• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/341

Click to flip

Use LEFT and RIGHT arrow keys to navigate between flashcards;

Use UP and DOWN arrow keys to flip the card;

H to show hint;

A reads text to speech;

341 Cards in this Set

  • Front
  • Back

What forms of wood, other than solid wood, are used in aircraft?

laminated and plywood

what is a laminated wood assembly?

two or more layers glued together with the grain of all layers approximately parallel

how is aircraft plywood constructed

usually made of an odd number of thin pieces with the grain of each layer at an angle of 45 to 90 degrees to the adjacent ply.

What species of wood is used as a standard for strength properties?

Spruce.

How would you inspect wood for rot?

check for dark discoloration of the wood surface or gray stains along the grain.

what are the approved types of glues used in aircraft wood structure repair?

casein and resin or any glue approved by the manufacturer.

what effect does room temperature have on gluing wood structures using resin glue?

curing time as well as joint strength.

when are mineral streaks acceptable?

if inspection fails to reveal any decay.

are hard knots acceptable?

yes, within the limits of AC 43.13-1b pg 1-2

why is compressed wood not acceptable?
is not as strong as other woods.

how do you inspect stressed plywood skin?

visual inspection for delamination irregularities and ring test.

why is a bushing in a wooden spar shorter than the spar thickness?

to allow for shrinkage to insure proper seating of the fitting.

what are the results of insufficient gluing pressure?

thick glue lines and weak joint.

what methods are used to apply pressure to wood glue joints?

clamps, brads, nails, presses, screws

what type of joint is generally used in splicing structural members?

scarf joint.

why does the strength of a beveled scarf joint depend on the accuracy of the scarf cut?

the effective glue areas will be reduced if both glue ends are not the same bevel.

how may plywood be prepared for bending?

soak in hot water.

what method will prevent a patch and a plywood pressure plate from adhering due to extruding glue from the patch?

use wax paper between the patch and the pressure plate.

what area of a wood spar may not be spliced?

under a wing attachment, landing gear, engine mount and lift strut fittings.

what is the maximum number of splices that should be made to any one spar?

two

why are large area washers used in wooden structures?

to minimize compression damage.

what is the minimum temperature for curing wood joints with resin glue?

70 degrees f.

what are the two types of fabric used for covering aircraft?

organic and synthetic.

what are organic fibers?

cotton and linen.

what are synthetic fibers?

fiberglass and heat shrinkable fibers (nylon, orlon and dacron)

what determines the strength requirements for a fabric covered aircraft?

the manufacturer by the never to exceed speed and wing loading.

what strength fabric should be used for recovering an aircraft?

high grade aircraft textile at least as good a quality and equivalent strength as those originally used by the manufacturer.

what is the purpose of reinforcing tape?

it is used over ribs and between fabric rib stitching to prevent the stitching cord from cutting through the fabric.

what is the fabric warp?

the direction along the length of the fabric.

what type of machine sewed stitches are used?

french fell, folded fell and plain overlap.

what should be done to structures that will be covered with doped fabric?

dope proof with a protective coating of paint or tape.

where is surface tape used?

sewed seams, lapped edges, rib stitching and screws.

what is the advantage of the envelope method of covering wings?

practically all sewing is by machine.

when are anti tear strips recommended?

when the never to exceed speed is in excess of 250 mph.

how are ventilation and drainage hole edges reinforced?

plastic, aluminum or brass grommets.

what methods are used to check doped fabric?

a punch tester. when the results are marginal, a laboratory test is needed.

what is the maximum permissible deterioration used for fabric aircraft?

30% of original fabric strength.

what type of fabric is not affected by moisture or mildew?

fiberglass.

what is the fabric selvage edge?

an edge of cloth woven to prevent raveling.

what rib stitching spacing is used when the original spacing is unknown?

use chart in ac 43.13-1b

what is a tie off knot?

a standard modified seine knot used on all stitches other than the starting knot.

inw hat direction is the warp and selvage edge of aircraft fabric applied and what identification is usually found on the selvage edge?

it is parallel to the line of flight and the TSO number is recorded on the selvage edge.

what are the common types of paints used on aircraft?

primers, enamels, lacquers and epoxies.

what is used with zinc chromate primer it it is too thick and needs to be thinned?

toulene

what are two types of dope used on aircraft?

nitrate and butyrate.

why should dope not be used over paint or enamel?

because it tends to remove the paint or enamel.

what happens to pain finishes if excess drier is added to the paint?

the results will be a brittle film causing cracking and peeling.

what is the purpose of zinc chromate primer?

serves as a corrosion resistant covering and base coat for protective topcoats.

what is the advantage of using butyrate dope instead of nitrate dope from a safety point of view?

less flammable.

when spraying acrylic lacquer, what health safety precaution should the mechanic observe?

use an approved respirator.

what are three methods of applying paint?

dipping, spraying and brushing.

what type of paint may be used over epoxy topcoats?

any paint system in good condition.

what is the cause for spray painting dust?

incorrect air pressure or distance of gun from work.

what may cause spray paint sags and runs?

too much paint being applied or inadequate surface preparation.

what causes "orange peel" spray finish?

incorrect paint viscosity, air pressure, gun setting or distance of the gun from the work.

what is a blushing paint finish?

clouding or light spots on the surface.

what will cause a blushing paint finish?

moisture in the air supply, adverse humidity or changes in temperature.

what would be the result of applying a coat of dope when the temperature of the dope room is too high?

pinholes in the dope film.

what areas must be protected from damage when using paint remover/stripper?

synthetic rubber products, composites, fabrics, acrylics and bonded surfaces.

what is the reason for paint touchup, other than appearance?

helps to eliminate general corrosion problems.

how can a mechanic determine if the control surfaces need to be checked for balance after painting?

check manufacturers service manual and/or check with the manufacturer.

what size and location standards must be used for an aircraft registration marking?

as prescribed by far 45.

what is done with the rivet head stem when a self plugging (friction lock) rivet is installed?

pulled until snapped and trimmed flush with the head.

give an example of a self plugging mechanical lock rivet.

cherry lock or huck.

what type of tools are required to install cherrylock rivets?

hand or power tools equipped with mechanical pulling head.

describe correct dimensions on a properly upset rivet.

1 1/2 diameter wide, 1/2 diameter tall.

what is bonded honeycomb construction?

laminar constructed combination alternating dissimilar materials (two metal facings bonded on each side of a core).

what materials are used in honeycomb construction?

stainless steel, titanium, magnesium, plywood, glass, nylon and cotton cloth.

what may cause delamination of honeycomb construction?

some vibration, liquid leakage, internal condensation and manufacturer mistakes.

what is a potting compound used for in bonded honeycomb repair?

hole filling.

what is done to the damaged area in a bonded honeycomb?

the damaged area must be removed.

what will cause crazing in transparent plastic panels/windshields?

stress, improper handling and harmful solvents.

what procedure should be used when drilling plexiglass, to prevent damage to the hole as the drill point breaks through the underside?

backup with wood and feed slowly.

what should be done to twist drills that are to be used for drilling completely through fiberglass?

modified to a 60 degree tip angle, cutting angle to a zero rake and increase the back lip 12 to 15 degrees.

what calculation must be made when bending sheet metal?

bend allowance.

what must be done when two bends intersect?

relief holes are drilled at the intersecting point.

what type of weathering damage may be found on metal aircraft?

corrosion.

what methods are used when forming sheet metal?
shrinking, stretching, bending, crimping and folding.

what factors are used to determine setback?

radius of the bend and thickness of the material.

what is the purpose of lightening holes cut in rib sections.

reduce weight.

what is a joggle?

an offset formed on an angle strip to allow clearance for a sheet or extrusion.

determine total length of a solid rivet for installation.

1 1/2 diameter greater than the total thickness of material to be joined.

how do you determine the proper material to be used for a repair?

manufacturers current data/service manual. if not covered by manufacturers current data, use 43.13-1b

what is the spacing and edge distance for protruding head rivets?

edge distance is two times the diameter and spacing is three times the diameter.

describe rivet head markings for a, b, d, ad and dd rivets.

a - plain (1100) b - cross (5056) d - raised dot (2017) ad - dimple (2117) and dd - double dash (2024)

why dimple for flush rivets instead of counter sink?

depends on the thickness of the sheet.

what kind of loads are rivets designed to withstand?

shear.

describe criteria for replacement of a 2024 rivet with a 2117 rivet.

for 5/32 or less diameter, use next size rivet, assuming spacing and edge distance meet minimum requirements.

what happens to magnesium if the flux is not removed after welding?

severe corrosion will occur.

magnesium is limited to what type of joint weld?

butt welds.

what must be done in the weld zone to successfully weld titanium?

the weld zone must be shielded with an inert gas.

why is it necessary to use flux in all silver soldering?

to have the base metal chemically clean without the slightest film of oxide.

what type of flame is used for silver soldering?

oxyacetylene flame should be neutral.

what type of repair could be made for a dented steel tube cluster joint?

weld a formed steel patch plate over the dented area.

what method can be used to insert a tight fitting inner sleeve into a tubular repair?

cool the sleeve with dry ice.

what are three general types of welding?

gas, electric arc and electric resistance.

how is a soft flame obtained without reducing thermal output?

using a larger tip and adjusting the gas pressure.

what is the most desirable method to use when welding aluminum?

heliarc (dc) welding.

what valve should be turned off first when extinguishing a torch?

the acetylene, to allow the gas tip to burn out.

what procedure will control expansion when welding a joint?

tack welding at intervals along the joint.

what safety precaution should be taken when gas welding has been completed?

turn off the valves and relieve all pressure.

what must be done with heat-treated aluminum alloys that are weldable after a weldable repair has been made?

it must be re-heat treated.

what is the result of insufficient penetration?

low strength weld.

what type of welding causes less buckling and warping than gas welding?

metallic arc-welding.

what is gas-shielded arc welding?

a gas is used as a shield around the arc to prevent the atmosphere from contaminating the weld.

what are the advantages of gas-shielded arc welding?

stronger, more ductile and more corrosion resistant.

what does the size of the torch tip opening determine?

the amount of heat, not the temperature.

what is a servo trim tab?

an auxiliary control positioned by movement of cockpit controls and aids in moving control surfaces.

what is a balance trim tab?

an auxiliary control positioned by fixed linkage in opposite direction of control surface and aids in control surface movement.

what is a spring tab?

an auxiliary control that aids in moving the primary control surface by keeping direct proportion of deflection to the aerodynamic load imposed on the surface.

name several high lift devices.

leading edge flaps, slots, slats and trailing edge flaps.

what are three mechanical methods used to actuate flight control systems?

cable, push-pull rods and torque tube.

what is the purpose of a rotorcraft cyclic pitch control?

changes the pitch of each main rotor blade during a cycle of rotation.

what is the purpose of the rotorcraft collective pitch control?

varies the lift of the main rotor(s) blade(s) simultaneously.

what unit compensates for helicopter main rotor torques?

auxiliary or tail rotor.

what control a helicopter tail rotor?

anti-torque pedals.

what flight control surfaces are considered the primary group?

ailerons, elevators and rudders.

what is considered the secondary flight control group?

trim tabs and spring tabs.

what flight controls are included in the auxiliary group?

wing flap, spoilers, speed brakes, leading edge flaps and slots.

what are the three axes of an aircraft?

vertical, longitudinal and lateral.

where does breakage of control cables occur most frequently?

where cables pass over pulleys and through fairleads.

what items must be known when measuring flight control cable tension?

desired tension and temperature.

what are cable tension regulators?

a mechanical device that automatically maintains cable tension.

what is a cable fairlead?

cable guide.

what is the purpose of vortex generators?
boundary layer air control.

why are control surfaces locked when an aircraft is parked?

prevent wind damage to controls.

what tools are used to check control surface travel?

propeller protractor, ruler, templates, rigging fixtures and special tools.

in accordance with far 65.85 and 65.87, what type of inspection may a certificated airframe and powerplant mechanic sign off?

100 hour inspection.

when may a mechanic perform an annual inspection?

when the mechanic holds an inspection authorization.

when must an annual inspection be performed, if required for a particular aircraft?

within the preceding 12 calendar months.

what may be used as a checklist for 100 hour inspection?

any checklist which meets the minimum standard of far 43 appendix d.

where is a list of information that is required for aircraft records after completion of a 100 hour inspection?

far 43 and far 91.

who may approve for return to service a progressive inspection phase check?

certificated a and p mechanic, certificated repair station or the aircraft manufacturer.

when is a 100 hour inspection required on aircraft operating under far 91 (general operating rules)?

aircraft carrying persons for hire or aircraft used for flight instruction for hire.

when is the first 100 hour inspection due after discontinuance of a progressive program?

100 hours after the last complete inspection of the progressive program.

does an aircraft under a progressive inspection program need a 100 hour inspection if the airplane is used for flight instruction for hire?

no.

what are the privileges and limitations of a mechanic with regards to propellers?

minor repairs and minor alterations and inspections.

what kind of charge is used to inflate a landing gear shock strut?

dry air or nitrogen.

what regular inspection should be made of the exposed portion of a landing gear strut?

clean and inspected for damage and proper extension.

what is the purpose of landing gear torque links?

keep the landing gear pointed in a straight ahead direction.

what power sources are normally used to retract landing gear systems?

hydraulic and electrical.

what type of nosewheel steering is provided on small aircraft?

simple system of mechanical linkage hooked to the rudder pedals.

what unit prevents nosewheel vibration?

shimmy damper through hydraulic action.

what are some types of brake systems?

independent, power boost, power control.

what is the purpose of power brake debooster cylinders?
reduce the pressure to the brake and increase the volume of fluid flow.

wha must be accomplished before inspecting a wheel and brake system for hydraulic leaks?

pressurize the system.

what prevents a split wheel from leaking air through the inner and outer mating surfaces or the wheel assembly?

a rubber packing between the two assemblies.

what is the most necessary maintenance function for safe, long aircraft tire service?

proper inflation.

what are the effects on tires if under inflated?

rapid or uneven wear near the edge of tread and creep or slip when the brakes are applied.

when should a landing gear retraction check be accomplished?

during an annual inspection (or other inspection), when landing gear components have been replaced, and after hard landings.

what is the indication of excessive heating of a wheel bearing?

discoloration.

what is the purpose of antiskid system?

bring a fast moving aircraft to a stop during ground roll without tires skidding.

what is the purpose of a wheel fusible plug?

relieve air pressure to prevent tire blowout.

what are some methods of bleeding brakes?

gravity and pressure.

how is the braking load transmitted from the wheel to the rotating disk?

by slots and keys.

what methods are used for steering large aircraft?

mechanical, electrical and hydraulic.

what prevents a nose landing gear from being retracted with the nosewheel out of the center position?

nosewheel centering internal cams or external track.

what are three types of hydraulic fluids?

vegetable, mineral and phosphate ester base fluids.

what color is mineral base hydraulic fluid?

red

what happens to plastic resins, vinyl, lacquers and oil base paints if exposed to phosphate eater based hydraulic fluid such as 'skydrol'?
the material will be damaged, softened and/or peeled.
what feature is built into a hydraulic pump-drive system to prevent damage in the event of a pump seizure or overload?
a shear section in the pump-drive shaft.
what precautions should be taken to minimize contamination during replacement of a hydraulic unit?
All lines should be plugged or capped after disconnecting and cleaned before assembly.
what would cause a hydraulic filter to go into open bypass, allowing unfiltered fluid into the system?
a clogged filter.
what are the sources of hydraulic pressure in an aircraft?
hand pumps, engine driven pumps, electrically driven pumps.
what are methods of pressurizing a hydraulic reservoir?

cabin pressurization, turbine compressor, aspiratior and venturi-tee.

how is a gear type pump operated?

two meshed gears that revolved in a housing are driven by a power unit. fluid is trapped and pressurized as the gears turn.

what are the types of engine driven hydraulic pumps?

constant-delivery and variable-delivery

what is the purpose of a pressure relief valve?

to limit the amount of pressure, thereby preventing failure of the system components.

what is the purpose of a pressure regulator?

to manage the output of the pump.

what is used in some hydraulic systems to supplement the power pump when several units are operated at the same time?

accumulator.

what are the types of accumulators?

diaphragm, bladder and piston.

for what purpose are pneumatic systems used in some aircraft?

to operate brakes, doors, drive pumps and engine starting.

what are sources of pneumatic power?

storage bottles, vane type pumps and turbine engine compressors.

what happens to excessive pressure in a pneumatic pressure system?

relief valve will bleed to the atmosphere.

What is the purpose of restrictors that are used in aircraft pneumatic systems?

to control the rate of airflow.

why should a pneumatic system be purged periodically?

to remove contamination and moisture.

what must be accomplished with any accumulator prior to disassembling?

make sure air or preload has been discharged.

what are the two groups of independent cabin compressors?

positive displacement and centrifugal.

what is the principal control of a pressurization system?

outflow valve.

what method is used by some turbine powered aircraft for pressurization?

bleed air from the turbine engine compressor section.

what is a roots blower?

engine driven compressor based on the intake of a predetermined volume of air that is compressed and delivered to the cabin duct.

what pressurization control unit will change the position of an outflow valve?

the cabin pressure controller.

what are three methods of supplying heat when "heat of compression" is not sufficient for cabin air conditioning?

gasoline combustion heater, electric heater, and exhaust gas air-to-air heat exchanger.

what is the function of ventilating air in a combustion heater?

a blower, ram air or cabin compressor.

what components are used in an air cycle cooling system?

expansion turbine, air-to-air heat exchanger and various valves.

what causes a temperature drop in an air cycle cooling system?

the compressed air performs the work of turning a turbine.

how does a water serparator remove moisture from the air?

the air passes through vanes that swirl the air and droplets are collected and drained.

what is vapor cycle cooling?

freon cooling.

what components are in a vapor cycle cooling system?

evaporator, compressor, condenser and expansion valve.

what is a continuous-flow oxygen system?

oxygen will flow from a charged cylinder through a high-pressure line to a reducing valve and to mask outlets.

what is a pressure demand oxygen system?

oxygen will fill from a charged cylinder on demand of the user.

what must be accomplished to an oxygen system if it has been open to atmosphere for 2 hours or more?

purged to remove moisture.

what is used to purge oxygen lines of moisture?

dry nitrogen, dry air or oxygen.

what type of oxygen must be used in aircraft?

Aviators breathing oxygen

why is oil added to a vapor cycle freon system?

to provide lubrication and prevent compressor failure.

what safety precautions should be observed when servicing oxygen systems?

oil free tools, clothing hands and adequate eye protection.

what are sources of ventilating air in a combustion heater?
a blower, ram air or cabin compressor.

what is used as a guide for range marking instruments?

aircraft specifications or type certificate data sheets and flight manual.

what does a yellow arc on an instrument dial indicate?

caution.

who can apply range marking to the instrument dial face?

certificated instrument repair stations.

why are slippage marks used on instrument dial face?

to indicate loose glass.

when are range markings placed on an instrument glass and what precaution must be taken?

the glass must be marked for slippage indication.

what can be used to static check a manifold pressure indicator?

current atmospheric pressure.

what other instruments may be used to check manifold pressure indicator for correct indication?

a sensitive altimeter or barometer.

what indication errors may be found in altimeters?

scale, hysteresis and installation.

what flight indication errors are usually connected to a pitot static system?

rate of climb, airspeed and altimeter.

why is it undesirable to clear obstructions from pitot static holes with a tool?

the holes are aerodynamically critical.

what is required for replacement of components connected to a pitot static system?
a leak test.

what methods are used to drive a turn and bank indicator?

air pressure (positive and negative) and electricity.

what causes and electric-driven gyro rotor to tilt when the aircraft is turned?

gyroscopic procession.

what is a synchro-type remote indicating system?

transmits information from one point to another point (flap position).

what does a capacitor-type fuel quantity system accurately determine?

weight of fuel in the tanks.

what does a tachometer indicate?

crankshaft or main turbine rotor speed.

where does an electrical resistance temperature indicator receive a signal from?

from a heat sensitive element or bulb.

what type of indicating system is a turbine-engine exhaust gas temperature system?

thermocouple.

what is the meaning of "swinging" a compass?

adjusting the n - s and e - w magnets.

what should be looked for during an inspection of a magnetic compass?

the bowl should be filled with liquid and should not contain any bubbles or discolorations.

what precautions should be taken regarding hardware used for installation of a magnetic compass or nearby instruments?

use non-magnetic hardware.

what are three basic autopilot components?

gyros, servos and an amplifier.

what are the sensing elements of an autopilot system?

direction gyro, turn and bank gyro, attitude gyro and altitude control.

what are the actuating elements of an autopilot system?

microphone, transmitter, transmitting antenna, receiving antenna, receiver and handset.

what is the most common communication system in use?

very high frequency (vhf).

how often does the atc transponder require certification?

every 24 calender months.

what are the components of a typical airborne VOR system?

receiver, visual indicator, frequency selector, antennas and power supply.

what are two antennas usually required for an ILS system?

vertical guidance for correct angle of descent.

when may an ELT legally be checked for operation?

during the first 5 minutes of the hour.

what is a DME?

distance measuring equipment.

what is VOR equipment used for?

navigation.

where should a DME antenna be located?

on the lower surface of the aircraft in a position that will not be blanked by the wings in a bank.

what is an ADF?

automatic direction finder.

what type of antennas do most transponders have?

short stub usually mounted on the lower surface of the fuselage.

what powers an emergency locater transmitter?

self-contained battery.

what method is used to monitor the output signal during an ELT test?

use vhf communications receiver tuned to 121.5 MHz.

how may the determination be made to replace the battery in an ELT even though the set operates?

the replacement date is marked on the outside of the transmitter.h

how should coaxial cable be routed from an antenna to a receiver?

secured every 2 feet, not routed with other wire bundles and at least ten times the cable diameter.

what is the purpose of a radio shock mount bonding jumper?

to provide a low-impedance ground return.

what are the components of a communication system?

mic, transmitter, transmitting antenna, receiving antenna, receiver and handset.

what information does a glideslope radio bean provide?

vertical guidance for correct angle of descent.

what is the purpose of a fuel dump system?

reduce the weight of the aircraft to a specified landing weight.

when would the fuel jettison system be required?

when the maximum takeoff weight exceeds the maximum landing weight.

what purpose other than reducing weight is accomplished with a fuel jettison system?

lateral stability may be obtained with a heavy wing aircraft due to fuel out of balance.

what are the two types of fuel tanks?

bladder and intergral.

what supports the weight of the fuel in a bladder type fuel cell?

the structure of the cavity that the cells fits into.

what is a wet wing type construction?

intergral fuel cell.

what is the purpose of a fuel temperature indicator in a turbine powered aircraft?

to determine when there may be a danger of ice crystals forming in the fuel.

what is the purpose of a crossfeed system?

an interconnected fuel system so that fuel can be fed from various tanks to any engine.

what positions may be selected on a fuel tank selector valve?

fuel tank positions, crossfeed and on or off.

what is a drip gauge?

an underwing bayonet type gauge.

what is an electrically operated fuel tank shut off valve in-transit light?

indicates when the valve is in motion.

what is a pressure fueling system?

underwing or single point fueling system.

what are advantages of single point pressure fueling?

reduces fueling time, eliminates aircraft skin damage and reduces chances of contamination.

what should be done with old gaskets and seals when replacing fuel system components?

remove and replace with new ones.

what type of fuel system leak will not be visible by evidence of stains or wet spots?

an internal fuel leak (shutoff valve, selector valve or crossfeed valve)

what are four types of fuel quantity gauges in use today?

sight glass, mechanical, electrical and electronic.

why is an electronic type fuel quantity gauge more accurate than others?

measure by weight instead of gallons.

what is the purpose of fuel tank internal baffles?

resist fuel surging caused by changes in attitude of aircraft.

what method may be used to check a fuel tank for leaks after a patch or weld has been performed?

air pressure up to 1/2 PSI and liquid soap to detect any leaks.

why should you wait a period of time after fueling before checking fuel pumps?

to allow time for water and sediments to settle to the drain point.

what may be used to determine the size of an unmarks wire?

a wire gauge.

why should an electrical system be checked before a load increase?

to determine that the wire, cable, or protection device limit will not be exceeded.

what instruments are used to monitor electrical loads?

ammeter and voltmeter.

what is a "trip free" circuit breaker?

it cannot be reset until the condition is corrected.

when should a switch be derated from its normal rating?

for high rush in circuits, inductive circuits and electrical motors.

where is the white position/navigation light mounted?

on the tail, always visible from the rear.

what color is the left wingtip light?

red.

what factors are considered when selecting wire size for electrical power?

allowable power loss, permissible voltage drop and current carrying ability.

what type of electrical items may cause short time demand loads on an electrical system?

landing gear motor, radio transmitter and flap motor.

when do electrical motors draw several times their rated current?

during start.

how long should bonding jumper wires be?

as short as practicibal.

what hardware is used to make bonding or grounding connections to a structure of dissimilar materials?

a washer of suitable material should be used so that corrosion will occur on the washer and not the part.

what should be done to a conduit end when fittings are not used?

flared to prevent wire insulation damage.

what size electrical conduit should be used?

twenty-five percent larger than the maximum diameter of the wire bundle.

what three faults are associated with electrical system malfunctions?

open circuits, shorted circuits and power.

when is a circuit breaker designed to open?

before the conductor emits smoke.

what causes an AC electric motor to run slow?

no lubrication, applied low voltage or wiring defects.

what could cause an AC electric motor to run fast?
excessive supply voltage or motor field windings shorted.

what controls the output voltage of an alternator?

the DC exciter.

during trouble shooting, when is a continuity check made?

when the power is off.

how many terminal lugs can be put on a single terminal strip in an aircraft?

four.

how can a particular wire in a bundle be identified?

ID code on the wire.

where is a circuit breaker located in a circuit?

as close to the power source as possible.

what types of landing gear warnings are provided for retractable landing gear systems?

an audible or visual device.

when does an audible device operate in a landing gear warning system?

when the throttle is retarded and the landing gear is not down and locked.

what types of position indicators indicate landing gear down and locked?

green lights and/or visual indicators.

what is the purpose of a mach warning system?
audible warning that aircraft speed

how does a take off audible warning differ from a landing gear audible warning?

audible tone of take off horn is intermittent.

what items may cause a take off warning horn to operate in a typical transport jet aircraft?
speed brakes, flaps, stabilizer and auxilliary power exhaust door.
what does an anti-skid warning indicate?
system failure or system is turned off.

what is the indication of an anti-skid system automatically returning to a manual brake system?

a warning light.

when is the time to check landing gear switches, lights and warning horns or buzzers for proper operation?

during a gear retraction check.

what positions of retractable landing gear must be indicated?

secure up and secured down.

if an aircraft has only one indicator light, will the switches on the landing gear be connected in series or parallel with each other?

series.

where are the procedures located for checking and adjusting landing gear switches?

aircraft manufacturers manual.

what other aircraft system may activate the landing gear warning system?

the flaps, when extended past the given number of degrees with the landing gear in the retracted position.

what type of indication is usually provided for stall warning?

audible and/or visual.

what type of indications are used for cabin doors in the open and closed position?

visual and warning lights.

what is the reason for a master caution warning system in aircraft?

to alert the crew of system operation or malfunction.

what system is used to indicate battery over-temperature?

warning lights or temperature indicator.

what is the purpose of the annunciator system?

to show, by warning lights, that a system has failed or a caution condition exists.

what is the source of the anti-skid warning system?
the anti-skid control box.

what condition will cause a wing leading edge anti-ice overheat light to illuminate?

failure of a thermal switch to cause closure of the anti-ice valve.

what are the two methods of inflating pneumatic deicer boots?

engine driven vacuum pump and bleed air from a turbine engine compressor.

how are deicer boots attached to leading edges of wing and tail surfaces?

cement, fairing stripes and screws, or a combination of both.

what is the function of the air/oil separator used in some deicer boot systems?

in a wet type vacuum pump system, it is used to remove oil from the pressurized air.

what must be accomplished to a deicer boot prior to a cold patch repair?

relieve the installed tension.

what normally keeps deicer boots held down in flight?

suction is supplied to the boots during flight.

what methods are used to supply heat for thermal anti-icing systems?

turbine compressor bleed air, engine exhaust heat exchangers and ram air heated by a combustion heater.

how is the temperature maintained in a thermal anti-icing system?

by mixing bleed air and ambient air.

what prevents overheating of the wing leading edge skin in a thermal anti-ice system, that is operated by engine bleed air?

a thermal switch will cause a valve to close and shut off the flow of bleed air when the temperature of the skin reaches a predetermined value.

what happens to the thermal anti-icing airflow after it has heated a leading edge surface?

the airflow is exhausted to the atmosphere.

why are anti-ice systems using turbine engine bleed air provided with an overheat system?

to prevent aircraft structure damage.

what are several problems associated with electrically heated windshields?
delamination, scratches, arching and discoloration.

when is windshield delamination acceptable?

when within limits established by manufacturer and it is not in an open area where it affects optical qualities of the windshield panel.

what are the effects of electric windshield arcing?

local overheating and damage of windshield.

how can an electrically heated pitot tube with an ammeter installed in the system be checked for operation?

verified by noting the current consumption when the heater is turned on.

what methods are used to remove rain from a windshield?

wiping off, blowing off and chemical rain repellent.

what powers windshield wiper systems?

electrical or hydraulic power.

what are the two problems accompanied with windshield wipers when operated in flight?

aerodynamic forces reduce blade pressure and failure to achieve fast enough wiper oscillation.

how does a pneumatic rain removal system work?

the air blast forms a barrier that prevents raindrops from striking the windshield.

why is a windshield rain repellent system not operated when the windshield is dry?

heavy undiluted repellent will restrict window visibility.

what is the purpose of the electronic timer in a pneumatic deicer boot system?

controls the operating sequence and time intervals.

where are carbon monoxide detectors normally used?
aircraft cabins and cockpits.
what is the indication of excess carbon monoxide fumes when using a "co" tester?
the tester changes color to green, dark gray or black.

how does a photoelectric smoke detector warn of possible fire?

smoke in the air will cause the photoelectric cell to conduct an electric signal to a detector amplifier.

how may a photoelectric smoke detector be checked?

use of a test switch circuit.

name two types of smoke instruments used in aircraft?

photoelectric and visual

what is a thermal switch fire detection system?

heat sensitive units that complete electrical circuits at a certain temperature.

how are thermal switch units wired?

parallel with each other and in series with the lights.

how are fenwal spot detectors wired?

parallel between two complete loops of wiring.

how is a thermal couple fire warning system different from a thermal switch system?

thermal switch works at a specific temperature whereas the thermocouple depends on a rate of temperature rise.

what is continuous loop detection system?

one or more wires imbedded in a special ceramic core that changes its resistance with a change in temperature.

what is continuous element fire detection system?

a stainless tube containing a discrete element which will produce gas with heat and a mechanical switch to activate the system.

what are two types of fire extinguishing systems?

high rate of discharge and conventional systems.

what is the most common fire extinguishing agent associated with a conventional system?

carbon dioxide.

what type of extinguishing agent is usually found in a high rate of discharge system?

halogenated hydrocarbon type agents (halon)

what procedure is used to check a freon container for pressure?

a chart must be used for a minimum and maximum gauge reading for every change of temperature.

what protection is provided for a fire bottle in case of a temperature rise in excess of set limits?

a safety disk will rupture and spill the agent overboard.

what is the purpose of the yellow disk in a co2 type fire extinguishing system.

indicates a normal system discharge.

what may be caused by kinks and sharp bends in sensing elements of a fire detection system?

false fire warning and/or inoperative system.

how is a fire bottle discharged?

electrically by a discharge cartridge.

how is the service life of a discharge cartridge calculated?

from the manufacturers data stamp or the face of the cartridge.