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51.

A spoiler may also be called as __________(a) Lift dumper(b) Lift enhancer(c) Thrust dumper(d) Thrust enhancerI had been asked this question in an international level competition.This question is from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Right answer is (a) Lift dumper

Explanation: A spoiler may ALSO be called a lift duper, or lift spoiler. It is a device PLACED to INTENTIONALLY manipulate the lift component of an airfoil in a controlled WAY.

52.

Which of the following spoilers are used for descent control?(a) Inboard spoilers(b) Outboard spoilers(c) Mid span spoilers(d) Fixed spoilersI had been asked this question during an interview for a job.My question is from Aircraft Electronics topic in section Aircraft Electronics of Aircraft Maintenance

Answer»

Correct ANSWER is (a) Inboard spoilers

Explanation: For DESCENT control in an aircraft, inboard spoilers are used. Further, when ROLL control is required, the aircraft MAKES use of outboard spoilers, which MAY also be referred to as mid span spoilers.

53.

Spoilers work differently from airbrakes.(a) False(b) TrueThis question was addressed to me in an internship interview.Question is taken from Aircraft Electronics in section Aircraft Electronics of Aircraft Maintenance

Answer» RIGHT CHOICE is (b) True

The best I can explain: True, spoilers on an aircraft work differently as COMPARED to AIRBRAKES. Spoilers are responsible for reducing lift, on the contrary airbrakes have no EFFECT on the lift of an aircraft.
54.

Which of the following is not true about spoilers?(a) Create a controlled stall(b) Decrease descent rate(c) Placed on wings(d) Reduce liftThe question was posed to me in semester exam.The origin of the question is Aircraft Electronics in portion Aircraft Electronics of Aircraft Maintenance

Answer»

The correct option is (b) DECREASE descent rate

Explanation: Spoilers help in increasing descent rate without increasing speed. These devices CREATE a controlled stall over the PORTION of the WING behind it.

55.

Where are the spoilers placed on an aircraft?(a) On the top surface of a wing(b) On the bottom surface of a wing(c) On the top surface of an engine(d) On the bottom surface of an engineI got this question during an online interview.Question is taken from Aircraft Electronics topic in division Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT ANSWER is (a) On the top surface of a wing

Explanation: In an AIRCRAFT, the spoilers are placed on the top surface of a wing. They are plates that can be extended upward into the AIRFLOW to spoil it.

56.

How is the airspeed affected in a descent without spoilers?(a) Set to zero(b) No affect(c) Decreased(d) IncreasedThis question was posed to me in class test.This intriguing question comes from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Correct choice is (d) Increased

For explanation I WOULD say: The airspeed is increased when an aircraft descends without spoilers. Further, the ENGINE will be at low POWER THUS producing less heat than normal.

57.

Which of the following position is selected for lift dumpers on the landing approach?(a) Off(b) Manual(c) Automatic(d) DeployedI have been asked this question in an interview for internship.Enquiry is from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (c) Automatic

The BEST EXPLANATION: Automatic position is selected for lift dumpers on the landing approach. These DEVICES are deployed in a fraction of a SECOND at the moment of touchdown.

58.

What is the combination of spoilers and ailerons called?(a) Ailpoilers(b) Spoilerons(c) Spelerons(d) SpoailsI have been asked this question by my college director while I was bunking the class.Asked question is from Aircraft Electronics topic in division Aircraft Electronics of Aircraft Maintenance

Answer»

The correct OPTION is (b) SPOILERONS

For EXPLANATION: The combination of spoilers and ailerons is called spoilerons. These DEVICES ALSO avoid the problem of control reversal that affects ailerons.

59.

Spoilers increase the lift component of an airfoil.(a) False(b) TrueThis question was addressed to me during an interview.My question is based upon Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

The correct option is (a) False

The best I can explain: False, spoilers reduce the lift component of an AIRFOIL. This reduction is DONE in a CONTROLLED WAY by ALTERING the airflow over an aircraft wing.

60.

What is the full form of PIO?(a) Pitch induced oscillation(b) Pilot inclined oscillation(c) Pilot induced oscillation(d) Pitch inclined oscillationI got this question during an interview for a job.I need to ask this question from Aircraft Electronics topic in division Aircraft Electronics of Aircraft Maintenance

Answer»

The correct option is (c) Pilot INDUCED oscillation

To explain I WOULD SAY: PIO refers to pilot induced oscillation. These are oscillations that OCCUR due to the pilot’s effort to control the aircraft. Such oscillations are necessary for providing stability to the aircraft.

61.

In an FBW system, how are the electronic signals transmitted?(a) Manually(b) Using radars(c) Using sensors(d) Using wiresThe question was posed to me during an internship interview.This key question is from Aircraft Electronics in section Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (d) USING wires

To explain I would say: In an FBW system, the ELECTRONIC SIGNALS are transmitted using wires. The movements of flight controls are first CONVERTED to electronic signals and then transmitted.

62.

FBW system replaces the manual flight controls of an aircraft with an _________ interface.(a) Automatic(b) Electronic(c) Mechanical(d) ThermalI had been asked this question during an internship interview.My question is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Right answer is (b) ELECTRONIC

Explanation: The FBW system REPLACES the manual flight CONTROLS of an aircraft with an electronic interface. The manual flight controls may ALSO be referred to as conventional controls.

63.

Fly by wire systems require pilot’s involvement.(a) True(b) FalseThis question was addressed to me during a job interview.This intriguing question comes from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT answer is (b) FALSE

The best EXPLANATION: False, fly by wire systems do not require pilot’s INVOLVEMENT. These systems protect the pilot operating outside of the aircraft’s safe PERFORMANCE envelope.

64.

FBW is a ________ electrically signaled system.(a) Pseudo(b) Physically(c) Partially(d) PurelyI have been asked this question in a job interview.The doubt is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

The correct answer is (d) PURELY

Easiest EXPLANATION: FBW SYSTEMS are purely electrically signaled systems. These are modern systems equipped on both military and commercial aircrafts. Such systems are ALSO helpful in reducing the gross weight of an aircraft.

65.

What is the full form of BITE?(a) Built in training equipment(b) Built in task equipment(c) Built in transfer equipment(d) Built in test equipmentI had been asked this question during an online interview.My doubt is from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (d) BUILT in test equipment

The best explanation: BITE in aviation terminology refers to built in test equipment. Such equipment’s are used primarily on aircraft’s FEATURING FBW SYSTEMS in ORDER to conduct their preflight safety checks.

66.

Which of the following was the first Airbus aircraft to feature FBW controls?(a) A320(b) A380(c) 777(d) A340I have been asked this question during an interview.This intriguing question comes from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

The correct option is (a) A320

For explanation I WOULD say: The Airbus A320 series of AIRCRAFTS were the FIRST Airbus airliners that used full-authority FBW CONTROLS. Boeing followed with its 777 aircraft.

67.

Which was the first pure electronic fly-by-wire aircraft with no mechanical or hydraulic backup?(a) Airbus A380(b) Airbus A320(c) Apollo 11(d) Apollo Lunar Landing Training VehicleI got this question in semester exam.I would like to ask this question from Aircraft Electronics topic in division Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (d) APOLLO LUNAR Landing TRAINING Vehicle

Explanation: The Apollo Lunar Landing Training Vehicle was the first ever aircraft to FEATURE pure electronic FBW SYSTEMS. The aircraft first flew in 1968 and did not have any kind of mechanical or hydraulic backup.

68.

A FBW aircraft can be lighter as compared to a similar design with conventional controls.(a) True(b) FalseThe question was asked in an international level competition.I would like to ask this question from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

Answer» RIGHT ANSWER is (a) True

To elaborate: True, FBW aircraft can be lighter as COMPARED to a similar design with conventional controls. This is partly because of the lower overall weight of the SYSTEM components, and partly because the NATURAL stability of the aircraft can be relaxed.
69.

Which of the following was the first production fly-by-wire airliner?(a) 737(b) A320(c) Concorde(d) MD80I got this question in my homework.Asked question is from Aircraft Electronics topic in section Aircraft Electronics of Aircraft Maintenance

Answer»

The correct ANSWER is (C) Concorde

The EXPLANATION is: The Concorde was the first production fly-by-wire AIRLINER. The aircraft first flew on 2 March 1969 and retired on 24 OCTOBER 2003.

70.

Which of the following is not true about FBW systems?(a) Improved safety(b) High maintenance costs(c) Physically lighter(d) ReliableI have been asked this question in an online interview.This interesting question is from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer» CORRECT option is (b) High maintenance costs

Explanation: FBW systems are credited for REDUCING the maintenance costs as COMPARED to the conventional controls. These systems are much more reliable and also provide enhanced flight economy.
71.

The Airbus A340 has a purely _________ back-up rudder control system.(a) Electrical(b) Electronic(c) Manual(d) HydraulicI have been asked this question during an online exam.I want to ask this question from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

The correct answer is (a) ELECTRICAL

To elaborate: The AIRBUS A340 has a purely electrical back-up rudder CONTROL SYSTEM. However, beginning with the A380, all flight control systems on airbus aircrafts have back-up systems that are purely electrical.

72.

Which of the following is the first business jet with fly-by-wire controls?(a) Learjet 45(b) Learjet 60(c) Dassault Falcon 7X(d) Gulfstream G550I have been asked this question during an online interview.My question is taken from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT answer is (C) Dassault Falcon 7X

For EXPLANATION I would say: The Dassault Falcon 7X was the first business jet with fly-by-wire CONTROLS. The aircraft OFFERS a range of 5,950 nautical miles.

73.

Fly by optics is also referred to as fly by light.(a) True(b) FalseThe question was posed to me by my college director while I was bunking the class.This question is from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

The correct answer is (a) TRUE

The best explanation: True, Fly by optics is also referred to as fly by light. This is due to the USE of fiber optics. The system might be USED instead of fly by wire because it offers a HIGHER data transfer rate.

74.

What is the full form of FADEC?(a) Flight Authority Direct Engine Control(b) Flight Authority Digital Engine Control(c) Full Authority Digital Engine Control(d) Full Authority Direct Engine ControlThis question was addressed to me during an interview.Question is from Aircraft Electronics in portion Aircraft Electronics of Aircraft Maintenance

Answer»

Correct choice is (c) Full AUTHORITY Digital Engine Control

Easiest explanation: FADEC refers to Full Authority Digital Engine Control. It is a system that permits OPERATION of the FLIGHT control SYSTEMS and auto throttles for the engines to be fully integrated.

75.

In power by wire systems, the hydraulic circuit is replaced by an ________ circuit.(a) Electrical power(b) Thermal power(c) Electronic power(d) Mechanical powerThe question was asked in examination.My question is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer» RIGHT ANSWER is (a) Electrical power

To explain I would say: In power by wire (PBW) systems, hydraulic CIRCUIT is REPLACED by an electrical power circuit. The elimination of hydraulic CIRCUITS reduces the maintenance cost and also improves the efficiency of an aircraft.
76.

Which of the following is the first production aircraft to feature fly by optics?(a) Learjet 23(b) Hawker 4000(c) Learjet 40(d) Kawasaki P-1I had been asked this question in final exam.This intriguing question originated from Aircraft Electronics topic in portion Aircraft Electronics of Aircraft Maintenance

Answer» RIGHT ANSWER is (d) Kawasaki P-1

Explanation: The Kawasaki P-1 is the FIRST production aircraft to feature FLY by optics. The aircraft is manufactured by Kawasaki Aerospace Company and first flew in 2007.
77.

Boeing airliners allow the pilots to completely override the computerized flight control system.(a) True(b) FalseI have been asked this question in an international level competition.This key question is from Aircraft Electronics in portion Aircraft Electronics of Aircraft Maintenance

Answer»

Correct answer is (a) True

To explain: True, Boeing aircrafts such as the 777 ALLOW the pilots to COMPLETELY override the computerized flight control SYSTEM. However, Airbus flight envelope control SYSTEMS always retain ultimate flight control while flying under NORMAL law.

78.

Electrostatic sensitive device is a component which can be damaged by common _________(a) Dynamic charges(b) Static charges(c) Electric charges(d) Electronic chargesI had been asked this question during an online interview.I need to ask this question from Aircraft Electronics topic in portion Aircraft Electronics of Aircraft Maintenance

Answer» CORRECT choice is (B) Static charges

Easiest explanation: Electrostatic SENSITIVE device is a component that can be damaged by common static charges. Densely packed electronic PARTS become more and more vulnerable to ESD.
79.

ESD in common terminology refers to ___________(a) Electrostatic discharge(b) Electric discharge(c) Electronic discharge(d) Elastic dischargeThis question was addressed to me in homework.My query is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer» CORRECT choice is (a) Electrostatic discharge

The best I can explain: The term ESD in common TERMINOLOGY refers to Electrostatic discharge. These are a certain type of charge particles that are commonly found on humans, ELECTRONIC tools and VARIOUS other objects. They may be HAZARDOUS under certain conditions.
80.

What is the electrical resistance of conductive ESD protective materials?(a) Between 1mΩ and 1MΩ(b) Between 1kΩ and 1MΩ(c) Between 10kΩ and 10MΩ(d) Between 10mΩ and 10MΩThe question was asked in an online quiz.My question is based upon Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer» CORRECT answer is (b) Between 1kΩ and 1MΩ

Explanation: The electrical RESISTANCE of conductive ESD PROTECTIVE materials is between 1kΩ and 1MΩ. There are several KINDS of ESD protective materials AVAILABLE.
81.

Which of the following is a material that attenuates current and electrical fields?(a) Anti-static(b) Conductive(c) Shielding(d) DissipativeThis question was addressed to me in an interview.The origin of the question is Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

The correct answer is (c) SHIELDING

To explain: Shielding material is a material that attenuates CURRENT and electrical fields. DIFFERENT ESD materials POSSESS different characteristics and BEHAVE differently in the same environment.

82.

Dissipative materials have an electrical resistance between 1kΩ and 1TΩ.(a) False(b) TrueI had been asked this question in homework.This interesting question is from Aircraft Electronics topic in section Aircraft Electronics of Aircraft Maintenance

Answer» RIGHT CHOICE is (a) FALSE

The best I can explain: False, dissipative materials have an electrical resistance between 1MΩ and 1TΩ. Electrical resistance of such materials is greater as COMPARED to conductive materials.
83.

Anti-static materials are also known as _________ materials.(a) Low charging(b) High charging(c) Null charging(d) Dash chargingThis question was addressed to me in an interview for job.I want to ask this question from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Correct answer is (a) LOW charging

To elaborate: The anti-static materials are also known as low charging materials. These materials limit the buildup of charges by PREVENTION of triboelectric EFFECTS, through PHYSICAL SEPARATION.

84.

Which of the following is an alternate to photoemission?(a) Shielding(b) Proton emission(c) Corona discharge(d) Electrical groundingThis question was addressed to me at a job interview.Question is from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT OPTION is (a) Shielding

The best I can explain: Corona DISCHARGE is an alternate to photoemission. It is an electron emission effect used by antistatic systems. It is mostly used in a larger area, such as a factory floor or workshop.

85.

An ionizing bar is sometimes referred to as a _________(a) Anti dynamic bar(b) Antistatic bar(c) Dynamic bar(d) Static barThe question was posed to me in semester exam.This interesting question is from Aircraft Electronics topic in portion Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT choice is (d) Static BAR

For EXPLANATION I would say: An ionizing bar is sometimes referred to as a static bar. It is a type of an anti-static device used for removing static ELECTRICITY from a production line.

86.

Human beings have natural electrical sources running through the body.(a) False(b) TrueI had been asked this question in exam.I would like to ask this question from Aircraft Electronics in section Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (b) True

Explanation: True, HUMANS beings have natural electrical sources running through the body, thus touching an ESD unequipped can result in serious material damage or injuries.

87.

Which of the following is a device that reduces or inhibits electrostatic discharge?(a) Dynamic device(b) Static device(c) Anti-static device(d) Anti-dynamic deviceThe question was asked in an interview for internship.This key question is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT answer is (C) Anti-static device

Easy EXPLANATION: Devices that decrease the magnitude of electrostatic DISCHARGE may be referred to as anti-static devices. Such devices if not used PROPERLY may also damage electrical components.

88.

Which of the following is used for the neutralization of static charges in a larger area?(a) Photoemission(b) Antistatic agents(c) Electrical grounding(d) Static agentsI got this question in unit test.The query is from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Correct answer is (a) Photoemission

The explanation: The process of neutralization of STATIC charges present in a SIGNIFICANTLY larger AREA, may be CALLED as photoemission. The process is based on the EMISSION of electrons into an area, which in turn neutralize the targeted object.

89.

Dissipative bags are usually _________ in color.(a) Yellow(b) Pink(c) Purple(d) BlueI got this question by my school principal while I was bunking the class.This question is from Aircraft Electronics in portion Aircraft Electronics of Aircraft Maintenance

Answer»

Correct CHOICE is (b) Pink

For EXPLANATION I would say: Dissipative bags are USUALLY pink in color. This is because of the dissipative chemical layer.These bags COME with a static dissipative coating or layer on the PLASTIC.

90.

A static bag is used for storing or shipping electronic components which may be prone to damage caused by electrostatic discharge.(a) False(b) TrueI got this question during an online exam.This intriguing question originated from Aircraft Electronics topic in portion Aircraft Electronics of Aircraft Maintenance

Answer»

The CORRECT ANSWER is (a) False

Best explanation: False, in order to store components that are prone to damage caused ESD, manufacturers MAKE USE of antistatic bags. These bags prevent any damage to the components that may be caused DUE to ESD.

91.

Which of the following antistatic bags are manufactured with a layer of conductive metal?(a) Shielding antistatic bags(b) Dissipative antistatic bags(c) Conductive antistatic bags(d) Grounding antistatic bagsI got this question in an interview for internship.My question is taken from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Right option is (c) Conductive antistatic BAGS

To elaborate: The conductive antistatic bags are manufactured with a layer of conductive metal. The conductive metal is often ALUMINUM ALONG with a dielectric layer of plastic covered in a static dissipative COATING.

92.

Metalized bags are more fragile than their non-metal counterparts.(a) False(b) TrueThis question was posed to me during an online interview.I'd like to ask this question from Aircraft Electronics topic in section Aircraft Electronics of Aircraft Maintenance

Answer»

Correct OPTION is (b) True

Easiest explanation: True, non-metalized bags are much more durable in COMPARISON to their METAL COUNTERPARTS. Non-metal bags also offer longer SHELF life in comparison to the metal bags, which have a much shorter shelf life.

93.

What is the color of conductive foam used for storing electronic components, prone to ESD?(a) Yellow(b) Red(c) Pink(d) BlackThis question was posed to me in an internship interview.My query is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Right choice is (d) BLACK

The EXPLANATION is: The conductive FOAM used for storing electronic components, prone to ESD is black in color. Foam also EXISTS in pink, but it is dissipative in nature.

94.

For the ESD garments to work appropriately, they must also be connected to _________(a) Electricity(b) Ground(c) Semiconductors(d) InsulatorsI have been asked this question by my school teacher while I was bunking the class.This intriguing question originated from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Correct choice is (b) Ground

Explanation: In order for ESD garments to function APPROPRIATELY, it is mandatory for the garment to have connection with the ground, i.e. ground reference. These garments may not be SUFFICIENT to prevent a person from ESD, and THUS ADDITIONAL DEVICES for ESD prevention may also be required.

95.

Which of the following will provide no ground reference?(a) Metal mat(b) Conducting mat(c) Insulating mat(d) Static matI got this question in my homework.I'm obligated to ask this question of Aircraft Electronics topic in section Aircraft Electronics of Aircraft Maintenance

Answer»

Correct choice is (c) INSULATING mat

For EXPLANATION I would say: Out of the given options, an insulating mat will offer no ground REFERENCE. In other TERMS, the mat will not have grounding and may not be safe for repairing and OVERHAUL of ESD components.

96.

What is the typical resistance of an antistatic mat, between points on the mat and to ground?(a) 10^5ohms to 10^8 ohms(b) 10^5kilo ohms to 10^8 kilo ohms(c) 10^8ohms to 10^10 ohms(d) 10^8 kilo ohms to 10^10 kilo ohmsThe question was posed to me in exam.I'm obligated to ask this question of Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer»

Correct answer is (a) 10^5ohms to 10^8 ohms

The best I can EXPLAIN: The TYPICAL resistance of an ANTISTATIC mat, between points on the mat and to GROUND is between 10^5ohms to 10^8 ohms. The antistatic mat is one of a number of antistatic devices designed to help eliminate static electricity.

97.

Which of the following materials is generally referred to as a material which possess triboelectric charging?(a) Dissipative(b) Anti-static(c) Insulative(d) ConductingI got this question during an interview.The origin of the question is Aircraft Electronics in section Aircraft Electronics of Aircraft Maintenance

Answer»

Right CHOICE is (b) Anti-static

To elaborate: Materials that POSSESS tribo electric charging MAY ALSO be referred to as anti-static materials. Such charging is done by getting the material in physical contact with ANOTHER material.

98.

The safety wrist strap is connected to the ground port by means of a ________ mega ohm resistor.(a) 50(b) 5(c) 100(d) 1The question was posed to me in semester exam.Enquiry is from Aircraft Electronics topic in chapter Aircraft Electronics of Aircraft Maintenance

Answer» CORRECT choice is (d) 1

The explanation is: The safety wrist STRAP is connected to the ground port by means of a 1 mega OHM resistor. This connection is made using a RETRACTABLE cable that is coiled along its ENTIRE length.
99.

The role of an antistatic agent is to make the surface or material slightly _________(a) Shielded(b) Dissipative(c) Conductive(d) StaticI have been asked this question during an online interview.My query is from Aircraft Electronics in division Aircraft Electronics of Aircraft Maintenance

Answer»

Correct option is (c) Conductive

The best EXPLANATION: The role of an antistatic agent is to make the SURFACE or material slightly conductive. The antistatic agent is a compound used for the treatment of materials, in order to ELIMINATE the buildup of STATIC electricity.

100.

Static charges remain in place on insulative materials for a very long time.(a) False(b) TrueThis question was posed to me by my college director while I was bunking the class.My doubt stems from Aircraft Electronics in section Aircraft Electronics of Aircraft Maintenance

Answer»

The correct ANSWER is (b) True

Explanation: True, static charges remain in place on INSULATIVE materials for a very LONG TIME. Such materials have a HIGH electrical resistance and are difficult to ground.