01.11.04 |
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Definition
| About one third of the tail fuel is transferred forward and replaced with warmer fuel |
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Term
| What happens when the fuel temperature in the tail tank drops to within 3º of the fuel freeze point? 11.01.11.04 |
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Definition
| Tail fuel management is terminated and all remaining fuel is transferred forward |
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Term
| What happens when the Fuel System Controller detects an overfill condition in the tail tank? 11.01.11.11 |
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Definition
| Fuel is transferred out of the tail and the tail quantity is limited to below 12000lbs |
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Term
| What happens to the main tank, aux tank transfer and tail tank transfer pumps when fuel system is selected to manual? 11.01.12.01 |
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Definition
| The pumps are commanded on |
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Term
| What happens to the Tank 2 transfer pump when the fuel system is selected to manual? 11.01.12.01 |
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Definition
| The pump remains in its previous condition |
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Term
| What is the approximate maximum fuel quantity in the tail tank? AOM 01.03.05.03 & SYS 11.01.03.01 |
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Definition
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Term
| What is the approximate maximum fuel quantity in Tank 1 or Tank 3? |
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Definition
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Term
| What is the approximate maximum fuel quantity in Tank 2? |
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Definition
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Term
| The level 1 FMS DUMP DISABLED alert indicates what? 11.02.02.01 |
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Definition
| The fuel dump was not stopped at the FMS dump-to-gross weight entry |
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Term
| What happens if one channel of the FADEC controller fails? 17.01.02.01 |
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Definition
| Normal engine control and operation is maintained |
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Term
| What happens if both channels of the FADEC controller fails? 17.01.02.01 |
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Definition
| The engine will revert to an automatically controlled shutdown |
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Term
| Where does the FADEC system get it power? 17.01.02.01 |
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Definition
| Permanent Magnet Alternator (PMA) |
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Term
| What pilot action will automatically engage the ALTN mode of the FADEC on both engine types. 17.01.02.02 |
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Definition
| Pushing the throttles through the overboost bar |
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Term
| Are autothrottles available with the FADEC system in ALTN? 17.01.02.02 |
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Definition
| GE engines yes, PW engines no |
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Term
| With the ignition system armed. when is ignition automatically provided? 17.01.04.01 |
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Definition
| During takeoff and landing and for 60 seconds after engine anti-ice is commanded on |
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Term
| During takeoff when are the igniters automatically shut off? 17.01.04.01 |
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Definition
| When the flaps/slats are retracted |
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Term
| What is the result of an auto-ignition failure? |
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Definition
| The MANUAL light will illuminate, ignition will be on |
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Term
| What is the function of the IGN TRANSFER switches? 17.01.04.01 |
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Definition
| Allows ignition B to be powered by the LEAC bus |
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Term
| What is the normal power source for A ignition? 17.01.04.01 |
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Definition
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Term
| What is the consequence of a clogged fuel filter? 17.01.06.01 |
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Definition
| Fuel will bypass the filter to maintain flow to the engine. |
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Term
| When will an ENGINE FAIL light be displayed to the flight crew? 17.01.11.01 |
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Definition
| During takeoff between 80 knots and V1 when an engine N1 rpm differs by 11% or more with any other engine N1 |
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Term
| What conditions are required by the FCC to arm the thrust reversers for operation? 17.01.12.01 |
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Definition
| Either radio altitude seven feet or wheel spin up greater than 80 knots |
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Term
| What condition must be met before the reverser interlock will release for the wing engines? 17.01.12.01 |
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Definition
| The reverser must be safely deployed |
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Term
| What condition must be met before the reverser interlock will release for the #2 engine? 17.01.12.01 |
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Definition
| There is no interlock for the #2 engine |
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Term
| What is the maximum taxi weight? |
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Definition
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Term
| What is the maximum takeoff weight? |
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Definition
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Term
| What is the maximum landing weight with the center gear extended? |
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Definition
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Term
| What is the maximum zero fuel weight with the center gear extended? |
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Definition
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Term
| What is the maximum runway slope allowed? |
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Definition
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Term
| What is the maximum allowable tailwind for takeoff or landing? |
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Definition
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Term
| What is the maximum lateral fuel imbalance between tanks 1 and 3? |
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Definition
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Term
| What is the maximum start EGT limits for a GE engine? |
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Definition
| 750 - No time limit/750-870 - 40 seconds |
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Term
| What is the maximum ground start EGT limit for a PW engine? |
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Definition
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Term
| What is the maximum in-flight start EGT limit for a PW engine? |
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Definition
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Term
| What is the maximum autoland weight? |
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Definition
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Term
| When must the autopilot be off during a non-precision approach? |
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Definition
| No lower than 50 feet below MDA |
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Term
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Definition
Eng Ign Ovrd Switch - Ovrd On
ADG - Deploy |
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Term
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Definition
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Term
Engine Abnormal Start
(Hot, Hung, No Start) |
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Definition
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Term
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Definition
Throttle - MCT
Flaps (unless on final) - Up
Speed (unless on final) - Drftdwn or up/ret Vmin +30
Gear (unless committed) - Up
Slats (unless on final) - Ret |
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Term
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Definition
Oxygen Masks - On/100%
Outflow Valve - Verify Closed |
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Term
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Definition
| Flashing Cargo Fire Agent Disch Switch - PUSH |
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Term
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Definition
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Term
| Engine Fire (or Severe Damage) |
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Definition
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