This quiz, titled '2A553C CDC Volume 2 URE', evaluates knowledge in aerospace maintenance, focusing on preventative inspections, damage types, lubrication, tool control, and tool kit organization. Essential for professionals managing aircraft maintenance and safety.
Electrostatic discharge (ESD).
Solvent.
Abrasion.
Solvent entrapment.
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Silicone.
General-purpose grease.
General-purpose lubricating oil.
High-temperature lubricating oil.
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Reduce tool costs through the use of chits.
Make end-of-shift tool inspections more efficient.
Eliminate damage to aircraft and to control aircraft costs.
Eliminate damage to aircraft, equipment, and to control tool assets.
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Foam cutouts in a tool tray.
Tools set loosely in a drawer.
Contrasting foam depressions.
Tools hung on a shadow board.
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In a way determined by the wing commander.
Tools that cannot be marked will not be placed in CTKs.
Create a designated position in the CTK for the item and listing it on an inventory.
In a container marked with the identification number and number of tools contained within.
Using nonconducting packaging materials.
Using proper insulating materials.
Dehumidified air.
Humid air.
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15,000.
9,000.
6,000.
4,000.
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Antistatic.
Conductive.
Nonconductive.
Static dissipative.
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Remove protective caps or covers.
Touch the LRU case with your hands.
Ensure the aircraft is properly grounded.
Touch the ends of aircraft wiring to the LRU case.
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A metallic braid over the insulation.
A metal conductor covered with a dielectric.
An inner conductor separated by an insulation dielectric.
A compact wire bundle with self-contained wire assemblies.
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Electromagnetic pulse (EMP).
Insulated wire.
Shielded.
Coaxial.
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Twisted pair.
Coaxial.
Triaxial.
Shielded.
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Smaller size.
Wider bandwidth.
Lower signal attenuation.
Immunity to electromagnetic interference.
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None.
Attenuation always increases.
Attenuation always decreases.
Attenuation increases or decreases depending on frequency.
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Source.
Emitter.
Detector.
Converter.
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Zener diode.
Pin photodiode.
Injection laser diode.
Avalanche photodiode
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Zener diode.
Pin photodiode.
Injection laser diode.
Light emitting diode.
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Core.
Buffer.
Cladding.
Shielding.
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100 meters.
150 meters.
300 meters.
450 meters.
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A shielded line.
An air coaxial line.
A flexible coaxial line.
A parallel two-wire open line.
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Check the standing-wave-ratio of the cable.
Check for an open between the inner and outer conductors.
Check for an open outer conductor between the connectors on each end of the cable.
Check for a shorted outer conductor between the connectors on each end of the cable.
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Copper.
Radiation.
Induction.
Dielectric.
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An ammeter.
A voltmeter.
A neon bulb.
A slotted line section.
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High power loss.
Size restrictions.
Low power handling capability.
Use is limited to low frequencies.
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Isolator.
Magic tee.
Choke joint.
Directional coupler.
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Friction coupling.
Threaded coupling ring.
Bayonet lock.
Insertion.
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Twice the inside diameter.
Double the outside diameter.
Six times the inside diameter.
Six times the outside diameter.
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Use rosin-core 60/40 tin/lead solder.
Use a small soldering pencil (less than 100 watts).
Apply heat at the dielectric end of the center pin body.
Feed solder through the hole in the side of the center pin.
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One and a half times the length of the cable.
Two times the length of the cable.
Two and a half times the length of the finished bundle.
Three times the length of the cable.
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Frayed to cable jacket.
Damage to internal wires.
Loose outer shield.
Broken pins at the connector.
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Up to 20 percent of the inner shield circumference.
Up to 20 percent of the outer shield circumference.
Up to 25 percent of the inner shield circumference.
Up to 25 percent of the outer shield circumference.
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Ensure proper lighting.
Inventory required tools.
Read all procedures in TO 1–1A–14.
Warnings concerning use of heat tools on aircraft.
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End separation.
Lateral displacement.
Angular misalignment.
Perpendicular displacement.
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Shine.
Polish.
Etch-and-bend.
Scribe-and-break.
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ST.
BNC.
SMA.
TNC.
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Code division.
Time division.
Frequency division.
Wavelength division.
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Increases reliability.
Decreases available space.
Reduces aircraft weight.
Reduces the volume of wires.
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It is faster and uses less twisted wire pairs.
It is faster and uses more twisted wire pairs.
All data bits are received in sequence and uses less twisted wire pairs.
All data bits are received at the same time and uses more twisted wire pairs.
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3.
16.
20.
32.
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Bus controller (BC) to RT.
RT to BC.
RT to RT.
BC to BC.
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Transferring the subsystem time.
Obtaining program data from an RT.
Sending initialization instructions to an RT.
Commanding an RT to initiate a system self-test.
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Fuselage.
Windows.
Stabilizers.
Wing carry-through.
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8.
6.
5.
4.
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Movable fairings for wing sweep mechanism.
The forward equipment avionics bay.
A wheel well fuel tank.
Two weapons bays.
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4.
5.
6.
7.
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Forward center.
Aft center.
Aft intermediate.
Outboard aft intermediate.
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Interior.
Exterior.
Intermediate.
GLAS.
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Upper and lower crew compartments.
Attachment point for the wings to the fuselage.
Landing gear, the bomb bay, and center wing tank.
Drag chute compartment, aft electronic countermeasures (ECM) system, and antennas.
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