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TEST FAR 4

COMENTARIOS ESTADÍSTICAS RÉCORDS
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Título del Test:
TEST FAR 4

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TEST FAR 4

Fecha de Creación: 2026/09/16

Categoría: Otros

Número Preguntas: 66

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151. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) What type of magnetization is the induction of a magnetic field consisting of concentric circles of force about and within the part? This is achieved by passing electric current through the part, locating defects running approximately parallel to the axis of the part. a) Circular magnetization. b) Flux direction. c) Residual method. d) Longitudinal magnetization.

152. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) What inspection method is a method of detecting invisible cracks and other defects in ferromagnetic materials, such as iron and steel? It is not applicable to nonmagnetic materials. a) Ultrasonic inspection. b) X-ray inspection. c) Magnetic particle inspection. d) Eddy current inspection.

153. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) A primary safety function of the FAA is to require correction of unsafe conditions found in an aircraft, aircraft engine, propeller, or appliance when such conditions exist and are likely to exist or develop in other products of the same design. How do you call to this?. a) Airworthiness Directives. b) Overhaul Manual. c) Maintenance Manual. d) Manufacturers’ Service Bulletins.

154. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) When accumulations of unwashed penetrant are found on a part; what must do with the part?. a) Do eddy current inspection. b) Removal all traces of the penetrant. c) Must be completely reprocessed. d) Identify broad areas.

155. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) Because of their unique ability to penetrate material and disclose discontinuities, this inspection medium and portable unit provides a fast and reliable means for checking the integrity of airframe structures and engines. Which one?. a) Eddy current inspection. b) Radiographic inspection. c) Ultrasonic inspection. d) Magnetic particle inspection.

156. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) What type of inspection makes it possible to locate defects in all types of materials? Minute cracks, checks, and voids too small to be seen by x-ray can be located by this inspection. a) Magnetic particle inspection. b) Eddy current inspection. c) Ultrasonic inspection. d) Acoustic emission inspection.

157. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) What document does present component breakdowns of structure and equipment in disassembly sequence?. a) The aircraft maintenance manual. b) The structural repair manual. c) The schematic manual. d) The Illustrated parts catalog.

158. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) The original specification was called ATA Spec 100. Over the years, Spec 100 has been continuously revised and updated. Eventually, ATA Spec 2100 was developed for electronic documentation. How was called these two specifications evolved into one document?. a) ATA iSpec 2200. b) ATA Spec 1200. c) ATA Spec 2200. d) ATA Spec 120.

159. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) Which document describes the type design and sets forth the limitations prescribed by the applicable CFR part? It also includes any other limitations and information found necessary for type certification of a particular model aircraft. a) Code of Federal Regulations (CFRs). b) The type certificate data sheet (TCDS). c) Airworthiness Directives (ADs). d) Manufacturers’ Service Bulletins (SBs).

160. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) Where are requirements for the altimeter system tests found?. a) Capacity List. b) 14 CFR Part 43, appendix D. c) 14 CFR Part 43, appendix E. d) Operations specifications (OpSpecs).

161. (CHAPTER 10 – INSPECTION CONCEPTS AND TECHNIQUES) What document would you use to perform troubleshooting respect with a malfunctioning electrical flap system?. a) The aircraft maintenance manual. b) The aircraft wiring diagram manual. c) The structural repair manual. d) The schematic manual.

162. (CHAPTER 11 – HAND TOOLS AND MEASURING DEVICES) There are times when definite pressure must be applied to a nut or bolt as it is installed. In such cases, this tool must be used. It is a precision tool consisting of a torque indicating handle and appropriate adapter or attachments. It measures the amount of turning or twisting force applied to a nut, bolt, or screw. Which one?. a) Torque wrench. b) Strap wrench. c) Special wrench. d) Impact driver.

163. (CHAPTER 11 – HAND TOOLS AND MEASURING DEVICES) The bevel edge of the thimble is divided into 25 equal parts. Each of these parts represents one twenty-fifth of the distance the thimble travels along the barrel in moving from one of the 0.025 inch divisions to another. Thus, each division on the thimble represents…. a) One quart of an inch. b) Twenty fifth hundredth (0.25) of an inch. c) One one-thousandth (0.001) of an inch. d) One one-hundredth (0.01) of an inch.

164. (CHAPTER 11 – HAND TOOLS AND MEASURING DEVICES) In reading a micrometer, the barrel reads 0.275 inch and the thimble reads more than 0.019 inch. The number 1 graduation on the thimble is aligned exactly with the number 4 graduation on the vernier scale. Thus, the final reading is: a) 0.2944 inch. b) 0.298 inch. c) 0.2941 inch. d) 0.4654 inch.

165. (CHAPTER 11 – HAND TOOLS AND MEASURING DEVICES) The bevel edge of the thimble is divided into 25 equal parts. Each of these parts represents one twenty-fifth of the distance the thimble travels along the barrel in moving from one of the 0.025 inch divisions to another. Thus, each division on the thimble represents…. a) One quart of an inch. b) Twenty fifth hundredth (0.25) of an inch. c) One one-thousandth (0.001) of an inch. d) One one-hundredth (0.01) of an inch.

166. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What formula is used to find resistance when voltage and current are known?. a) R = I / E. b) R = A / I. c) R = E / I. d) R = I/A.

167. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) How do we call to materials that do not conduct electrical current very well or not at all, such as glass, ceramic, and plastic? Under normal conditions, atoms in these materials do not produce free electrons. a) Conductors. b) Insulators. c) Ions. d) Free electrons.

168. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) How many cells are there in a 24-volts lead-acid battery?. a) 12. b) 24. c) 18. d) N/A.

169. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What gases are released when a lead-acid battery is being charged?. a) Nitrogen and oxygen. b) Hydrogen and Nitrogen. c) Hydrogen and oxygen. d) Lead and hydrogen.

170. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) A battery with a capacity of 1 amp-hour should be able to continuously supply a current of 1 amp to a load for exactly 1 hour, or 2 amps for 1⁄2 hour, or 1⁄3 amp for 3 hours, etc., before becoming completely discharged. Actually, the ampere-hour output of a particular battery depends on…. a) Its specific gravity. b) Time during which the battery is expected to furnish current. c) The rate at which it is discharged. d) The temperature of the electrolyte must be taken into consideration.

171. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) A field of force exists around a charged body. This field is represented by lines extending in all directions from the charged body and terminating where there is an equal and opposite charge. How do we call this field?. a) Dielectric field (sometimes called an electric field). b) Field of force. c) Electrostatic field (sometimes called a dielectric field). d) Imaginary lines.

172. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What are three types of DC circuit with regard to the placement of the various circuit components?. a) Series, capacitive, and inductive. b) Series, parallel, and series-parallel. c) Parallel, resistive, and capacitive. d) Solenoid, transistor, and capacitor.

173. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What part of an amp is a milliamp?. a) 0.01 of an amp. b) 0.1 of an amp. c) 0.001 of an amp. d) 0.0001 of an amp.

174. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What electrolyte is used in Nickel-Cadmium batteries?. a) Sulfuric acid and water. b) Potassium hydroxide and distilled water. c) Potassium hydroxide and organic solvent. d) Potassium carbonate and distilled water.

175. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What is used to neutralize spilled electrolyte from a lead-acid battery?. a) Only water. b) Only Solution of bicarbonate of soda. c) Solution of bicarbonate of soda and water. d) Wash the area thoroughly with water and then apply bicarbonate of soda.

176. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What is the opposition to the flow of alternating current which inductances put in a circuit?. a) Inductance positive. b) Inductive reactance. c) Resistance. d) Capacitive reactance.

177. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) How is named to the process by which small amounts of additives called impurities are added to the semiconductor material to increase their current flow by adding a few electrons or a few holes?. a) Filtering. b) Doping. c) Biasing. d) Rectifying.

178. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What is meant by impedance?. a) The opposition to the flow in a DC circuit. b) The total opposition to the flow of alternating current. c) The opposition to the flow in a battery. d) Same that resistance.

179. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) In what units is apparent power expressed?. a) In volt-amps. b) In watts. c) In horse power. d) In Joules.

180. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) Which law of electricity is the most important for an aircraft mechanic to know?. a) Kirchhoff law. b) Ohms law. c) Farad law. d) Newton’s law.

181. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What constitutes a capacitor?. a) A coil in a circuit. b) Two conductors separated by a dielectric. c) A plate positively charged. d) A plate negatively charged.

182. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What is the purpose of a capacitor?. a) Stores electrical energy in a battery. b) Serves as a reservoir or storehouse for electricity. c) Stores electrical energy in an Inverter. d) Separate plates negatively charged.

183. (CHAPTER 12 – FUDAMENTALS OF ELECTRICITY AND ELECTRONICS) What is the basic unit of capacitance?. a) The farad. b) The Henry. c) The joule. d) The ohm.

184. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) These inspection methods can be used for measurement of material thickness in aircraft parts and structures. Which one?. a) Eddy current. b) Penetrant. c) Ultrasonic. d) Magnetic particle.

185. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) This inspection type is used to detect surface cracks, pits, subsurface cracks, corrosion on inner surfaces, and to determine alloy and heat-treat condition. Which one?. a) Ultrasonic. b) Magnetic particle. c) Eddy current. d) Dye penetrant.

186. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) What kind of inspection is used to detect the loss of metal as a result of corrosion? An estimation of material loss due to corrosion can be made by comparison with thickness standards. a) Visual. b) Eddy current. c) Ultrasonic. d) Dye penetrant.

187. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI))This inspection is a method for detecting cracks, laps, seams, voids, pits, subsurface holes, and other surface, or slightly subsurface, discontinuities in ferromagnetic materials. Which one?. a) Eddy current. b) Magnetic particle. c) Dye penetrant. d) Ultrasonic.

188. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) These are flaws where adhesive attaches to only one surface in an adhesive-bonded assembly. They can be the result of crushed, broken, or corroded cores in adhesive-bonded structures. These areas have no strength and place additional stress on the surrounding areas making failure more likely. a) Stress corrosion cracks. b) Delamination. c) Unbonds, or disbonds. d) Fatigue cracks.

189. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) The following characteristics should be considered when selecting these devices for visual inspection: foot-candle rating; explosive atmosphere rating; beam spread (adjustable, spot, or flood); efficiency (battery usage rate); brightness after extended use; and rechargeable or standard batteries. Which one?. a) Inspection mirrors. b) Flashlights. c) Simple magnifiers. d) Borescopes.

190. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) This inspection is used on nonporous metal and nonmetal components to find material discontinuities that are open to the surface and may not be evident to normal visual inspection. The part must be clean before performing a penetrant inspection. Which one?. a) Penetrant. b) Ultrasonic. c) Visual. d) Ultrasonic.

191. (CHAPTER 5. NONDESTRUCTIVE INSPECTION (NDI)) What type of cleaners are water solutions of chemicals that remove contaminants by chemical action or displacement rather than dissolving the contaminant?. a) Alkaline. b) Solvents. c) Detergents. d) Etching Chemicals.

192. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) The following precautions should be taken when using any type of blasting equipment: Which one?. a) Operators should be adequately protected with complete face and head covering equipment, and sometimes provided with pure breathing air. b) Static-ground the dry abrasive blaster and the material to be blasted. c) Titanium alloys cuttings and small shavings can ignite easily and are an extreme hazard. d) Magnesium and high-tensile-strength aluminum create sparks during dry abrasive blasting.

193. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) When required to use or handle solvents, special cleaners, paint strippers (strong alkalies and acids), etchants (corrosion removers containing acids), or surface activation material (Alodine 1200), observe the following safety precautions: Which one?. a) Avoid prolonged breathing of solvent or acid vapors. b) Never add acid to water. Always add water to acid. c) Clean water for emergency use should be available in the immediate work area after starting work. d) Equipment never should be effectively grounded where any flammable materials are being used.

194. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) What is the most common surface treatment of aluminum alloy surfaces?. a) Blasting. b) Alodizing. c) Anodizing. d) Iodizing.

195. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) This type of corrosion is one of the most destructive and intense forms of corrosion. It can occur in any metal but is most common on metals that form protective oxide films, such as aluminum and magnesium alloys. Which one?. a) Concentration cell. b) Pitting. c) Filiform. d) Fretting.

196. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) What type of corrosion is an attack on the grain boundaries of a metal? A highly magnified cross section of any commercial alloy shows the granular structure of the metal. a) Exfoliation. b) Galvanic. c) Inter-granular. d) Fatigue.

197. (CHAPTER 6 – CORROSION, INSPECTION & PROTECTION) Several standard mechanical and chemical methods are available for corrosion removal. Mechanical methods include hand sanding using abrasive mat, abrasive paper, or metal wool; and powered mechanical sanding, grinding, and buffing, using abrasive mat, grinding wheels, sanding discs, and abrasive rubber mats. What the method used depends upon?. a) The electrical flow of electrons. b) The mechanical working. c) The metal and degree of corrosion. d) The special treatment.

198 (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) In general, bolt grip lengths of a fastener is the thickness of the material the fastener is designed to hold when two or more parts are being assembled. Bolts of slightly greater grip length may be used, provided washers are placed under the nut or bolt head. How much is the maximum combined height of washers that should be used?. a) 1/8 inch. b) 1/16 inch. c) ¼ inch. d) 3/8 inch.

199. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) 1. Be sure that the torque applied is for the size of the bolt shank not the wrench size. 2. Many applications of bolts in aircraft/engines require stretch checks prior to reuse. This requirement is due primarily to bolt stretching caused by overtorquing. With respect to the statements, mark the correct answer: a) Only 1 is true. b) Only 2 is true. c) Both are true. d) Any are true.

200. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) What nuts are commonly called speed nuts? They are used with standard and sheet metal self-tapping screws in nonstructural applications. They are used to support line and conduit clamps, access doors, etc. Their use should be limited to applications where they were originally used in assembly of the aircraft. a) Wingnuts. b) Sheet spring nuts. c) Checknuts. d) Self-locking nut plates.

201. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) When installing a castle nut, start alignment with the cotter pin hole at the minimum recommended torque plus friction drag torque. Do not exceed the maximum torque plus the friction drag. What do you do if the hole and nut castellation do not align?. a) Change washer and nut and try again. b) Change washer or nut and try again. c) Change bolt or screw. d) Adjust the nut until cotter pin hole align.

202. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) These bolts are only used in applications subject to shear stress, and are often used as mechanical pins in control systems. Which one?. a) Eyebolts. b) Close tolerance shear bolts. c) Clevis bolts. d) Engine bolts.

203. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) AN standard steel bolts are marked with either a raised dash or asterisk, corrosion resistant steel is marked by a single dash, and AN aluminum-alloy bolts are marked with…. a) A recessed dash. b) Two raised asterisk. c) Two raised dashes. d) A recessed triangle.

204. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) These nuts should not be used with bolts or screws on turbine engine airplanes in locations where the loose nut, bolt, washer, or screw could fall or be drawn into the engine air intake scoop. Which one?. a) Fiber or nylon locknuts. b) Self-locking castellated nuts. c) Self-locking nuts. d) Self-locking nut plates.

205. (CHAPTER 7 – AIRCRAFT HARWARE, CONTROL CABLES, AND TURNBUCKES) 1. When installing cable system turnbuckles, it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount. 2. Turnbuckle ends are designed for providing the specified cable tension on a cable system, and a bent turnbuckle would place undesirable stress on the cable, impairing the function of the turnbuckle. With respect to the statements, mark the correct answer: a) Only 1 is true. b) Only 2 is true. c) Both are true. d) Any are true.

206. (CHAPTER 8 – CLEANING AND CORROSION CONTROL) How appear the corrosion on the surface of aluminum alloys and magnesium?. a) A reddish corrosion by product commonly referred to as rust. b) The corrosion forms a greenish film. c) It appears as pitting and etching and is often combined with a gray or white powdery deposit. d) May appear etched and pitted, depending upon the length of exposure and severity of attack.

207. (CHAPTER 8 – CLEANING AND CORROSION CONTROL) This type of corrosion is a special form of oxygen concentration cell that occurs on metal surfaces having an organic coating system. It is recognized by its characteristic worm-like trace of corrosion products beneath the paint film. Which one?. a) Pitting. b) Surface. c) Filiform. d) Concentration cell.

208. (CHAPTER 8 – CLEANING AND CORROSION CONTROL) What may be used to neutralize acid deposits in lead-acid battery compartments and to treat acid burns from chemical cleaners and inhibitors?. a) Solution of bicarbonate of soda and water. b) Wash the area thoroughly with water and then apply bicarbonate of soda. c) A mixture of boric acid and water. d) Baking soda.

209. (CHAPTER 8 – CLEANING AND CORROSION CONTROL) There are two general classifications of corrosion that cover most of the specific forms. Which are these?. a) Dissimilar attack and micro-organism attack. b) Direct chemical attack and electrochemical attack. c) Physical loads and chemical attack. d) Anodic change and cathodic change.

210. (CHAPTER 8 – CLEANING AND CORROSION CONTROL) This form of corrosion involves constant or cyclic stress acting in conjunction with a damaging chemical environment. The stress may be caused by internal or external loading. Which one?. a) Intergranular Corrosion. b) Stress-Corrosion/Cracking. c) Fatigue Corrosion. d) Galvanic Corrosion.

211. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) This device must be kept at a minimum and must be used to protect wire and cable from abrasion, chafing, exposure to fluid, and other conditions which could affect the cable insulation. Which one?. a) Metal stand-offs. b) Insulating tubing. c) Phenolic blocks. d) Rubber grommets.

212. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) What is true with respect installing batteries?. a) Remove the grounding lead first for battery removal, then the positive lead. b) Remove the positive lead first for battery removal, then the grounding lead. c) Connect the positive lead of the battery last to minimize the risk of shorting the “hot terminal” of the battery during installation. d) Connect the grounding lead of the battery first to minimize the risk of shorting the “hot terminal” of the battery during installation.

213. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) What is the process of electrically connecting conductive objects to either a conductive structure or some other conductive return path for the purpose of safely completing either a normal or fault circuit?. a) Bonding. b) Grounding. c) Grinding. d) Crimping.

214. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) The resistance of the current return path through the aircraft structure is generally considered negligible. However, this is based on the assumption that adequate bonding to the structure or a special electric current return path has been provided that is capable of carrying the required electric current with a negligible voltage drop. What must you check to determine circuit resistance?. a) The input voltage should be maintained at a constant value. b) The voltage drop across the circuit. c) The input voltage and the output voltage are same. d) The amperage should be lower.

215. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) All isolated conducting parts inside and outside the aircraft, having an area greater than 3 in2 and a linear dimension over 3 inches, that are subjected to appreciable electrostatic charging due to precipitation, fluid, or air in motion, should have a mechanically secure electrical connection to the aircraft structure of sufficient conductivity to dissipate possible static charges. How is named this procedure?. a) Metallic surface bonding. b) Static bonds. c) Grounding. d) Bonding jumpers.

216. (CHAPTER 11 – AIRCRAFT ELECTRICAL SYSTEMS) All conducting objects on the exterior of the airframe must be electrically connected to the airframe through mechanical joints, conductive hinges, or bond straps capable of conducting static charges and lightning strikes. Which one is an exception?. a) Grounds for Sensitive Circuits. b) Static bonds. c) Antenna elements. d) Single point grounds.

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