Term
| If winds exceed 65 knots, how should an aircraft be positioned? |
|
Definition
| Position the Aircraft into the wind |
|
|
Term
| When entering the tail compartment, how long must the spaces be allowed to vent prior to entry? |
|
Definition
|
|
Term
The short wire antenna and power ampliflier coaxial tube are pressurized with what?
|
|
Definition
| Sulfur Hexafluoride (SF6) |
|
|
Term
| Since wheel failure can occur with explosive force, what must be considered a special hazard? |
|
Definition
| Overheating or Burning Brakes |
|
|
Term
| Name the three fuselage sections of an E-6B Mercury |
|
Definition
Forward Fuselage
Center Fuselage
Aft Fuselage |
|
|
Term
| How is pressure maintained in the fuselage? |
|
Definition
Seals in the fuselage
a wing-to-body pressure seal
a vapor wing-to-body seal at the wing root |
|
|
Term
Which fuselage compartments are pressurized in flight?
|
|
Definition
Main Cabin
Flight Deck
Forward Lower Lobe
Aft Lower Lobe
Lower Nose Section |
|
|
Term
| What type of Aircraft is the E-6B |
|
Definition
| A jet propelled, long range, high speed aircraft with a swept wing and tail. The E-6B provides a mobile, fast moving platform for the E-6B mission avionics system. |
|
|
Term
| In the Wing Flap System, how many leading edge flaps are there on each wing? |
|
Definition
|
|
Term
| In the Wing Flap System, how many leading edge slats are there on each wing? |
|
Definition
|
|
Term
| In conjunction with the spoilers, what provides lateral control about the roll axis of the aircraft? |
|
Definition
|
|
Term
| The Spoilers are used for all of the following: |
|
Definition
- To assist the ailerons in providing lateral control about the roll axis
- For aircraft speed reduction
- to increase the rate of descent
- On landing, to increase braking effectiveness by transferring weight to wheels more rapidly
- For aircraft pitch trim correction in the event of stabilizer trim malfunction |
|
|
Term
| What are used to spoil the airflow over the wing to decrease lift and create aerodynamic drag? |
|
Definition
|
|
Term
| How many spoilers are located on the upper surface of the wings? |
|
Definition
|
|
Term
| In the Wing Flap System, how many single slotted fillet flaps are on each wing? |
|
Definition
|
|
Term
| How many ailerons are on the trailing edge of each wing? |
|
Definition
|
|
Term
| In the Wing Flap System, how many double slotted wing flaps are on each wing? |
|
Definition
|
|
Term
True/False
The outboard ailerons are used along with the spoilers for high speed and low speed operation
|
|
Definition
|
|
Term
| What system provides longitudinal trim about the pitch axis? |
|
Definition
| Stabilizer Trim Contol System |
|
|
Term
| How is the Stabilizer Trim actuator operated? |
|
Definition
Manually
Manually-electrically
The auto-pilot system |
|
|
Term
| Directional (YAW) control of the aircraft about the vertical axis is provided by which component? |
|
Definition
Rudder
Rudder Control tab
Rudder Control System |
|
|
Term
| When does the Rudder Mechanical system provide directional control? |
|
Definition
| If the hydraulic rudder system fails |
|
|
Term
| What system is designed to provide high lift on takeoff and maximum lift and high drag on approach and landing? |
|
Definition
|
|
Term
| What provides the primary pitch control about the lateral axis of the aircraft? |
|
Definition
|
|
Term
| Once extended, what is required to raise the landing gear? |
|
Definition
|
|
Term
| What Supports the aircraft during landing and all ground operations? |
|
Definition
| Main Landing Gear together with the Nose Landing Gear |
|
|
Term
| What direction does the Main Landing Gear retract? |
|
Definition
|
|
Term
| Name five of the eight major components that each Main Landing Gear consist of? |
|
Definition
Trunion
Shock Strut
Truck
Brakes
Tires and Wheels
Drag Strut
Side Strut
Actuator Walking Beam |
|
|
Term
TRUE / FALSE
The landing gear can be manually extended by operating the emergency extension system hand crank drums |
|
Definition
|
|
Term
| What provides directional control for the aircraft during ground operations? |
|
Definition
|
|
Term
| Which direction does the nose landing gear retract? |
|
Definition
|
|
Term
| Normal Access to the aircraft for maintenance is through the _______________ and through the _______________on to the main deck. |
|
Definition
Forward Lower Lobe
Forward Access Hatch |
|
|
Term
| Which emergency exits are equiped with excape straps that are used for emergency aircraft exit only? |
|
Definition
Pilot and Co-Pilot Sliding Windows
Over the Wing hatches
(4) |
|
|
Term
| Name Six of the Ten Emergency Exits that can be used for ground evacuation form the E-6B Mercury |
|
Definition
- Forward Entry Door
- Aft Entry Door
- Bailout Door
- Forward Cargo Door
- Aft Cargo Doors
- Electronic/Battery Access Door
- Port Overwing Hatch
- Starboard Overwing Hatch
- Pilot Sliding Window
- CO-Pilot Sliding Window
|
|
|
Term
| How many Emergency Exits are there that can be used for ground evacuation from the E-6B Mercury? |
|
Definition
|
|
Term
| What is each main deck entry door equipped with? |
|
Definition
|
|
Term
| What are the exhaust danger areas with engine at takeoff thrust on the E-6B Mercury? |
|
Definition
| Within a 30 degree sweep of the exhaust to 500 feet behind the engine |
|
|
Term
| What are the inlet danger areas with engines at takeoff thrust on the E-6B Mercury? |
|
Definition
| 50 feet in front of the engine inlet and 6 feet behind engine inlet |
|
|
Term
| What is required near aircraft engines during start-up and operation? |
|
Definition
|
|
Term
| What is the exhaust velocity 100 feet aft of the engine at idle on the E-6B Mercury? |
|
Definition
|
|
Term
| What are the Dangers Areas from exhaust at engine idle on the E-6B Mercury? |
|
Definition
| Within a 20 degree sweep of the exhaust to 200 feet behind the engine |
|
|
Term
| What are the engine inlet danger areas at idle on the E-6B Mercury? |
|
Definition
| 25 feet in front of the engine and 5 feet behind the engine inlet |
|
|
Term
| What are the APU danger areas on the E-6B Mercury? |
|
Definition
| 25 feet at a 30 degree arc at the inlet and exhaust of the APU |
|
|
Term
| What component of the CFM56-2A-2 engine is a "front mounted four-staged axial flow unti driven by the LPT (Low Pressure Turbine) |
|
Definition
|
|
Term
| In the CFM56-2A-2 engine, what converts the core engine exhaust gas energy into mechanical energy to drive the fan? |
|
Definition
| Low Pressure Turbine (LPT) |
|
|
Term
| Name two examples of engine mounted sensors and transmitters installed to sense various engine operations of conditions and turn on caution lights if malfunctions exist? |
|
Definition
- Oil Pressure Transmitter
- Oil Quanity Indicator
- N1 Speed Sensor
- N2 Speed Sensor
|
|
|
Term
| Which CFM56-2A-s engine module is the gas generator that provides power to drive the low-pressure system of the engine? |
|
Definition
|
|
Term
| What type of engines are on the E-6B Mercury? |
|
Definition
| CFM56-2A-2 High Bypass Ratio Turbofan |
|
|
Term
| What stage of the four-stage rotor provides engine bypass air? |
|
Definition
|
|
Term
| What act as the LPC (Low Pressure Compressor) for the HPC (High Pressure Compressor) intake? |
|
Definition
| Stages 1 through 4 of the rotor |
|
|
Term
| The four-stage rotor in the Fan module consist of what? |
|
Definition
| a 68 Inch diameter first stage fan and three smaller diameter stage fans |
|
|
Term
| What are the three major components of the Fan Module? |
|
Definition
|
|
Term
| Where is the Accessory Drive Module mounted on the CFM-2A-2 engine? |
|
Definition
| on the bottom of the Fan Frame (which is part of the Fan Module) |
|
|
Term
| In addition to providing thrust for flight, what do the engines provide the E-6B Mercury? |
|
Definition
Power for hydraulic and electrical systems
Bleed Air for the environmental control system
Cross Starting |
|
|
Term
TRUE / FALSE
In the Core Module, discharge air is compressed by the HPC (High Pressure Compressor), heated and expanded in the combustion chamber, then directed by the HPT (High Pressure Turbine) nozzles to the HPT (High Pressure Turbine). |
|
Definition
|
|
Term
| What components are retained in the Fan Frame? |
|
Definition
Front end of the HPC
Fan Rotor
Stator
Accessory Drive
The 12 VBVs. |
|
|
Term
| The accessory drive module consist of what two components? |
|
Definition
Accessory Gearbox (AGB)
Transder Gearbox (TGB) |
|
|
Term
| In the Accessory Drive Module, all of the following are components driven by the AGB (Accessory Gearbox) |
|
Definition
Drives the engine lubrication oil unit
Fuel Pump
N2 Control alternator
aircraft utility hydraulic system pump |
|
|
Term
| What type of electrical power is used by the ignition system of each CFM-2A-2 engine? |
|
Definition
|
|
Term
| How many ignition exciters are used for ground starting as well as in-flight start of the CFM-2A-2 engine? |
|
Definition
|
|
Term
| What component of the CFM-2A-2 engine is "an HPC (high pressure compressor) with variable stator vanes and 5th and 9th stage bleed air manifolds, annular combustion chamber, high pressure turbine nozzles, and HPT (high pressure turbine)? |
|
Definition
|
|
Term
TRUE / FALSE
The LPT (Low Pressure Turbine) drives the fan and booster compressor by an outter (N1) concentric shaft outside the (N2) shaft |
|
Definition
|
|
Term
| What components comprises the LPT (Low Pressure Turbine) of the CFM-2A-2 engine? |
|
Definition
| Four-stage rotor and shaft, case, and frame |
|
|
Term
| How many fuel tanks are there on an E-6B Mercury? |
|
Definition
|
|
Term
| How many fuel tanks are there on an E-6B Mercury? |
|
Definition
|
|
Term
| How many fuel tanks are there on an E-6B Mercury? |
|
Definition
|
|
Term
| What provides postive pressure to vent the fuel system on the E-6B Mercury? |
|
Definition
| A vent scoop at each wing tip |
|
|
Term
| Which two main fuel tanks have an associated reserve tank? |
|
Definition
| Main Tank # 1 and Main Tank # 4 |
|
|
Term
| The E-6B Mercury is equipped with what two methods of refueling? |
|
Definition
Single point ground refueling
Air Refuleing from boom equipped tankers |
|
|
Term
| How is fuel transferred from the reserve tanks to the outboard main tanks on the E-6B Mercury? |
|
Definition
|
|
Term
| What is installed in each main tank and center tank to provide positive fuel pressure to the engine driven fuel pumps? |
|
Definition
| Two Boost pumps are installed in each main tank and center tank |
|
|
Term
| On the CFM56-2A-2 engine, the Bleed Air System consist of all the following components |
|
Definition
Engine Bleed Air
APU Bleed Air
Ground Air Cart
Ducting Distribution
Bleed Air Leak Detectors |
|
|
Term
| What supplies compressed air from the engines, the APU (Auxiliary Power Unit), system and the engine start system |
|
Definition
|
|
Term
| The APU (Auxiliary Power Unit) is gravity fed by which fuel tank? |
|
Definition
|
|
Term
| What is a self contained electrical and pneumatic power source for ground operations on the E-6B Mercury? |
|
Definition
| Auxiliary Power Unit (APU) |
|
|
Term
| The APU (Auxiliary Power Unit) proves pneumatic power for what two purposes? |
|
Definition
Air Conditioning
Engine Starting |
|
|
Term
| What does the APU (Auxiliary Power Unit) provide shaft power for? |
|
Definition
|
|
Term
Where is the APU (Auxiliary Power Unit) installed in the
E-6B Mercury? |
|
Definition
| Lower Aft fuselage section |
|
|
Term
TRUE / FALSE
External electrical or aircraft battery power is normally used to operate the APU (Auxiliary Power Unit) start system. |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Name four of the principal pressure points |
|
Definition
- Superficial Temporal Artery
- Facial Artery
- Common Carotid Artery
- Subclavian Artery
- Brachial Artery
- Radial/Ulnar Artery
- Femoral Artery
- Iliac Artery
- Popliteal Artery
- Anterior/Posterior Tibial Artery
|
|
|
Term
| If hydraulic fluid is decomposed by heat, what is released? |
|
Definition
|
|
Term
TRUE/FALSE
3000 psi of hydraulic fluid pressure is enough to penetrate the skin? |
|
Definition
|
|
Term
| What type of hazard is created by disconnecting pressurized hyraulic lines? |
|
Definition
|
|
Term
TRUE/FALSE
To prevent damage to No. 1 or No. 2 auxiliary hydraulic pumps, verify primary reservior is properly serviced. |
|
Definition
|
|
Term
| What safety equipment shall be worn by personel servicing a hydraulic acculator? |
|
Definition
| Safety Glasses or Face Shield |
|
|
Term
| How many personnel shall be present when servicing a hydraulic accumulator? |
|
Definition
|
|
Term
| What are hydraulic accumulators precharged with? |
|
Definition
|
|
Term
TRUE/FALSE
Hydraulic fluid is not considered hazardous material |
|
Definition
|
|
Term
| What are the five basic hydraulic components? |
|
Definition
| Hydraulic Reservoir, Hydraulic Pump, Check Valves, Hydraulic Lines, Actuator |
|
|
Term
| The E-6B Mercury Utility Hydraulic System has how many variable displacement engine driven hydraulic pumps? |
|
Definition
|
|
Term
| How is the hydraulic utility system powered? |
|
Definition
| Two variable displacement engine driven hydraulic pumps |
|
|
Term
| At a take off RPM, what is each engine driven hydraulic pump capable of delivering? |
|
Definition
|
|
Term
| At cruise RPM, what is each engine driven hydraulic pump capable of delivering? |
|
Definition
|
|
Term
| How is the auxiliary hydraulic system powered? |
|
Definition
| Two electrically driven hydraulic pumps |
|
|
Term
| Name four of the eight systems supplied by the Utility Hydraulic System. |
|
Definition
| Air Refueling Receiver System(Alternate), Landing Gear, Brakes, Leading Edge Flaps, Trailing Edge Flaps, Outboard Spoilers, Nose Gear Steering, Thrust Reversers. |
|
|
Term
| Name the four systems supplied by the Auxiliary Power System. |
|
Definition
| Air Refueling Receiver System (Primary), Auxiliary Power Unit (APU) Start System, Inboard Spoiler System, Rudder Power Control System |
|
|
Term
| The E-6B Mercury hydraulic system delivers hydraulic fluid from what type of reservior? |
|
Definition
|
|
Term
| What directs the flow of hydraulic fluid under pressure? |
|
Definition
|
|
Term
Name two fo the four types of hydraulic system valves on the E-6B Mercury
|
|
Definition
| Brake Interconnect Valve, System Interconnect Valve, Priority Valves, Check Valves |
|
|
Term
| What is the capacity of the hydraulic Utility System reservoir? |
|
Definition
|
|
Term
TRUE/FALSE
The two Auxiliary System hydraulic fluid reservoir are interconnected and are also connected to the Utility System Hydraulic fluid reservoir. |
|
Definition
|
|
Term
| Where are the Auxiliary System hydraulic fluid reservoir located? |
|
Definition
|
|
Term
| Auxiliary system hydraulic fluid is delivered from two reservoirs of what sizes? |
|
Definition
|
|
Term
| The E-6B Mercury has how many 1.25 gallon hydraulic fluid reservoirs in the hydraulic Auxiliary System? |
|
Definition
|
|
Term
TRUE/FALSE
Hydraulic accumalators act as a surge dampener and store hydraulic/pneumatic pressure. |
|
Definition
|
|
Term
| How is a hydraulic accumalator used as a surge dampener? |
|
Definition
| Fluctuations in hydraulic fluid pressure and flow are leveled out |
|
|
Term
| How many types of hydraulic accumalators are on the E-6B Mercury? |
|
Definition
|
|
Term
Name Three of the five hydraulic accumalators on the E-6B Mercury.
|
|
Definition
| Auxiliary Accumalators, Brake Accumalators, APU Start Accumalators, Aerial Refueling Accumalators, Thrust Reverser Accumalators. |
|
|
Term
| How many functions do hydraulic accumalators serve? |
|
Definition
|
|
Term
| What is the maximum hydraulic fluid contamination level? |
|
Definition
| Navy Class 3 for support equipment, Navy Class 5 for all Naval Aircraft |
|
|
Term
TRUE/FALSE
Ground service connections are provided for pressurizing the auxiliary and utliity systems from a hydraulic test stand only. |
|
Definition
|
|
Term
| What is a force which causes current to flow through an electrical conductor? |
|
Definition
|
|
Term
| What is a circuit that consists of both series and parallel networks? |
|
Definition
|
|
Term
| What is an arrangement where electrical devices are connected so that the total current must flow through all the devices , electrons have one path to travel, from the negative terminal to the positive terminal? |
|
Definition
|
|
Term
| What law states: The current in an electric circuit is directly porportional to the electromotive force in the circuit? |
|
Definition
|
|
Term
| What is an electric current that flows in both directions> |
|
Definition
|
|
Term
| The complete path of an electric current is called what? |
|
Definition
|
|
Term
| What is the elementary negative charge that revolves around the nucleus of an atom? |
|
Definition
|
|
Term
| What term is used to signify electrical pressure? |
|
Definition
|
|
Term
| What is a device to connect, disconnect, or change the connections in an electrical circuit? |
|
Definition
|
|
Term
| What is the property of a conductor which determines the amount of current that will flow as the results of the application of a given electromotive force? |
|
Definition
|
|
Term
| What is a unit of electrical resistance? |
|
Definition
|
|
Term
| What type of current flows in one direction only? |
|
Definition
|
|
Term
| Which integrated Drive Generators (IDG) provide power to the mission equipment synchronoius bus |
|
Definition
IDG 2, 4, 6, 7, 8
IDG 2, 4, 6, 8 is okay also |
|
|
Term
| How many integrated Drive Generators (IDG) are there on the E-6B Mercury? |
|
Definition
|
|
Term
| The Auxiliary Power Unit (APU) Generator Power System is connected to the Air Vehicle Synchronoius Bus (AVE Sync Bus) Through which component? |
|
Definition
| Auxiliary Power Contactor (APC) |
|
|
Term
| The Auxiliary Power Unit (APU) Generator Power Systems is connected to which Synchronous Bus through the Auxiliary Power Contactor (APC)? |
|
Definition
| Air Vehicle Equipment Synchronous Bus (AVE Sync Bus) |
|
|
Term
| How many KVA is the Auxiliary Power Unit (APU) Generator on the E-6B Mercury? |
|
Definition
|
|
Term
| What is the minimum electrical power required to perform normal ground operations? |
|
Definition
| 120/208 volt, three-phase, 400 Hz |
|
|
Term
| What is the minimum electrical power required to perform normal ground operations? |
|
Definition
| 120/208 volt, three-phase, 400 Hz |
|
|
Term
| How many integrated drive generators (IDG) are mounted on each E-6B Mercury engine? |
|
Definition
|
|
Term
| Which integrated drive generators (IDG) provide power to the Air Vehicle Equipment Synchronous Bus (AVE Sync Bus)? |
|
Definition
|
|
Term
| What is the power output of the integrated drive generator (IDG)? |
|
Definition
| Three-Phase, 115 Volt, 400 Hz |
|
|
Term
| How many Transformer Rectifier Unit (TRUs) are located on the E-5 rack in the DC Distribution system on board the E-6B Mercury? |
|
Definition
|
|
Term
|
Definition
| External Power Receptacles installed on the left side of the fuselage forward of the wing |
|
|
Term
| In the 28 VAC Power system, the single-phase 115 VAC to 28 VAC transformers are powered by what? |
|
Definition
|
|
Term
| In the 28 VAC power system, how many single-phase transformers are there that reduce 115 VAC to the required 28 VAC? |
|
Definition
|
|
Term
| The 28 volt AC buses supply power to. |
|
Definition
|
|
Term
| How many Transformer Rectifier Units (TRUs) are located on the E-16 equipment rack providing power tot he P-67 circuit breaker panel Mission DC buses? |
|
Definition
|
|
Term
| What does the acronym TRU stand for? |
|
Definition
| Transformer Rectifier Unit (TRU) |
|
|
Term
| What does the acronym ELCU stand for? |
|
Definition
| Electrical Load Control Unit |
|
|
Term
| Name the two main electrical distribution systems on board the E-6B Mercury? |
|
Definition
| AC Distribution System, DC Distribution System |
|
|
Term
| When are the External Power Receptacles EP2A and EP2B used |
|
Definition
| During high power performance checks |
|
|
Term
| How many total External Power Receptacles are there? |
|
Definition
|
|
Term
| Where are External Power Receptacles EP2A and EP2B located? |
|
Definition
| Forward end of the E-16 rack |
|
|
Term
| What happens if the current flowing through a circuit breaker exceeds the circuit breaker's current rating? |
|
Definition
| The circuit breaker should automatically trip |
|
|
Term
| What is the complete path of an electric current is called? |
|
Definition
|
|
Term
| Due to fire hazards, how many times may a circuit breaker be reset? |
|
Definition
|
|
Term
| What does the acronym GCU stand for? |
|
Definition
| Generator Control Unit (GCU) |
|
|
Term
| What are the three sources of power for the Bus Power Control Unit (BCPU)? |
|
Definition
| Auxiliary Power Unit (APU), External Power, Aircraft Generators |
|
|
Term
| Which component's function is to control and protect the synchronous bus? |
|
Definition
| Bus Power Control Unit (BPCU) |
|
|
Term
| What does the acronym FLCU stand for? |
|
Definition
| Frequency and Load Control Unit (FLCU) |
|
|
Term
| What does the acronym BPCU stand for? |
|
Definition
| Bus Power Control Unit (BPCU) |
|
|
Term
| How many frequency and load control units (FLCU)are there on the E-6B Mercury? |
|
Definition
|
|
Term
| Which components provides precise frequency control, which is fed to all eight main generatro frequency and load control units? |
|
Definition
| Frequency Reference Auto-Paralleling Unit |
|
|
Term
| What component provides speed trim signals for controlling real load in each generator channel |
|
Definition
| Frequency and Load Control Unit (FLCU) |
|
|
Term
| What component provides Automatic voltage regulation, Reactive load division, Fault current limiting and power limiting, Fault protection, bus tie breaker, generator circuit breaker, and generator control relay control? |
|
Definition
| Generator Control Unit (GCU) |
|
|
Term
| What does the acronym FRAPU stand for? |
|
Definition
| Frequency Reference Auto-Paralleling Unit (FRAPU) |
|
|
Term
| What are the three pilot static systems for on the E-6B Mercury? |
|
Definition
| Pilot Station Instruments, Co-pilot Station Instruments, Auxiliary System Instruments |
|
|
Term
| What subsystems provides heating circuits on all flight deck windows? |
|
Definition
|
|
Term
| Where is the Fire Detection push to test switch located? |
|
Definition
|
|
Term
TRUE/FALSE
Should the loop be broken, in the wheel well fire detection system, the system retains full capability to detect a fire and the break will be discovered. |
|
Definition
|
|
Term
| What is a single loop system that is activated whenever the control unit detects a decrease in resistance to ground of the sensing element loop due to a overheat condition? |
|
Definition
| Wheel Well Fire Detection System |
|
|
Term
| The Anti-Skid brake system is _____________controlled and provides varying braking pressure according to tire adhesion on the runway after brake pressure is applied. |
|
Definition
|
|
Term
| How many separate pitot static systems are there on the E-6B Mercury? |
|
Definition
|
|
Term
| What system consist of pitot proves and static ports, connected by tubing to flight instruments and equipment for measuring or indicating dynamic (impact) and ambient (static) air pressures? |
|
Definition
|
|
Term
| Which electrical sub-system si commonly known as Auto Pilot? |
|
Definition
| Flight Guidance System(FGS) |
|
|
Term
| What electrical subsystem provides maximum braking efficiency by continously bodulating applied brake pressure? |
|
Definition
|
|
Term
| What provides nominal 24 VDC power to meet emergency DC and AC (inverter) load requirement for a two hour emergency period? |
|
Definition
| Main Aircraft battery set (M686 and M689 is an acceptable answer) |
|
|
Term
| What is a condition in which the current for a fully charged nickel-cadium battery rises out of proportion tot he impressed voltage? |
|
Definition
|
|
Term
| Which batteries are the E-6B Mercury main aircraft battery set? |
|
Definition
|
|
Term
| Name the four batteries located in the E-6B Mercury Forward lower compartment? |
|
Definition
|
|
Term
| How many batteries are located in the E-6B Mercury forward lower compartment? |
|
Definition
|
|
Term
| Which batteries are the Emergency Lighting Battery set that provide power for the emergency lighting system> |
|
Definition
|
|
Term
| What term is applied to those components of the E-6B Mercury aircraft and mission system whose sensitivity to nuclear weapon environments can affect system nuclear survivability? |
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Definition
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Term
| What must be taken in all maintenance operations to retain nuclear hardness? |
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Definition
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Term
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Definition
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Term
| EMP protection built into the E-6B Mercury ensures all mission essential equipment has at least what level safety margin to EMP induced upset? |
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Definition
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Term
| The E-6B Mercury EMP hardening is at how many levels? |
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Definition
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Term
| What is the first level of EMP hardening on the E-6B Mercury aircraft? |
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Definition
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Term
| What is the second level of EMP hardening on the E-6B Mercury aircraft? |
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