1

AC 65-28

AVIATION MECHANIC GENERAL,AIRFRAME, AND POWERPLANT

KNOWLEDGE TEST GUIDE

U.S. Department of TransportationFederal Aviation Administration

2

AVIATION MECHANIC GENERAL,AIRFRAME, AND POWERPLANT

KNOWLEDGE TEST GUIDE

1995

U.S. DEPARTMENT OF TRANSPORTATIONFEDERAL AVIATION ADMINISTRATION

Flight Standards Service

3

PREFACE

The Flight Standards Service of the Federal Aviation Administration (FAA) has developed this guide to helpapplicants meet the knowledge requirements for aviation mechanic certification.

This guide contains information about eligibility requirements, test descriptions, testing and retesting procedures,and sample test questions representative of those used in the official tests. Sample test questions and choices ofanswers are based on regulations, principles, and practices valid at the time this guide was printed. In addition,appendix 1 provides a list of reference materials and subject matter knowledge codes, and computer testingdesignees. The list of subject matter knowledge codes should be referred to when reviewing areas of deficiency onthe airman test report. Changes to the list of reference materials for all mechanic, pilot, and parachute rigger testswill be published as a separate advisory circular.

The aviation mechanic general, airframe, and powerplant test question bank; and reference and subject matterknowledge code list, with changes, may be obtained by computer modem from FedWorld at (703) 321-3339. Thisbulletin board service is provided by the U.S. Department of Commerce, 24 hours a day, 7 days per week. Fortechnical assistance regarding computer software and modem requirements for this service, contact the FedWorldhelp desk at (703) 487-4608 from 7:30 a.m. to 5 p.m. EST, Monday through Friday.

This publication may be purchased from the Superintendent of Documents, U.S. Government Printing Office,Washington, DC 20402-9325 or from U.S. Government Printing Office bookstores located in major citiesthroughout the United States.

Comments regarding this guide should be sent to:

Federal Aviation AdministrationOperations Support Branch, AFS-630Attn: Aviation Mechanic Certification ManagerP. O. Box 25082Oklahoma City, OK 73125

4

CONTENTS

Preface................................ ................................ ................................ ................................ .................. iiiContents................................ ................................ ................................ ................................ ................v

Introduction................................ ................................ ................................ ................................ ...........1Eligibility Requirements................................ ................................ ................................ .........................1Knowledge Areas on the Tests................................ ................................ ................................ ...............2Description of the Tests................................ ................................ ................................ .........................2Taking A Knowledge Test by Computer................................ ................................ ................................ .3Cheating or Other Unauthorized Conduct................................ ................................ ............................... 3Retesting Procedures................................ ................................ ................................ .............................3

Sample Test Questions and Answers:Aviation Mechanic General ................................ ................................ ................................ ...................5Aviation Mechanic Airframe ................................ ................................ ................................ .................6Aviation Mechanic Powerplant ................................ ................................ ................................ .............7

APPENDIX 1

List of Reference Materials and Subject Matter Knowledge Codes ................................ .........................1Aviation Mechanic General Abbreviations and References................................ ................................ .....1Aviation Mechanic General Examination Question References................................ ............................... 3Aviation Mechanic Airframe Abbreviations and References................................ ................................ ....6Aviation Mechanic Airframe Examination Question References................................ .............................. 9Aviation Mechanic Powerplant Abbreviations and References................................ ................................ 14Aviation Mechanic Powerplant Examination Question References................................ ..........................16Computer Testing Designees................................ ................................ ................................ ..................21

5

AVIATION MECHANIC GENERAL,AIRFRAME, AND POWERPLANT

KNOWLEDGE TEST GUIDE

INTRODUCTION

The FAA has available hundreds of computer testing centers nationwide. These testing centers offer the full rangeof airman knowledge tests. Refer to appendix 1 in this guide for a list of computer testing designees.

This knowledge test guide was developed to be used by applicants preparing to take the following knowledge testson the computer:

Aviation Mechanic GeneralAviation Mechanic AirframeAviation Mechanic Powerplant

What is required to become a skilled and effective airframe and powerplant (A & P) aviation mechanic? Althoughsome individuals possess more knowledge and skills than others, no one is born a natural aviation mechanic. Acompetent aviation mechanic becomes so through study, hard work, and experience.

This guide is not offered as a quick and easy way to obtain the necessary information for passing the knowledgetests. There is no quick and easy way to obtain the background of experience, knowledge, and skill needed to safelyand effectively maintain either vintage or modern, highly complex aircraft. Rather, the intent of this guide is todefine and narrow the field of study, as much as possible, to the required knowledge areas for obtaining an aviationmechanic certificate.

The questions on the aviation mechanic tests pertain to FAA regulations, and a wide variety of aircraft,powerplants, and systems. The information contained in the questions must never take precedence over specificinformation furnished by a manufacturer in the maintenance of an aircraft.

ELIGIBILITY REQUIREMENTS

The general qualifications for an aviation mechanic certificate require that the applicant have a combination ofexperience, knowledge, and skill. An applicant for an aviation mechanic certificate with airframe and powerplantratings should carefully review the appropriate sections of Federal Aviation Regulations (FAR) Part 65 for detailedinformation pertaining to eligibility requirements. Further information may be obtained from the nearest FAA FlightStandards District Office (FSDO).

Eligibility requirements must be met before taking the certification knowledge and practical tests. The determinationof eligibility of applicants for the general, airframe, and powerplant tests is made on the basis of one of thefollowing options:

1. Civil and/or military experience. (See FAR Part 65, Subpart A—General, and Subpart D—Mechanics.) If you believe you may be qualified to exercise this option, you must have your experience evaluatedand certified by an FAA Aviation Safety Inspector (Airworthiness). If the inspector determines that you have therequired experience, FAA Forms 8060-7, Airman's Authorization for Written Test, are issued. These forms areissued—one each for the general, airframe, and powerplant tests—and MUST be presented along with appropriateidentification to take the corresponding knowledge tests.

6

2. Graduation from an FAA-certificated Aviation Maintenance Technician School (AMTS).Depending upon the testing facility affiliation,1 a graduation certificate or certificate of completion or FAA Forms8060-7 are required, along with proper identification.

If your test is to be taken at a computer testing center and the practical testing administered by a designatedmechanic examiner (DME), and BOTH are affiliated with the AMTS, a copy of the graduation certificate orcertificate of completion (along with proper identification) may be all that you are required to present. In this case,the school, the testing center, the DME, and the local FAA FSDO will all be involved and know what authorizationis needed. On the other hand, if either one, or both the testing center and the DME are NOT affiliated with theAMTS, then FAA Forms 8060-7 are required.

KNOWLEDGE AREAS ON THE TESTS

The mechanic tests are comprehensive because they must test an applicant’s knowledge in many subject areas.

The subject areas for the tests are the same as the required AMTS curriculum subjects listed in FAR Part 147,Appendixes B, C, and D. However, the subject area titled “Unducted Fans” (in Appendix D) is not a tested subjectat this time. The terms used in FAR Part 147, Appendixes B, C, and D, are defined in FAR Part 147, Appendix A.

DESCRIPTION OF THE TESTS

All test questions are the objective, multiple-choice type with three choices of answers. Each question can beanswered by the selection of a single response. Each test question is independent of other questions, that is, acorrect response to one does not depend upon, or influence the correct response to another. The minimum passinggrade for each test is 70 percent.

The maximum time allowed for taking each test is either 1.5 or 2 hours, and is based on previous experience andeducational statistics. This amount of time is considered adequate for applicants with proper preparation andinstruction.

The aviation mechanic general test contains 50 questions, and 1.5 hours is allowed to take the test.

The aviation mechanic airframe and aviation mechanic powerplant tests each contain 100 questions, and 2 hours isallowed to take each test.

Communication between individuals through the use of words is a complicated process. In addition to being anexercise in the application and use of aeronautical knowledge, a test is also an exercise in communication since itinvolves the use of the written language. Since the tests involve written rather than spoken words, communicationbetween the test writer and the person being tested may become a difficult matter if care is not exercised by bothparties. Consequently, considerable effort is expended to write each question in a clear, precise manner. Applicantsshould carefully read the information and instructions given with the tests, as well as the statements in each testitem.

When taking a test, keep the following points in mind:

1. Answer each question in accordance with the latest regulations and procedures.

1Affiliation is a procedural arrangement to provide for graduates to take the knowledge and practical tests. The arrangementrequirements are agreed to by a particular school, testing center, and designated mechanic examiner (DME), having alsobeen approved by the supervising FAA FSDO.

7

2. Read each question carefully before looking at the possible answers. You should clearly understand theproblem before attempting to solve it.

3. After formulating an answer, determine which choice most nearly corresponds with that answer. Theanswer chosen should completely resolve the problem.

4. From the answers given, it may appear that the re is more than one possible answer. However, there isonly one answer that is correct and complete. The other answers are either incomplete, erroneous, or represent acommon misconception.

5. If a certain question is difficult for you, it is best to mark it for RECALL and proceed to the nextquestion. The recall marking procedure will be explained to you prior to starting the test. After you answer the lessdifficult questions, return to any questions you marked for recall and answer them. Although the computer shouldalert you to unanswered questions, make sure every question has an answer recorded. This procedure will enableyou to use the available time to the maximum advantage.

6. When solving a calculation problem, select the answer nearest your solution. The problem has beenchecked by various individuals and calculators; therefore, if you have solved it correctly, your answer will be closerto the correct answer than any of the other choices.

TAKING A KNOWLEDGE TEST BY COMPUTER

You should determine what authorization requirements are necessary before contacting or going to the computertesting center. Testing center personnel cannot begin the test until you provide them with the proper authorization.You must provide authorization and present identification that includes a current photograph, your signature, andactual residential address. In the case of retesting, you must present either a passed, failed or expired, test report forthat particular test. However, you should always check with the local FAA FSDO if you are not sure what kind ofauthorization to bring to the testing facility.

The next step is the actual registration process. Most computer testing centers require that all applicants contact acentral 1-800 phone number. At this time, you should select a testing site of your choice, schedule a test date, andmake financial arrangements for test payment. You may register for tests several weeks in advance of the proposedtesting date. You may cancel your appointment up to 2 business days before test time, without financial penalty.After that time, you may be subject to a cancellation fee as determined by the testing center.

You are now ready to take the test. Remember, you always have an opportunity to take a sample test before youractual test begins. Your actual test is under a time limit, but if you know the material, there should be sufficienttime to complete and review your test. Within moments of completing the test, you will receive an airman testreport, which contains your score. It also lists those subject matter knowledge areas where questions were answeredincorrectly. The total number of subject matter knowledge codes shown on the test report is not necessarily anindication of the total number of questions answered incorrectly. These codes refer to the specific subjectscovered on each of the Aviation Mechanic Knowledge Tests (General, Airframe, and Powerplant). To determine thesubject area in which a particular question was incorrectly answered, compare the subject matter code(s) on theairman test report, to the General, Airframe, or Powerplant subject matter outlines in appendix 1 of this guide. Youcan study the subject matter reference material to improve your understanding of the subject matter. The examinermay quiz you on these areas of deficiency during the practical test.

The airman test report, which must show the computer testing company's embossed seal, is an important document.DO NOT LOSE THE AIRMAN TEST REPORT as you will need to present it to the examiner prior to takingthe practical test. Loss of this report means that you will have to request a duplicate from the FAA in OklahomaCity. This will be costly and time consuming.

8

CHEATING OR OTHER UNAUTHORIZED CONDUCT

Computer testing centers are required to follow rigid testing procedures established by the FAA. This includes testsecurity. When entering the testing area, you are permitted to take only scratch paper furnished by the testadministrator and an authorized calculator, approved for use in accordance with FAA Order 8080.6, Conduct ofAirmen Knowledge Testing via the Computer Medium, and AC 60-11, Aids Authorized for Use by Airman WrittenTest Applicants. The FAA has directed testing centers to stop a test any time a test administrator suspects acheating incident has occurred. An FAA investigation will then follow. If the investigation determines that cheatingor other unauthorized conduct has occurred, any airman certificate that you hold may be revoked, and you may notbe allowed to take a test for 1 year.

RETESTING PROCEDURES

If the score on the airman test report is 70 or above, the report is valid for 24 calendar months. You may elect toretake the test in anticipation of a better score, after 30 days from the date your last test was taken. Prior toretesting, you must give your current airman test report to the computer testing administrator. Remember, the scoreof the latest test you take will become the official test score. The FAA will not consider allowing anyone to retake avalid test prior to the 30-day remedial study period.

A person who fails a knowledge test may apply for retesting before 30 days of the last test providing that personpresents the failed test report and an endorsement from an authorized mechanic certificate holder certifying thatadditional instruction has been given, and the person has been found competent to pass the test. A person mayretake a failed test after 30 days without the endorsement from an authorized certificate holder.

9

SAMPLE TEST QUESTIONS AND ANSWERS

The questions in this section are similar to some of those contained in FAA tests for mechanics. The subjectscovered here represent a sampling of the subjects covered on the actual tests.

AVIATION MECHANIC GENERAL

1. If the cross sectional area of a given conductor is increased to four times its original value, and the lengthand temperature remain constant, the resistance of the conductor will be

A—one-fourth its original value.B—four times its original value.C—found by multiplying the original resistance by the percentage increase in cross-sectional area.

Answer A—Subject Matter Code: A02; (Reference - AC 65-9A). One of the factors affecting the resistance of aconductor is cross-sectional area. Resistance varies inversely with the cross-sectional area of a conductor. If thecross-sectional area of a conductor is doubled, the resistance to current flow will be reduced by half (all otherfactors remaining unchanged).

2. When making a forward weight and balance check to determine that the center of gravity (cg) will notexceed the forward limit during extreme conditions, the items of useful load which should be computed attheir minimum weights are those located aft of the

A—forward cg limit.B—rearward cg limit.C—empty weight cg.

Answer A—Subject Matter Code: C02; (Reference - AC 65-9A). When making a forward weight and balancecheck, part of the information needed is the minimum weights of the items of useful load that are located aft ofthe forward cg limit.

3. What must a certificated mechanic with both airframe and powerplant ratings do prior to returning toservice an aircraft on which he or she has performed and approved a 100-hour inspection?

A—Present his/her work and records to a mechanic holding an Inspection Authorization for final approval andrelease.

B—Make the proper entries in the appropriate aircraft maintenance record.C—Notify the local FAA FSDO in writing of his/her intention to return the aircraft to service.

Answer B—Subject Matter Code: I02; (Reference - FAR Section 43.11(a)). The person approving for return toservice an aircraft after any inspection shall make an entry in the maintenance record containing the requiredinformation.

10

AVIATION MECHANIC AIRFRAME

1. Which of the following drill bit types work best when drilling an aramid fiber (Kevlar) compositelaminate?

A—Tool steel with standard grind.B—Diamond dust coated.C—Carbide W-Point.

Answer C—Subject Matter Code: D03; (Reference - AMR). Standard tool steels dull rapidly when drilling ortrimming composite materials. If diamond-dust coated drills are used, the fibers will grab at the drill bit and pullthe diamond from the base metal or fill voids in the dust pattern with material. The W-Point carbide drill designlasts longer and helps solve fuzz, delamination, and burn problems when drilling.

2. What is the minimum edge distance allowed for aluminum alloy single lap sheet splices containing a singlerow of rivets as compared to a joint with multiple rows, all rivets being equal in diameter?

A—The minimum edge distance for the single row is greater than that for the multiple row.B—The minimum edge distance for the single row is less than that for the multiple row.C—The minimum edge distance for the single row is equal to that for the multiple row.

Answer C—Subject Matter Code: D06; (Reference - AC 43.13-1A). The minimum edge distance is to be not lessthan two times the diameter of the rivets used for both single and multiple row single lap sheet splices.

3. What is commonly used to connect an emergency source of power, and at the same time disconnect thenormal hydraulic source from critical parts of a landing gear or wheel braking system for operation (usuallywhen the normal source system fails)?

A—Selector valve.B—Shuttle valve.C—Sequence valve.

Answer B—Subject Matter Code: K01; (Reference - AMR). The function of a shuttle valve is to provide a meansof disconnecting a normal source of hydraulic (or pneumatic) power and connecting an emergency source ofpower (hydraulic or pneumatic) to operate the critical parts of a system.

11

AVIATION MECHANIC POWERPLANT

1. If an unsupercharged reciprocating engine equipped with a constant speed propeller is operated at partthrottle and at cruising rpm, a reduction in rpm with no change in throttle setting will result in

A—no change in manifold pressure.B—an increase in manifold pressure.C—a decrease in manifold pressure.

Answer B—Subject Matter Code: A03; (Reference - EA-ITP-P2). A reduction in rpm setting (propeller pitchincrease) on an unsupercharged reciprocating engine equipped with a constant speed propeller, with no changein throttle setting, will cause an increase in manifold pressure. In this case, the decrease in rpm is caused by ahigher load being placed on the engine rather than a reduction in fuel flow into the engine.

2. What are the two main sections of a turbine engine for inspection purposes?

A—Hot and cold.B—Combustion and exhaust.C—Compressor and turbine.

Answer A—Subject Matter Code: B02; (Reference - EA-ITP-P2). For inspection purposes, the two main sectionsof a turbine engine are hot and cold. The cold section includes the compressor back through the diffuser. The hotsection includes the combustor and turbine.

3. Aluminum propeller blade failure at the site of an unrepaired nick or scratch is usually the result of

A—material defect.B—intergrannular corrosion.C—stress concentration.

Answer C—Subject Matter Code: R07; (Reference - AP). Even a small defect such as a nick or scratch causes aconcentration of stresses that may develop into a crack. The crack in turn results in even greater stressconcentration. The resulting growth of the crack will almost inevitably result in blade failure.

12

APPENDIX 1

13

LIST OF REFERENCE MATERIALSAND SUBJECT MATTER KNOWLEDGE CODES

The publications listed in the following pages contain study material you need to be familiar with when preparingfor aviation mechanic knowledge tests. All of these publications can be purchased through U.S. Governmentbookstores, commercial aviation supply houses, or industry organizations. The latest revision of the listedreferences should be requested. Additional study material is also available through these sources that may behelpful in preparing for aviation mechanic knowledge tests. All publications listed would be excellent for amechanic to have in a personal reference library.

The following abbreviations are used to identify the reference(s) associated with the subject matter.

AVIATION MECHANIC GENERAL

ABBREVIATIONS AND REFERENCES

AMT-G Aviation Maintenance Technician Series General - Aviation Supplies and Academics (ASA), Inc.ABS Aircraft Basic Science - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAP Aircraft Powerplants - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAEE Aircraft Electricity and Electronics - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAC Advisory Circular - Federal Aviation Administration (FAA), Government Printing Office (GPO)AIM Airman's Information Manual - FAA, GPOFAR Federal Aviation Regulations - FAA, GPOMBM Marathon Battery Instruction ManualEA-192-1 Electronic Circuit Devices - International Aviation Publishers, (IAP) Inc.EA-AB-1 Aircraft Batteries, Lead Acid/Nickel-Cadmium - IAP, Inc.EA-ATD-2 Aircraft Technical Dictionary - IAP, Inc.EA-ITP-G2 A & P Technician General Textbook - IAP, Inc.EA-ITP-P2 A & P Technician Powerplant Textbook - IAP, Inc.EA-MAT Advanced Mathematics - IAP, Inc.

Basic Electricity—AC 65-9A, AC 43.13-1A, AMT-G, AEE, MBM, EA-192-1, EA-AB-1, EA-ITP-G2

A01 Calculate and measure capacitance and inductanceA02 Calculate and measure electrical powerA03 Measure voltage, current, resistance, and continuityA04 Determine the relationship of voltage, current, and resistance in electrical circuitsA05 Read and interpret electrical circuit diagrams, including solid state devices and logic functionsA06 Inspect and service batteries

Aircraft Drawings—AC 65-9A, AC 43.13-1A, AC 65-15A, ABS, EA-ITP-G2

B01 Use drawings, symbols, and system schematicsB02 Draw sketches of repairs and alterationsB03 Use blueprint informationB04 Use graphs and charts

Weight and Balance—AC 65-9A, AC 43.13-1A, FAR 23.29

C01 Weigh aircraftC02 Perform complete weight-and-balance check and record data

14

Fluid Lines and Fittings—AC 65-9A, AC 43.13-1A, ABS, EA-ITP-G2

D01 Fabricate and install rigid and flexible fluid lines and fittings

Materials and Processes—AC 65-9A, AC 43-3, AC 65-15A, AC 43.13-1A, ABS, AP, EA-ATD-2, EA-ITP-P2, EA-ITP-G2

E01 Identify and select appropriate nondestructive testing methodsE02 Perform dye penetrant, eddy current, ultrasonic, and magnetic particle inspectionsE03 Perform basic heat-treating processesE04 Identify and select aircraft hardware and materialsE05 Inspect and check weldsE06 Perform precision measurements

Ground Operation and Servicing—AC 65-9A, AC 61-21A, AC 65-12A, AIM, ABS, EA-ITP-G2

F01 Start, ground operate, move, service, and secure aircraft and identify typical ground operation hazardsF02 Identify and select fuels

Cleaning and Corrosion Control—AC 65-9A, AC 65-12A, AC 43.13-1A, AC 43-4A, EA-ITP-G2

G01 Identify and select cleaning materialsG02 Inspect, identify, remove, and treat aircraft corrosion and perform aircraft cleaning

Mathematics—AC 65-9A, AC 65-12A, ABS, EA-MAT, EA-ITP-G2

H01 Extract roots and raise numbers to a given powerH02 Determine areas and volumes of various geometrical shapesH03 Solve ratio, proportion, and percentage problemsH04 Perform algebraic operations involving addition, subtraction, multiplication, and division of positive and

negative numbers

Maintenance Forms and Records—AC 65-9A, AC 65-19E, AC 43.13-1A, FAR 91.417, FAR 43

I01 Write descriptions of work performed including aircraft discrepancies and corrective actions using typicalaircraft maintenance records

I02 Complete required maintenance forms, records, and inspection reports

Basic Physics—AC 65-9A, AC 61-21A, ABS, EA-ITP-G2

J01 Use and understand the principles of simple machines; sound, fluid, and heat dynamics; basicaerodynamics; aircraft structures; and theory of flight

Maintenance Publications—AC 65-9A, AC 65-19E, FAR 21, FAR 39, FAR 43, ABS, EA-ITP-G2

K01 Demonstrate ability to read, comprehend, and apply information contained in FAA and manufacturer'saircraft maintenance specifications, data sheets, manuals, publications, and related Federal AviationRegulations, Airworthiness Directives, and Advisory material

K02 Read technical data

Mechanic Privileges and Limitations—AC 43.13-1A, FAR 43, FAR 65

L01 Exercise mechanic privileges within the limitations prescribed by FAR Part 65

15

AVIATION MECHANIC GENERAL EXAMINATION QUESTION REFERENCES

A01:1. AC 65-9A2. AEE3. EA-ITP-G24. AC 65-9A5. AC 65-9A6. AEE7. AEE8. AC 65-9A9. AEE10. AC 65-9A11. AEE12. EA-ITP-G213. EA-ITP-G214. AEEA02:15. AC 65-9A16. AC 65-9A17. AEE18. AC 65-9A19. AC 65-9A20. AC 65-9A21. AC 65-9A22. AC 65-9A23. AC 65-9A24. AC 65-9AA03:25. AC 65-9A26. AC 65-9A27. AC 65-9A28. AC 65-9A29. AC 65-9A30. AC 65-9A31. AEE32. AC 65-9A33. AC 65-9A34. AC 65-9AA04:35. EA-ITP-G236. AEE37. AEE38. AEE39. AC 65-9A40. AC 65-9A41. AC 65-9A42. AC 65-9A43. AC 65-9A44. AC 65-9A45. AC 65-9A46. AC 65-9A47. AC 65-9A48. AC 65-9A49. AC 65-9A50. AC 65-9A51. AC 65-9A52. AC 65-9A

16

53. AC 65-9A54. AC 65-9A55. AC 43.13-1AA05:56. AC 65-9A57. AC 65-9A58. AC 65-9A59. AC 65-9A60. AC 65-9A61. AC 65-9A62. AC 65-9A63. AC 65-9A64. AC 65-9A65. AC 65-9A66. AC 65-9A67. AC 65-9A68. AC 65-9A69. AC 65-9A70. AC 65-9A71. AC 65-9A72. AC 65-9A73. AC 65-9A74. AC 65-9A75. EA-192-176. EA-192-177. EA-192-178. EA-192-179. EA-192-180. EA-192-181. EA-192-182. AEE83. AEE84. AEEA06:85. AC 65-9A86. EA-ITP-G287. AC 43.13-1A88. EA-ITP-G289. EA-ITP-G290. AMT-G91. MBM92. AC 65-9A93. AC 65-9A94. EA-ITP-G295. EA-ITP-G296. AC 65-9A97. MBM98. MBM99. EA-ITP-G2100. AC 65-9A101. EA-AB-1102. EA-ITP-G2B01:103. AC 65-9A104. AC 65-9A105. AC 65-9A106. AC 65-9A107. AC 65-9A

17

108. AC 65-9A109. AC 65-9A110. AC 65-9A111. AC 65-9A112. AC 65-9AB02:113. AC 65-9A114. AC 65-9A115. AC 65-9A116. AC 65-9A117. AC 65-9A118. AC 65-9A119. AC 65-9A120. AC 65-9A121. ABS122. AC 65-9AB03:123. AC 65-9A124. AC 65-9A125. AC 65-9A126. AC 65-9A127. AC 65-9A128. AC 65-9A129. AC 65-9A130. AC 65-9A131. AC 65-9A132. AC 65-9A133. AC 65-9A134. AC 65-9A135. EA-ITP-G2136. EA-ITP-G2137. EA-ITP-G2138. EA-ITP-G2139. EA-ITP-G2140. EA-ITP-G2141. ABSB04:142. AC 65-9A143. AC 65-9A144. AC 65-9A145. AC 43.13-1A146. AC 65-9A147. AC 43.13-1A148. AC 43.13-1A149. AC 65-15A150. AC 65-15A151. AC 65-9A152. AC 65-9AC01:153. AC 65-9A154. AC 65-9A155. AC 65-9A156. AC 65-9A157. AC 65-9A158. AC 65-9A159. AC 65-9A160. AC 65-9A161. AC 65-9A

18

162. AC 65-9A163. AC 65-9A164. AC 65-9A165. AC 65-9A166. AC 65-9A167. AC 65-9A168. AC 65-9A169. AC 65-9AC02:170. AC 43.13-1A171. FAR 23.29172. AC 65-9A173. AC 65-9A174. AC 65-9A175. AC 65-9A176. FAR 23.29177. AC 65-9A178. AC 65-9A179. AC 65-9A180. AC 65-9A181. AC 65-9A182. AC 65-9A183. AC 65-9A184. AC 65-9A185. AC 43.13-1A186. AC 43.13-1A187. AC 65-9A188. AC 65-9A189. AC 65-9A190. AC 43.13-1A191. AC 65-9AD01:192. AC 65-9A193. AC 65-9A194. AC 65-9A195. ABS196. AC 65-9A197. AC 65-9A198. AC 65-9A199. AC 65-9A200. AC 65-9A201. AC 65-9A202. AC 43.13-1A203. AC 43.13-1A204. AC 65-9A205. AC 65-9A206. AC 65-9A207. AC 65-9A208. AC 65-9A209. AC 65-9A210. AC 65-9A211. EA-ITP-G2212. AC 65-9A213. AC 65-9A214. AC 65-9A215. AC 65-9A216. AC 65-9A217. AC 65-9A

19

218. AC 65-9AE01:219. AC 65-9A220. AC 65-9A221. AC 43-3222. AC 43-3223. AC 65-9A224. AC 65-9A225. EA-ITP-G2226. AC 65-9A227. AC 65-15AE02:228. AC 65-9A229. AC 65-9A230. EA-ITP-G2231. AC 65-9A232. AC 65-9A233. AC 65-9A234. AC 65-9A235. AC 65-9A236. AC 65-9A237. AC 65-9A238. AC 65-9A239. AC 43.13-1A240. AC 65-9A241. AC 65-9A242. AC 65-9A243. AC 65-9A244. AC 65-9AE03:245. AC 65-9A246. ABS247. AC 65-9A248. AC 65-9A249. ABS250. ABS251. AC 65-9A252. AC 65-9A253. ABS254. AC 65-9A255. AC 65-9AE04:256. AC 65-9A257. AC 65-15A258. AC 65-9A259. AC 65-9A260. AC 43.13-1A261. AC 65-9A262. AC 43.13-1A263. AC 65-9A264. AC 43.13-1A265. AC 43.13-1A266. AC 43.13-1A267. AC 65-9A268. AC 43.13-1A269. AC 65-9A270. AC 65-9A271. AC 65-9A

20

272. AC 43.13-1A273. AC 65-9A274. AC 65-9A275. AC 65-9A276. AC 65-9A277. AC 65-9AE05:278. AC 65-9A279. AC 65-9A280. AC 65-15A281. AC 43.13-1A282. AC 65-15A283. AC 65-15A284. AC 43.13-1A285. AC 65-15A286. AC 65-15A287. AC 65-15A288. AC 65-9AE06:289. EA-ATD-2 & AP290. AC 65-9A291. AC 65-9A292. AC 65-9A293. AC 65-9A294. AC 65-9A295. AC 65-9A296. AC 65-9A297. AC 65-9A298. AC 65-9A299. AC 65-9A300. EA-ITP-G2301. AP302. AP303. AP304. AP305. AP306. EA-ITP-P2307. APF01:308. AC 65-9A309. AC 65-9A310. AC 65-9A311. EA-ITP-G2312. AC 65-9A313. AC 65-9A314. AC 65-9A315. AC 65-9A316. AC 65-9A317. ABS & EA-ITP-G2318. AC 65-9A319. EA-ITP-G2320. EA-ITP-G2321. AC 65-9A322. AC 65-9A323. AC 65-9A324. AC 65-9A325. AC 65-9A326. ABS

21

327. AC 61-21A328. AC 61-21A329. ABS & AIM330. EA-ITP-G2331. ABS & AIM332. ABS & AIM333. AC 61-21A334. AC 61-21A & AIMF02:335. EA-ITP-G2336. AC 65-9A337. AC 65-9A338. AC 65-9A339. AC 65-9A340. AC 65-9A341. AC 65-9A342. AC 65-9A343. AC 65-9A344. AC 65-9A345. AC 65-9A346. AC 65-9AG01:347. AC 65-12A348. AC 65-12A349. AC 65-9A350. AC 65-9A351. AC 65-9A352. AC 65-9A353. AC 65-9A354. AC 65-9A355. AC 65-9AG02:356. EA-ITP-G2357. AC 43-4A358. AC 65-9A359. AC 43-4A360. AC 65-9A361. AC 65-9A362. AC 65-9A363. AC 65-9A364. AC 65-9A365. AC 43.13-1A366. AC 65-9A367. AC 65-12A368. AC 65-9A369. AC 65-9A370. AC 65-9A371. AC 65-9A372. EA-ITP-G2 & AC 43-4A373. AC 43.13-1A374. EA-ITP-G2 & AC 43-4A375. AC 43-4A376. AC 43-4A377. EA-ITP-G2378. AC 43-4AH01:379. AC 65-9A380. AC 65-9A

22

381. EA-MAT382. AC 65-9A383. AC 65-9A384. ABS385. AC 65-9A386. AC 65-9A387. AC 65-9A388. AC 65-9A389. AC 65-9A390. AC 65-9A391. AC 65-9A392. AC 65-9A393. AC 65-9AH02:394. AC 65-12A395. AC 65-9A396. AC 65-9A397. AC 65-9A398. AC 65-9A399. AC 65-9A400. AC 65-9A401. AC 65-9A402. AC 65-9A403. AC 65-9A404. AC 65-9A405. AC 65-9A406. AC 65-9A407. AC 65-9A408. AC 65-12AH03:409. AC 65-9A410. EA-ITP-G2411. AC 65-12A412. AC 65-9A413. AC 65-9A414. AC 65-9A415. AC 65-9A416. AC 65-9A417. AC 65-9A418. AC 65-9A419. AC 65-9A420. AC 65-9A421. AC 65-9A422. AC 65-9A423. AC 65-9A424. AC 65-9A425. AC 65-9A426. AC 65-9A427. AC 65-9A428. AC 65-9A429. AC 65-9A430. AC 65-9A431. AC 65-9AH04:432. AC 65-9A433. AC 65-9A434. AC 65-9A435. AC 65-9A

23

436. AC 65-9A437. AC 65-9A438. AC 65-9A439. AC 65-9A440. AC 65-9A441. AC 65-9A442. AC 65-9AI01:443. AC 65-9A444. FAR 43.9445. FAR 43.11446. AC 65-9A447. FAR 43 APP A448. AC 65-19E449. FAR 43450. AC 65-9A451. AC 43.13-1A452. AC 43.13-1A453. AC 43.13-1AI02:454. FAR 43.11455. FAR 43.3(b)456. FAR 43.9457. AC 65-9A458. FAR 43459. FAR 91.417460. FAR 43.11461. FAR 43.15(c)462. FAR 43463. FAR 43.9464. FAR 43.7J01:465. AC 65-9A466. AC 65-9A467. AC 65-9A468. AC 65-9A469. AC 65-9A470. AC 65-9A471. AC 65-9A472. EA-ITP-G2473. AC 65-9A474. ABS475. AC 65-9A476. AC 65-9A477. AC 65-9A478. AC 65-9A479. AC 65-9A480. AC 65-9A481. AC 65-9A482. EA-ITP-G2483. AC 65-9A484. AC 65-9A485. AC 65-9A486. AC 61-21A487. AC 61-21A488. AC 61-21A489. AC 61-21A490. AC 61-21A

24

491. AC 61-21AK01:492. FAR 39493. FAR 21494. FAR 39495. AC 65-9A496. EA-ITP-G2497. FAR 21.179498. FAR 21499. FAR 21500. EA-ITP-G2501. EA-ITP-G2502. FAR 43.11(b)503. EA-ITP-G2504. FAR 43.13505. FAR 23.1543506. FAR 39.1507. AC 65-19E508. AC 65-19E509. AC 65-19E510. AC 65-9A511. ABS512. ABS513. ABS514. FAR 43 APP AK02:515. FAR 39516. FAR 23.1545517. FAR 43.13518. FAR 43.13L01:519. FAR 65.7520. FAR 43521. FAR 43522. FAR 43523. FAR 65.7524. FAR 65.1525. FAR 65.1526. FAR 65.1(a)527. FAR 43 APP A528. FAR 65.1529. FAR 65.7530. FAR 65531. FAR 65.3532. FAR 65.1533. FAR 43.13(6)534. AC 43.13-1A535. FAR 43536. FAR 65.7537. AC 43.13-1A

25

AVIATION MECHANIC AIRFRAME

ABBREVIATIONS AND REFERENCES

AC Advisory CircularAEE Aircraft Electricity and Electronics - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAMR Aircraft Maintenance and Repair - Glencoe Division, Macmillan/McGraw-Hill Publishing CompanyAP Aircraft Powerplants - Glencoe Division, Macmillan/McGraw-Hill Publishing CompanyDAT Dictionary of Aeronautical Terms - Aviation Supplies and Academics (ASA) PublicationsEA-AAC-1 Aircraft Air-conditioning (Vapor Cycle) - International Aviation Publishers (IAP), Inc.EA-FMS Aircraft Fuel Metering Systems - IAP, Inc.EA-AH-1 Aircraft Hydraulic System - IAP, Inc.EA-AIS Aircraft Instrument Systems - IAP, Inc.EA-AOS-1 Aircraft Oxygen System - Aviation Maintenance Publishers (AMP) 1975EA-ITP-A2 A & P Technician Airframe Textbook - IAP, Inc.EA-ITP-G2 A & P Technician General Textbook - IAP, Inc.EA-NMR Aircraft Bonded Structure - IAP, Inc.EA-WB-1 Welding Guidelines with Aircraft Supplement - IAP, Inc.EA-356 Aircraft Radio Systems - IAP, Inc.EA-358 Advanced Composites - IAP, Inc.FAR Federal Aviation RegulationsMBM Marathon Battery ManualMMM Manufacturer's Maintenance ManualTSO Technical Standard Order

Wood Structures—AC 65-15A, AC 43.13-1A, AMR

A01 Service and repair wood structuresA02 Identify wood defectsA03 Inspect wood structures

Aircraft Covering — AC 65-15A, AC 43.13-1A, AMR

B01 Select and apply fabric and fiberglass covering materialsB02 Inspect, test, and repair fabric and fiberglass

Aircraft Finishes—AC 65-15A, AC 43.13-1A, AMR, DAT, EA-ITP-A2

C01 Apply trim, letters, and touchup paintC02 Identify and select aircraft finishing materialsC03 Apply finishing materialsC04 Inspect finishes and identify defects

Sheet Metal and Non-Metallic Structures—AC 65-9A, AC 65-15A, AC 43.13-1A, FAR 23, TSO, AMR, EA-358, EA-NMR, EA-ITP-G2, EA-ITP-A2

D01 Select, install, and remove special fasteners for metallic, bonded, and composite structuresD02 Inspect bonded structuresD03 Inspect, test, and repair fiberglass, plastics, honeycomb, composite, and laminated primary and secondary

structuresD04 Inspect, check, service, and repair windows, doors, and interior furnishingsD05 Inspect and repair sheet-metal structures

26

D06 Install conventional rivetsD07 Form, lay out, and bend sheet metal

Welding—AC 65-15A, AC 43.13-1A, AMR, EA-WB-1, EA-ITP-A2

E01 Weld magnesium and titaniumE02 Solder stainless steelE03 Fabricate tubular structuresE04 Solder, braze, gas-, and arc-weld steelE05 Weld aluminum and stainless steel

Assembly and Rigging—AC 65-9A, AC 65-15A, AC 61-13B, AC 43.13-1A &2A, FAR 23, AMR, EA-ITP-A2

F01 Rig rotary-wing aircraftF02 Rig fixed-wing aircraftF03 Check alignment of structuresF04 Assemble aircraft components, including flight control surfacesF05 Balance, rig, and inspect movable primary and secondary flight control surfacesF06 Jack aircraft

Airframe Inspection—AC 65-9A, FAR 43, FAR 65, FAR 91

G01 Perform airframe conformity and airworthiness inspectionsHXX ReservedIXX ReservedJXX Reserved

Aircraft Landing Gear Systems—AC 65-9A, AC 65-15A, AC 43.13-1A, FAR 43, AMR, EA-AH-1, EA-ITP-A2

K01 Inspect, check, service, and repair landing gear, retraction systems, shock struts, brakes, wheels, tires, andsteering systems

Hydraulic and Pneumatic Power Systems—AC 65-9A, AC 65-15A, AC 43.13-1A, AMR, EA-AH-1, EA-ITP-A2

L01 Repair hydraulic and pneumatic power system componentsL02 Identify and select hydraulic fluidsL03 Inspect, check, service, troubleshoot, and repair hydraulic and pneumatic power systems

Cabin Atmosphere Control Systems—AC 65-15A, AC 43.13-1A, AMR, EA-AAC-1, EA-ITP-A2

M01 Inspect, check, service, troubleshoot, and repair heating, cooling, air-conditioning, pressurization, and aircycle machines

M02 Inspect, check, troubleshoot, service, and repair oxygen systems

Aircraft Instrument Systems—AC 65-9A, AC 65-15A, FAR 23, FAR 65, FAR 91, AEE, AMR, DAT, EA-AIS, EA-ITP-A2

N01 Inspect, check, service, troubleshoot, and repair electronic flight instrument systems and both mechanicaland electrical heading, speed, altitude, temperature, pressure, and position indicating systems to include theuse of built-in test equipment

N02 Install instruments and perform a static pressure system leak test

27

Communication and Navigation Systems—AC 65-15A, AC 91-44A, AC 43.13-2A, AEE, AP, EA-356, EA-ITP-A2

O01 Inspect, check, and troubleshoot autopilot, servos and approach coupling systemsO02 Inspect, check, and service aircraft electronic communication and navigation systems, including VHF,

passenger address interphones and static discharge devices, aircraft VOR, ILS, LORAN, radar beacontransponders, flight management computers, and GPWS

O03 Inspect and repair antenna and electronic equipment installations

Aircraft Fuel Systems—AC 65-9A, AC 65-12A, AC 65-15A, AC 43.13-1A & 2A, FAR 23, FAR 25, AMR,MMM, EA-FMS, EA-ITP-G2, EA-ITP-A2

P01 Check and service fuel dump systemsP02 Perform fuel management, transfer, and defuelingP03 Inspect, check, and repair pressure fueling systemsP04 Repair aircraft fuel system componentsP05 Inspect and repair fluid quantity indicating systemsP06 Troubleshoot, service, and repair fluid pressure and temperature warning systemsP07 Inspect, check, service, troubleshoot, and repair aircraft fuel systems

Aircraft Electrical Systems—AC 65-9A, AC 65-15A, AC 43.13-1A & 2A, FAR 23, AEE, MBM, EA-ITP-G2,EA-ITP-A2

Q01 Repair and inspect aircraft electrical system components; crimp and splice wiring to manufacturer'sspecifications; and repair pins and sockets of aircraft connectors

Q02 Install, check, and service airframe electrical wiring, controls, switches, indicators, and protective devicesQ03 Inspect, check, troubleshoot, service, and repair alternating and direct current electrical systemsQ04 Inspect, check, and troubleshoot constant speed and integrated speed drive generators

Position and Warning Systems—AC 65-9A, AC 65-15A, AC 43.13-1A, FAR 23, AMR, EA-AIS, EA-ITP-A2

R01 Inspect, check, and service speed and configuration warning systems, electrical brake controls, and antiskidsystems

R02 Inspect, check, troubleshoot, and service landing gear position indicating and warning systems

Ice and Rain Control Systems—AC 65-15A. AC 43.13-1A

S01 Inspect, check, troubleshoot, service, and repair airframe ice and rain control systems

Fire Protection Systems—AC 65-9A, AC 65-15A, AP, EA-ITP-A2

T01 Inspect, check, and service smoke and carbon monoxide detection systemsT02 Inspect, check, service, troubleshoot, and repair aircraft fire detection and extinguishing systems

28

AVIATION MECHANIC AIRFRAME EXAMINATION QUESTION REFERENCES

A01-A03:1. AMR2. AC 43.13-1A3. AC 43.13-1A4. AC 43.13-1A5. AC 43.13-1A6. AC 43.13-1A7. AC 43.13-1A8. AC 65-15A9. AC 43.13-1A10. AC 65-15A11. AC 65-15A12. AC 65-15A13. AMR14. AC 43.13-1AB01-B02:15. AC 43.13-1A16. AC 65-15A17. AC 43.13-1A18. AC 43.13-1A19. AC 65-15A20. AC 65-15A21. AMR22. AMR23. AC 65-15A24. AC 43.13-1A25. AC 43.13-1AC01-C04:26. AMR27. EA-ITP-A228. DAT29. AMR30. EA-ITP-A231. AMR32. AC 65-15A33. EA-ITP-A234. EA-ITP-A235. AC 43.13-1A36. AC 65-15A37. EA-ITP-A238. AC 65-15A39. AMR40. AC 65-15AD01:41. AC 65-15A42. EA-ITP-A243. AC 65-9A44. AC 65-15A45. AC 65-15A46. EA-ITP-A247. AC 65-9A48. AC 65-9A49. AC 65-9A50. EA-ITP-A251. AMR52. EA-ITP-A253. EA-ITP-A2D02:54. AC 65-15A55. AMR

29

56. AMR57. EA-NMR58. EA-NMR59. EA-ITP-A260. AMR61. EA-NMR62. EA-NMR63. AMR64. AC 43.13-1AD03:65. EA-ITP-A266. EA-ITP-A267. EA-ITP-A268. AC 65-15A69. AC 43.13-1A70. EA-ITP-A271. AC 65-15A72. EA-ITP-A273. EA-ITP-A274. EA-ITP-A275. EA-ITP-A276. EA-ITP-A277. EA-ITP-A278. EA-NMR79. EA-NMR80. EA-35881. AC 43.13-1A82. AC 43.13-1A83. AC 43.13-1A84. EA-35885. EA-ITP-A286. EA-ITP-A287. EA-ITP-A288. EA-ITP-A289. EA-ITP-A2D04:90. AC 65-15A91. AC 43.13-1A92. TSO93. AC 65-15A94. AC 65-15A95. AC 65-15A96. FAR 23.85397. AC 65-15A98. AC 65-15AD05:99. AC 65-15A

100. AC 65-9A & EA-ITP-G2101. AC 43.13-1A102. AC 65-15A103. AC 65-15A104. AC 65-9A105. AC 65-15A106. AC 65-15A107. AC 65-15A108. AC 43.13-1A109. AC 65-15A110. AC 65-15A111. AC 43.13-1A112. AC 65-9A113. AC 65-15A114. AC 65-15A

30

115. AC 65-9A116. AC 43.13-1A117. AMR118. AC 65-9A119. AC 65-15A120. AMR121. AC 65-15A122. AC 65-9A123. AC 65-15A124. AC 65-15A125. AC 65-15A126. AMR127. AC 65-15A128. AC 65-15A129. EA-ITP-G2D06:130. AC 65-9A131. AC 65-9A132. AC 43.13-1A133. AMR134. AC 65-9A135. AC 43.13-1A136. EA-ITP-G2137. AC 65-9A138. AC 65-9A139. AC 65-9A140. AC 43.13-1A141. AC 65-9A142. AC 65-9A143. AC 43.13-1A144. AC 65-15A145. AC 65-9A146. AC 43.13-1A147. AC 65-9A148. AC 43.13-1A149. AC 65-9A150. AC 65-15A151. AMR152. AC 65-15A153. AC 65-15A154. AC 65-9A155. AC 65-9A156. AC 65-15AD07:157. AC 65-15A158. AC 65-15A159. AC 65-15A160. AC 65-15A161. AC 65-15A162. AC 65-15A163. AC 65-15A164. AC 65-15A165. AC 65-15A166. AC 65-15A167. AC 65-15A168. AC 65-15A169. AC 65-15A170. AC 65-9A171. AC 65-15A172. AC 65-15A173. AC 65-15A174. AC 65-15A

31

175. AMR176. AC 65-15A177. AC 65-15A178. AC 65-9AE01-E03:179. EA-ITP-A2180. AC 65-15A181. AC 65-15A182. AC 65-15A183. AC 65-15A184. AC 65-15A185. AC 43.13-1AE04:186. AC 43.13-1A187. AC 65-15A188. AC 65-15A189. AMR190. AC 65-15A191. AC 65-15A192. AC 43.13-1A & EA-ITP-A2193. AMR194. AC 65-15A195. AMR196. AC 65-15A197. AC 65-15A198. AC 65-15AE05:199. AC 65-15A200. AC 65-15A201. AC 65-15A202. AC 65-15A203. AC 65-15A204. AC 65-15A205. AC 65-15A206. AC 65-15A207. AC 65-15A208. AC 43.13-1A209. AC 65-15A210. AC 65-15A211. AMR & EA-WB-1F01:212. AC 65-15A213. AC 65-15A214. AC 65-15A215. AC 43.13-2A216. AC 65-15A217. AC 65-15A218. AC 65-15A219. AC 65-15A220. AC 65-15A221. AC 65-15A222. AC 61-13B223. AC 61-13B224. AC 61-13B225. AC 65-15A226. AC 65-15AF02:227. AC 65-15A228. AC 43.13-1A229. EA-ITP-A2230. AC 65-15A231. AC 65-15A

32

232. AC 65-15A233. AC 65-15A234. AC 65-15A235. AC 65-15A236. AC 65-15A237. AC 65-15A238. AC 65-15A239. AC 65-15A240. AC 65-15A241. AC 65-15A242. AC 65-15A243. AC 65-15A244. AC 65-15A245. AC 65-15A246. AC 65-15A247. AC 65-15A248. AC 65-15A249. AC 65-15A250. AC 65-15AF03-F04:251. AC 65-15A252. AC 65-15A253. AC 65-15A254. AC 65-15A255. AC 65-15A256. AC 65-15A257. AC 43.13-1A258. AC 43.13-1A259. AC 43.13-1A260. AC 43.13-1A261. AC 43.13-1A262. AC 65-9A263. AC 43.13-1A264. AC 65-15AF05:265. AC 65-15A266. FAR 23.69(a)(1)267. AC 65-15A268. EA-ITP-A2269. AC 65-15A270. AC 65-15A271. AC 43.13-1A272. AC 43.13-1A273. AC 43.13-1A274. AC 65-15A275. AC 65-9A276. AC 65-15A277. FAR 23.677(a)278. AC 65-15A279. AC 65-15A280. AC 65-15A281. AC 65-15A282. AC 65-15A283. AC 65-15A284. AMR285. AC 65-15A286. AC 65-15A287. AC 65-9A288. AC 65-15A289. AC 65-15A290. AC 65-15AF06-G01:

33

291. AC 65-9A292. AC 65-9A293. AC 65-9A294. AC 65-9A295. FAR 43.7296. FAR 43297. FAR 91.409298. FAR 43.11299. FAR 91.409300. FAR 43.7(b)301. FAR 91.409302. FAR 65303. FAR 91.409304. FAR 91.409K01:305. AMR & AC 65-9A306. AC 65-15A307. AC 65-15A308. AC 65-15A309. AC 65-15A310. AC 65-15A311. AC 43.13-1A312. AC 65-15A313. AC 65-15A & EA-ITP-A2314. AC 65-15A315. AMR316. AC 65-15A317. AC 65-15A318. AC 65-15A319. AC 43.13-1A320. AC 65-15A321. AC 65-15A322. AC 65-15A323. AC 65-15A324. EA-ITP-A2325. AC 65-15A326. AC 65-15A327. AC 43.13-1A328. AC 65-15A329. AC 65-15A330. FAR 43.3 & APP A331. AC 65-15A332. AC 65-15A333. AC 65-15A334. AC 65-15A335. AC 65-15A336. AMR337. AC 65-15A338. AC 65-15A339. AC 65-15A340. AC 65-15A341. AC 65-15A342. AC 65-15A343. AC 65-15A344. EA-ITP-A2345. AC 65-15A346. AC 65-15A347. AC 65-15A348. AC 65-15A349. AC 65-15A350. AC-65-15A351. AC 43.13-1A

34

352. AC 65-15A353. AC 65-15A354. AC 65-15A355. AC 65-15A356. AC 65-15A357. AC 65-15A358. AC 65-15A359. AC 65-15A360. EA-ITP-A2361. AC 65-15A362. AC 65-15A363. AC 65-15A364. AC 65-15A365. AC 65-15A366. AC 65-15A367. AC 65-15A368. AC 65-15A369. AMR370. AC 65-15A371. AMR372. AC 65-15A373. AC 65-9A374. EA-AH-1375. AC 65-15A376. AC 65-15A377. EA-AH-1378. EA-AH-1379. EA-AH-1380. EA-AH-1381. AMR382. EA-ITP-A2383. AC 65-15A384. AC 65-9A385. AC 65-9AL01:386. AC 43.13-1A387. AC 65-9A388. AC 65-15A389. AC 65-15A390. AC 65-15A391. AC 65-15A392. AC 65-15A393. AC 65-15A394. AC 65-15A395. AC 65-15A396. EA-ITP-A2397. AC 65-15A398. AC 65-15A399. AC 65-15A400. AC 65-15A401. AC 65-15A402. AC 65-9A403. AC 65-15A404. AC 65-9A405. AC 65-9A406. EA-ITP-A2407. EA-AH-1408. AMR409. AC 65-9A410. EA-ITP-A2L02:411. EA-ITP-A2

35

412. AC 65-15A413. AC 65-15A414. AC 65-15A415. AC 65-15A416. AC 65-15A417. EA-ITP-A2418. AC 65-15A419. AC 65-15A420. AC 65-15A421. AC 65-15A422. AC 65-15A423. AC 65-15A424. AC 65-15A425. AC 65-15A426. AC 65-15A427. EA-AH-1428. EA-AH-1429. EA-AH-1430. EA-ITP-A2431. AC 65-15AL03:432. AC 65-15A433. EA-ITP-A2434. AMR435. AC 65-15A436. AC 65-15A437. AMR438. AC 65-15A439. AC 65-15A440. AMR441. AC 65-15A442. AC 65-15A443. AC 65-15A444. AC 65-15A445. AC 65-9A446. AC 65-9A447. AC 65-9A448. AMR449. AC 65-15A450. AC 65-15A451. AC 65-15A452. AC 65-15A453. AC 65-15A454. AMR455. AC 65-15A456. AC 65-15A457. AC 65-15A458. AC 65-15A459. AC 65-15A460. AC 65-15A461. AC 65-15A462. AC 65-15A463. AMR464. AC 65-15A465. AC 65-15A466. AC 65-15A467. AC 65-15A468. AC 65-15A469. AMR470. AC 65-15A471. EA-ITP-A2472. AC 65-15A

36

473. AC 65-15A474. AC 65-15A475. AMR476. AC 65-15A477. AC 65-15A478. AC 65-15A479. AC 65-15A480. AC 65-15A481. AC 65-9A482. AC 65-15A483. AC 65-15A484. AC 65-15A485. AC 65-15A486. AC 65-15A487. AC 65-15A488. AC 65-15A489. AC 65-15A490. AC 65-15A491. AC 65-15A492. AMR493. EA-AH-1494. EA-AH-1495. AC 43.13-1A496. AC 65-15AM01:497. AC 65-15A498. AC 65-15A499. AC 65-15A500. AC 65-15A501. AC 65-15A502. AC 65-15A503. EA-ITP-A2504. AC 65-15A505. AC 65-15A506. AC 65-15A507. EA-AAC-1508. EA-AAC-1509. EA-AAC-1510. AC 65-15A511. EA-AAC-1512. AC 43.13-1A513. AC 43.13-1A514. AC 43.13-1A515. EA-ITP-A2516. AC 65-15A517. AC 65-15A518. AC 65-15A519. AC 65-15A520. AC 65-15A521. AC 65-15A522. AC 65-15A523. AC 65-15A524. AC 65-15A525. AC 65-15A526. AC 65-15A527. AC 65-15A528. AC 65-15A529. AC 65-15A530. AC 65-15A531. AC 65-15A532. AC 65-15A533. AC 65-15A

37

534. AC 65-15A535. AC 65-15A536. AC 65-15A537. AMR538. AMR539. AC 65-15A540. AC 65-15A541. AC 65-15A542. AC 65-15A543. AC 65-15A544. AC 65-15A545. AC 65-15A546. AC 65-15A547. AC 65-15A548. AC 65-15A549. AC 65-15A550. EA-AAC-1551. EA-AAC-1552. EA-AAC-1553. EA-ITP-A2554. EA-AAC-1555. EA-AAC-1556. EA-AAC-1557. EA-AAC-1558. EA-ITP-A2559. EA-AAC-1560. AC 65-15A561. EA-ITP-A2562. EA-ITP-A2563. EA-ITP-A2M02:564. AC 65-15A565. AC 65-15A566. AC 65-15A567. AC 65-15A568. AC 65-15A569. AC 65-15A570. AC 65-15A571. AC 65-15A572. AC 65-15A573. AC 65-15A574. AC 65-15A575. AC 65-15A576. AC 65-15A577. AC 65-15A578. AC 65-15A579. EA-ITP-A2580. EA-ITP-A2581. AC 65-15A582. EA-ITP-A2 & EA-AOS-1583. EA-ITP-A2584. EA-ITP-A2585. AC 65-15AN01:586. AC 65-15A587. AC 65-15A588. AC 65-15A589. AC 65-15A & FAR 23590. AC 65-15A591. AC 65-15A592. FAR 23.1327593. AC 65-15A

38

594. AC 65-15A595. FAR 23.1325596. AC 65-15A597. AC 65-9A598. FAR 65.1599. FAR 65.1600. AC 65-15A601. DAT602. AC 65-15A603. AC 65-15A604. AC 65-15A605. AC 65-15A606. AC 65-15A607. AC 65-15A608. AC 65-15A609. AC 65-15A610. AC 65-15A611. AC 65-15A612. FAR 91.411613. AC 65-15A614. AEE615. AEE616. AEE617. EA-ITP-A2618. AEE619. AEE620. AEE621. AMRN02:622. AC 65-15A623. AC 65-15A624. AC 65-15A625. AC 65-15A626. FAR 23.1545627. AC 65-15A628. AC 65-15A629. AC 65-15A630. AC 65-15A631. AC 65-15A632. AC 65-15A633. AC 65-15A634. AC 65-15A635. AC 65-15A636. AC 65-15A637. FAR 65.1638. AC 65-15A639. FAR 65.1(a)640. AC 65-15A641. AC 65-15A642. EA-AIS643. AC 65-15A644. EA-ITP-A2645. EA-ITP-A2646. EA-ITP-A2O01:647. AC 65-15A648. AC 65-15A649. AC 65-15A650. AC 65-15A651. AEE652. EA-ITP-A2653. AC 65-15A

39

654. AC 65-15A655. AC 65-15A656. AP657. AEE658. AEE659. EA-ITP-A2660. AC 65-15AO02:661. AC 65-15A662. AC 43.13-2A663. AC 65-15A664. AC 65-15A665. AC 65-15A666. AC 65-15A667. AC 65-15A668. AC 65-15A669. EA-ITP-A2670. AC 91-44A671. AC 65-15A672. AC 65-15A673. EA-ITP-A2674. EA-ITP-A2675. EA-356676. AEE677. AEE678. AEE679. AEEO03:680. AC 43.13-2A681. AC 65-15A682. AC 65-9A683. AC 65-15A684. AC 43.13-2A685. AC 65-15A686. AC 43.13-2A687. AC 65-15A688. AC 43.13-2A689. AC 43.13-2A690. AC 65-15A691. AC 65-15A692. AC 65-15A693. AC 65-15A694. AC 65-15A695. AC 65-15A696. AC 43.13-2A697. AC 65-15AP01-P03:698. AC 65-9A699. AMR700. FAR 23.1001701. AC 65-9A702. AC 65-9A703. EA-ITP-A2704. EA-ITP-A2705. MMM706. AC 65-9A707. AC 65-9A708. AC 65-9A709. AC 65-9A710. AC 65-9A711. AC 43.13-1A712. AC 65-9A

40

713. AC 65-9A714. AC 65-9A715. AC 65-9A716. AC 65-9A717. AC 65-9AP04:718. AC 65-9A719. AC 65-9A720. AC 65-9A721. FAR 23.965(a)(1)722. AC 65-9A723. AC 65-9A724. AC 65-9A725. AC 43.13-1A726. AC 65-9A727. AC 65-9A728. EA-FMS729. AC 43.13-1A730. EA-ITP-A2731. EA-FMS732. AC 43.13-1A733. AC 43.13-1A734. AC 43.13-1A735. EA-ITP-G2736. AC 43.13-1AP05:737. AC 65-9A738. AC 65-9A739. AC 65-9A740. AC 65-9A741. AC 65-9A742. AC 65-9A743. AC 65-15A744. AC 65-9A745. AC 65-9A746. AC 65-9A747. EA-ITP-A2748. AC 65-9A749. AC 65-9A750. AC 65-9A751. AC 65-9A752. AC 65-9A753. AC 65-9A754. AC 65-9A755. EA-ITP-A2756. FAR 23.1337P06:757. AC 65-9A758. AC 65-9A759. AC 65-9A760. AC 65-9A761. AC 65-9A762. AC 65-9A763. AC 65-9A764. AC 65-9A765. AC 65-9A766. AC 65-9A767. AC 65-9A768. AC 65-9A769. AC 65-12A770. AC 65-12A771. AC 65-12A

41

772. AC 65-9A773. AC 65-9AP07:774. AC 65-9A775. AC 65-9A776. AC 65-9A777. AC 43.13-2A778. AC 65-9A779. FAR 23.951(b)780. AC 65-9A781. FAR 25.1557782. AC 65-9A783. AC 65-9A784. AC 65-9A785. AC 65-9A786. AC 65-9A787. FAR 23.1557788. AC 65-9A789. AC 65-9A790. AC 65-9A791. AC 65-9A792. AC 43.13-1A793. AC 65-9A794. AC 65-9A795. AC 65-9A796. AC 65-9A797. AC 65-9A798. AC 65-9A799. AC 43.13-1A800. AC 65-9A801. EA-ITP-A2802. AC 65-9AQ01:803. AC 65-9A804. AEE805. AEE806. AC 65-9A807. AC 65-9A808. AC 65-9A809. AC 65-9A810. AC 65-9A811. AC 65-9A812. AC 65-9A813. AC 65-9A814. AC 65-9A815. AC 65-9A816. AC 65-9A817. AC 65-9A818. AC 65-9A819. AC 65-9A820. AEE821. AC 65-15A822. AC 65-9A823. AC 65-9A824. AC 65-9A825. AEE826. FAR 23.135827. AC 65-9A828. AC 65-9A829. AC 65-9A830. EA-ITP-G2831. AEE

42

832. EA-ITP-G2833. EA-ITP-G2834. EA-ITP-G2835. EA-ITP-G2836. MBM837. EA-ITP-G2838. AC 65-9A839. AC 65-9A840. AC 65-9A841. AC 65-15A842. AC 65-15A843. AC 43.13-1A844. AC 43.13-1A845. AC 43.13-1A846. AEE847. AEE848. EA-ITP-A2849. AC 65-9AQ02:850. AC 65-15A851. AC 65-15A852. AC 65-15A853. AC 65-9A854. AC 65-9A855. EA-ITP-A2856. AC 65-9A857. AC 43.13-1A858. AC 43.13-1A859. AC 43.13-1A860. AC 65-15A861. AC 65-15A862. AC 65-9A863. AC 43.13-1A864. AC 43.13-1A865. AC 43.13-1A866. AC 43.13-1A867. AC 65-15A868. AC 65-15A869. AC 65-9A870. AC 65-15A871. AC 43.13-1A872. AC 43.13-1A873. AC 43.13-1A874. AC 43.13-1A875. AC 65-9A876. AC 65-15A877. AC 65-9A878. AC 43.13-1A879. AC 65-15A880. AC 65-9A881. AC 43.13-1A882. AC 43.13-1A883. AC 43.13-1A884. AC 65-15A885. AC 43.13-1A886. AC 65-9A887. AC 43.13-1A888. AC 65-15A889. AC 65-9A890. AC 65-15A891. AC 65-9A892. AC 65-9A

43

Q03:893. AC 65-9A894. AEE895. AC 65-9A896. AC 65-9A897. AEE898. AC 65-9A899. AC 65-9A900. AC 43.13-2A901. AC 65-9A902. AC 65-9A903. AC 65-9A904. AC 65-9A905. AC 65-9A906. AC 65-9A907. AC 43.13-1A908. AC 65-9A909. AEE910. AC 65-9A911. AC 65-9A912. AC 65-9A913. AC 43.13-2A914. AC 65-9A915. AC 65-9A916. AC 65-9A917. AC 65-9A918. AC 65-9A919. AC 65-9A920. AC 65-9A921. AC 65-9A922. AC 65-9A923. AC 65-9A924. AC 65-9A925. AC 65-9A926. AC 65-15A927. AC 65-9AQ04:928. AEE929. AEE930. AEE931. EA-ITP-A2932. AEE933. EA-ITP-A2R01:934. AC 65-15A935. AC 65-15A936. AC 65-15A937. AC 65-15A938. AMR939. AC 65-15A940. FAR 23.1323941. AC 65-15A942. EA-ITP-A2943. AC 65-15A944. AC 65-15A945. AC 65-15A946. AC 65-15A947. AC 65-15A948. AMR949. AMR950. AMRR02:

44

951. AC 65-15A952. AC 65-15A953. AC 65-15A954. AC 65-15A955. AC 65-15A956. AC 65-15A957. AC 43.13-1A958. AC 65-15A959. AC 65-15A960. AC 65-15A961. AC 65-15A962. AC 65-15A963. EA-AIS964. EA-AIS965. EA-AIS966. AC 65-9A967. AC 65-15A968. AC 65-15AS01:969. AC 65-15A970. AC 65-15A971. AC 43.13-1A972. AC 65-15A973. AC 65-15A974. AC 65-15A975. AC 65-15A976. AC 65-15A977. AC 65-15A978. AC 65-15A979. AC 65-15A980. AC 65-15A981. AC 65-15A982. AC 65-15A983. AC 65-15A984. AC 65-15A985. AC 65-15A986. AC 65-15A987. AC 65-15A988. AC 65-15A989. AC 65-15A990. AC 65-15A991. AC 65-15A992. AC 65-15A993. AC 65-15A994. AC 65-15A995. AC 65-15A996. AC 65-15AT01:997. AC 65-15A998. AC 65-15A999. AC 65-15A1000. AC 65-15A1001. AC 65-15A1002. AC 65-15A1003. AC 65-15A1004. AC 65-15A1005. AC 65-15A1006. AC 65-9A1007. AC 65-15A1008. AC 65-15A1009. AC 65-15AT02:

45

1010. AC 65-15A1011. AC 65-15A1012. AC 65-15A1013. AC 65-15A1014. AC 65-15A1015. AC 65-15A1016. EA-ITP-A21017. AP1018. AC 65-15A1019. AC 65-15A1020. AC 65-15A1021. AC 65-15A1022. AC 65-15A1023. AC 65-15A1024. AC 65-15A1025. AC 65-15A1026. AC 65-15A1027. AC 65-15A1028. AC 65-15A

46

AVIATION MECHANIC POWERPLANT

ABBREVIATIONS AND REFERENCES

ABS Aircraft Basic Science - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAC Advisory CircularAEE Aircraft Electricity and Electronics - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAMR Aircraft Maintenance and Repair - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyAP Aircraft Powerplants - Glencoe Division, Macmillan/McGraw-Hill Publication CompanyDAT Dictionary of Aeronautical Terms - Aviation Supplies & Academics (ASA), Inc.EA-363 Transport Category Aircraft Systems - IAP, Inc.EA-APC Aircraft Propellers and Controls - International Aviation Publishers (IAP), Inc.EA-ATD-2 Aircraft Technical Dictionary - IAP, Inc.EA-ITP-G2 A & P Technician General Textbook - IAP, Inc.EA-ITP-P2 A & P Technician Powerplant Textbook - IAP, Inc.EA-TEP-2 Aircraft Gas Turbine Powerplants - IAP, Inc.FAR Federal Aviation Regulations

Reciprocating Engines—AC 65-9A, AC 65-12A, FAR 43, AP, EA-ITP-P2

A01 Inspect and repair a radial engineA02 Overhaul reciprocating engineA03 Inspect, check, service, and repair reciprocating engines and engine installationsA04 Install, troubleshoot, and remove reciprocating engines

Turbine Engines—AC 65-9A, AC 65-12A, AC 65-15A, FAR 33, AP, EA-TEP-2, EA-ITP-P2

B01 Overhaul turbine engineB02 Inspect, check, service, and repair turbine engines and turbine engine installationsB03 Install, troubleshoot, and remove turbine engines

Engine Inspection—AC 65-9A, AC 65-12A, AC 39-7B, AC 43.13-1A, FAR 23, FAR 33, FAR 43, FAR 65,ABS, AP, EA-ITP-G2, EA-ITP-P2

C01 Perform powerplant conformity and airworthiness inspectionsDXX ReservedEXX ReservedFXX ReservedGXX Reserved

Engine Instrument Systems—AC 65-12A, AC 65-15A, AC 20-88A, FAR 65, AMR, AP, EA-TEP-2, EA-ITP-P2

H01 Troubleshoot, service, and repair electrical and mechanical fluid rate-of-flow indicating systemsH02 Inspect, check, service, troubleshoot, and repair electrical and mechanical engine temperature, pressure,

and RPM indicating systems

Engine Fire Protection Systems—AC 65-9A, AC 65-12A, ABS, AMR, AP, EA-ITP-P2

I01 Inspect, check, service, troubleshoot, and repair engine fire detection and extinguishing systems

47

Engine Electrical Systems—AC 65-9A, AC 65-12A, AC 65-15A, AC 43.13-1A, FAR 23, FAR 25, AEE, AP,EA-ITP-G2, EA-ITP-P2

J01 Repair engine electrical system componentsJ02 Install, check, and service engine electrical wiring, controls, switches, indicators, and protective devices

Lubrication Systems—AC 65-12A, AC 65-15A, FAR 33, AP, EA-TEP-2, EA-ITP-P2

K01 Identify and select lubricantsK02 Repair engine lubrication system componentsK03 Inspect, check, service, troubleshoot, and repair engine lubrication systems

Ignition and Starting Systems—AC 65-12A, AC 65-15A, AEE, AP, EA-TEP-2, EA-ITP-P2

L01 Overhaul magneto and ignition harnessL02 Inspect, service, troubleshoot, and repair reciprocating and turbine engine ignition systems and componentsL03 Inspect, service, troubleshoot, and repair turbine engine electrical starting systemsL04 Inspect, service, and troubleshoot turbine engine pneumatic starting systems

Fuel Metering Systems—AC 65-9A, AC 65-12A, AP, EA-TEP-2, EA-ITP-P2

M01 Troubleshoot and adjust turbine engine fuel metering systems and electronic engine fuel controlsM02 Overhaul carburetorM03 Repair engine fuel metering system componentsM04 Inspect, check, service, troubleshoot, and repair reciprocating and turbine engine fuel metering systems

Engine Fuel Systems—AC 65-9A, AC 65-12A, AC 43.13-1A , FAR 23, AP, EA-ITP-P2

N01 Repair engine fuel system componentsN02 Inspect, check, service, troubleshoot, and repair engine fuel systems

Induction and Engine Airflow Systems—AC 65-9A, AC 65-12A, AC 43.13-1A, AP, EA-TEP-2, EA-ITP-P2

O01 Inspect, check, troubleshoot, service, and repair engine ice and rain control systemsO02 Inspect, check, service, troubleshoot, and repair heat exchangers, superchargers, and turbine engine airflow

and temperature control systemsO03 Inspect, check, service, and repair carburetor air intake and induction manifolds

Engine Cooling Systems—AC 65-12A, ABS, AP, EA-ITP-P2

P01 Repair engine cooling system componentsP02 Inspect, check, troubleshoot, service, and repair engine cooling systems

Engine Exhaust and Reverser Systems—C 65-12A, AC 43.13-1A, EA-ITP-P2

Q01 Repair engine exhaust system componentsQ02 Inspect, check, troubleshoot, service, and repair engine exhaust systemsQ03 Troubleshoot and repair engine thrust reverser systems and related components

Propellers—AC 65-9A, AC 65-12A, AC 43.13-1A, FAR 43, FAR 65, AP, EA-ATD-2, EA-APC, EA-ITP-P2

R01 Inspect, check, service, and repair propeller synchronizing and ice control systemsR02 Identify and select propeller lubricants

48

R03 Balance propellersR04 Repair propeller control system componentsR05 Inspect, check, service, and repair fixed pitch, constant speed and feathering propellers, and propeller

governing systemsR06 Install, troubleshoot, and remove propellersR07 Repair aluminum alloy propeller blades

Auxiliary Power Units—DAT, EA-363, EA-ATD-2, EA-TEP-2

T01 Inspect, check, service, and troubleshoot turbine-driven auxiliary power units

NOTE: AC 00-2, Advisory Circular Checklist, transmits the status of all FAA advisory circulars (AC's), as wellas FAA internal publications and miscellaneous flight information such as Airman’s Information Manual (AIM),Airport/Facility Directory, knowledge test study guides, and other material directly related to a certificate orrating. To obtain a free copy of AC 00-2, send your request to:

U.S. Department of TransportationProperty Use and Storage Section, M-483.7Washington, DC 20590

49

AVIATION MECHANIC POWERPLANT EXAMINATION QUESTION REFERENCES

A01:1. AC 65-12A2. AC 65-12A3. AC 65-12A4. AC 65-12A5. AC 65-12A6. AC 65-12A7. AC 65-12A8. AC 65-12A9. AC 65-12A10. AC 65-12AA02:11. AP12. AC 65-12A13. AP14. AC 65-12A15. AC 65-12A16. AP17. AC 65-12A18. AC 65-12A19. AC 65-12A20. AP21. EA-ITP-P222. AC 65-12A23. AP24. AP25. AC 65-12A26. AC 65-12A27. AC 65-12A28. AC 65-12A29. AC 65-12A30. EA-ITP-P231. AP32. AC 65-12A33. AC 65-12A34. AC 65-12A35. AP36. AP37. AP38. AC 65-12A39. AC 65-12A40. AC 65-12A41. AC 65-12A42. AC 65-12A43. AC 65-12A44. AC 65-12A45. AC 65-12A46. AC 65-12A47. APA03:48. AC 65-12A49. AP50. AC 65-12A51. AC 65-12A52. AC 65-12A53. FAR 43

50

54. EA-ITP-P255. AC 65-12A56. AC 65-12A57. AC 65-12A58. AP59. AC 65-12A60. AC 65-12A61. AC 65-12A62. AC 65-12A63. AC 65-12A64. AC 65-12A65. AC 65-12A66. EA-ITP-P267. AC 65-9A68. AC 65-12A69. AC 65-12A70. EA-ITP-P271. AC 65-12A72. AC 65-12A73. AC 65-12A74. AC 65-12A75. AC 65-12A76. AC 65-12A77. AC 65-12A78. AC 65-12A79. AC 65-12A80. AC 65-12A81. AP82. AC 65-12A83. AP84. APA04:85. AP86. AC 65-12A87. AC 65-12A88. AC 65-12A89. AC 65-12A90. AP91. AC 65-12A92. AC 65-12A93. EA-ITP-P294. AC 65-12A95. AC 65-12A96. AC 65-12A97. AC 65-12A98. AC 65-12A99. AP100. AC 65-12A101. AC 65-12A102. AC 65-12A103. AC 65-12A104. AC 65-12A105. AP106. EA-ITP-P2107. APB01:108. AC 65-12A109. AC 65-12A

51

110. AC 65-12A111. AC 65-12A112. AP113. EA-TEP-2114. AC 65-12A115. AC 65-12A116. AC 65-12A117. AC 65-12A118. AC 65-12A119. AC 65-12A120. AC 65-12A121. AC 65-12A122. AC 65-12A123. AC 65-9A124. AC 65-12A125. EA-ITP-P2126. AC 65-12A127. AC 65-12A128. EA-TEP-2129. AC 65-12A130. AC 65-12A131. EA-TEP-2132. AC 65-12A133. AC 65-12A134. AC 65-12A135. FAR 33136. EA-TEP-2137. EA-TEP-2138. EA-ITP-P2139. FAR 33.4140. EA-TEP-2B02:141. AC 65-12A142. EA-ITP-P2143. AC 65-12A144. AC 65-12A145. AC 65-15A146. AC 65-12A147. AC 65-12A148. AC 65-12A149. AC 65-12A150. AC 65-15A151. AC 65-12A152. AC 65-12A153. AC 65-12A154. AC 65-12A155. AC 65-12A156. AC 65-12A157. AC 65-12A158. AC 65-12A159. AC 65-12A160. AC 65-12A161. AC 65-12A162. AC 65-12A163. AC 65-9A164. AC 65-9A165. AC 65-12A166. AC 65-12A

52

167. EA-TEP-2168. AC 65-12A169. AC 65-12A170. AC 65-12A171. AC 65-12A172. AC 65-12A173. EA-ITP-P2174. EA-TEP-2175. EA-ITP-P2176. AP177. AC 65-12A178. AC 65-12A179. AC 65-15A180. AC 65-15A181. AC 65-15A182. AC 65-15A183. EA-TEP-2184. AP185. AC 65-12A186. AC 65-12A187. AC 65-12A188. AC 65-12A189. AC 65-12A190. AC 65-12A191. EA-ITP-P2192. AC 65-12A193. EA-ITP-P2194. AC 65-12A195. AC 65-12A196. EA-ITP-P2197. EA-TEP-2198. EA-TEP-2199. EA-ITP-P2B03:200. AC 65-12A201. AC 65-9A202. AC 65-12A203. AC 65-12A204. AC 65-12A205. AC 65-12A206. AC 65-12A207. AC 65-12A208. EA-ITP-P2209. EA-ITP-P2210. AC 65-12A211. AC 65-12A212. AC 65-12A213. AC 65-12A214. AC 65-12A215. AC 65-12A216. AC 65-12A217. AC 65-12A218. AC 65-12A219. EA-ITP-P2220. EA-ITP-P2221. AC 65-12A222. AC 65-12A223. EA-TEP-2

53

224. EA-TEP-2225. AP226. AP227. EA-TEP-2C01:228. AC 39-7B229. EA-ITP-G2230. AC 65-12A231. AC 65-12A232. AC 65-9A233. FAR 43234. FAR 39.3 & AC 39-7B235. EA-ITP-G2236. FAR 43237. AC 65-12A238. ABS239. AC 43.13-1A240. AC 65-12A241. FAR 23.903242. AC 65-12A243. AC 65-12A244. AC 65-9A245. FAR 65.95246. FAR 43247. FAR 23248. FAR 43.13249. FAR 43.9250. FAR 43.13a251. AC 65-9A252. FAR 23253. AC 65-12A254. FAR 33255. EA-ITP-P2256. APH01:257. AC 65-12A258. AC 65-15A259. AC 65-12A260. AC 65-15A261. AC 65-15A262. AC 65-12A263. AP264. AEE265. EA-TEP-2266. APH02:267. AC 65-12A268. AP269. AC 65-15A270. AC 65-15A271. AC 65-15A272. AC 65-12A273. AC 65-12A274. AC 65-15A275. AC 65-12A276. AC 65-12A277. AC 65-12A278. AC 65-15A

54

279. AC 65-15A280. AP281. AC 65-12A282. AC 65-12A283. AC 65-12A284. AC 65-12A285. AC 65-15A286. EA-ITP-P2 & EA-TEP-2287. AC 65-12A288. AC 65-15A289. AC 65-15A290. AC 65-12A291. FAR 65.81292. AC 65-15A293. AC 65-12A294. AC 65-12A295. AP296. EA-TEP-2297. EA-TEP-2298. AC 65-12A299. AC 65-12A300. AC 65-12A301. AC 65-12A302. AC 65-12A303. AC 65-12A304. AC 65-12A305. AMR306. AMR307. EA-TEP-2308. AP309. AC 20-88AI01:310. AC 65-12A311. AC 65-12A312. AC 65-12A313. AC 65-12A314. AC 65-12A315. AC 65-12A316. AC 65-15A317. AC 65-12A318. AC 65-12A319. AC 65-15A320. AC 65-12A321. AC 65-12A322. AC 65-12A323. AC 65-15A324. AC 65-15A325. AC 65-12A326. AP327. AC 65-12A328. AC 65-15A329. AC 65-15A330. AC 65-12A331. AC 65-12A332. AC 65-9A333. AC 65-12A334. AC 65-15A335. AC 65-15A

55

336. AC 65-12A337. AC 65-12A338. AMR339. ABS340. EA-ITP-P2341. AC 65-12AJ01:342. AEE343. AC 65-9A344. AC 65-9A345. AC 65-12A346. AC 65-9A347. AC 65-9A348. AC 65-9A349. AC 65-9A350. AC 65-9A351. AC 65-9A352. AC 65-9A353. AEE354. FAR 25.1351355. AC 65-9A356. AC 65-9A357. AC 65-9A358. AC 65-15A359. AEE360. AC 65-9A361. AEE362. EA-ITP-P2363. AEE364. AEE365. AEE366. AEE367. EA-ITP-G2368. EA-ITP-G2369. EA-ITP-G2370. EA-ITP-G2371. AP372. EA-ITP-P2373. EA-ITP-G2374. AEEJ02:375. AC 43.13-1A376. AC 65-12A377. AC 43.13-1A378. AC 43.13-1A379. AC 65-12A380. AC 65-12A381. AEE382. AEE383. AC 65-9A384. AC 65-12A385. AC 65-12A386. AP387. AC 43.13-1A388. AC 65-12A389. AC 65-12A390. AC 43.13-1A391. AC 43.13-1A

56

392. AC 65-12A393. AC 43.13-1A394. AC 43.13-1A395. EA-ITP-G2396. EA-ITP-G2397. EA-ITP-P2398. EA-ITP-P2399. EA-ITP-P2400. FAR 23.1357401. EA-ITP-P2402. EA-ITP-P2403. AEE404. EA-ITP-P2405. EA-ITP-P2406. EA-ITP-P2407. EA-ITP-P2408. EA-ITP-P2409. AEE410. EA-ITP-P2K01:411. AC 65-12A412. AC 65-12A413. AC 65-15A414. AC 65-12A415. AP416. AC 65-12A417. AC 65-12A418. AC 65-12A419. AC 65-12A420. AP421. AC 65-12A422. AC 65-12A423. AC 65-12A424. AC 65-12A425. AC 65-12A426. AC 65-12A427. AP428. AP429. AP430. EA-TEP-2431. EA-ITP-P2432. EA-ITP-P2K02:433. EA-TEP-2434. AP435. AC 65-12A436. AC 65-12A437. AC 65-12A438. AC 65-12A439. AP440. EA-TEP-2441. AC 65-12A442. AC 65-12A443. AC 65-12A444. AC 65-12A445. AC 65-12A446. AC 65-12A447. FAR 33.71

57

448. FAR 33.71449. AC 65-12A450. EA-TEP-2451. AC 65-12A452. AC 65-12A453. AC 65-12A454. AC 65-12A455. AC 65-12A456. EA-TEP-2K03:457. EA-ITP-P2458. AC 65-12A459. AC 65-12A460. AC 65-12A461. AC 65-12A462. AP463. AC 65-12A464. AC 65-12A465. AP466. AC 65-12A467. AC 65-12A468. AC 65-12A469. AC 65-12A470. AC 65-12A471. AC 65-12A472. AP473. AC 65-12A474. AC 65-12A475. AC 65-12A476. AC 65-12A477. AC 65-12A478. AC 65-12A479. AC 65-12A480. AC 65-12A481. AP482. AC 65-12A483. AC 65-12A484. AC 65-12A485. AC 65-12A486. AC 65-12A487. AC 65-12A488. AC 65-12A489. AC 65-12A490. AC 65-12A491. AC 65-12A492. AC 65-12A493. AC 65-12A494. AC 65-12A495. AC 65-12A496. AC 65-12A497. AC 65-12A498. FAR 23.1013499. EA-TEP-2500. AC 65-12A501. EA-ITP-P2502. AC 65-12AL01:503. AP

58

504. AC 65-12A505. AC 65-12A506. AC 65-12A507. AC 65-12A508. AP509. AC 65-12A510. AP511. AC 65-12A512. AC 65-12A513. AC 65-12A514. AC 65-12A515. EA-ITP-P2516. AC 65-12A517. AC 65-12A518. EA-ITP-P2519. AC 65-12A520. AC 65-12A521. AC 65-12A522. AC 65-12A523. AC 65-12A524. AC 65-12A525. AP526. AC 65-12A527. AC 65-12A528. AC 65-12A529. AC 65-12A530. AC 65-12A531. AC 65-12A532. AP533. AC 65-12A & AP534. AC 65-12A535. AC 65-12A536. AC 65-12A537. AC 65-12A538. AC 65-12A539. AP540. APL02:541. EA-ITP-P2542. AC 65-12A543. AC 65-12A544. AP545. AC 65-12A546. AC 65-12A547. AC 65-12A548. AP549. AC 65-12A550. AC 65-12A551. AC 65-12A552. AC 65-12A553. AP & EA-ITP-P2554. AEE555. AC 65-12A556. AC 65-12A557. AC 65-12A558. AC 65-12A559. EA-TEP-2560. EA-TEP-2

59

561. AP562. EA-ITP-P2563. EA-ITP-P2L03:564. AC 65-12A565. AP566. AC 65-12A567. AC 65-12A568. AC 65-12A569. AC 65-12A570. AC 65-12A571. AP572. AP573. AC 65-12A574. AC 65-12A575. AC 65-12A576. AP577. AC 65-12A578. AP579. AC 65-12A580. AC 65-12A581. AC 65-12A582. AC 65-12A583. AC 65-12A584. AC 65-12A585. AC 65-12A586. AC 65-12A587. AC 65-12A588. AC 65-12A589. AC 65-12A590. AC 65-12A591. AC 65-12A592. AC 65-12A593. AC 65-12A594. AC 65-12A595. EA-ITP-P2596. AC 65-12A597. AC 65-12A598. AC 65-12A599. AC 65-15A600. AP601. AC 65-12A602. AC 65-12A603. AC 65-12A604. AC 65-12A605. AC 65-12A606. AC 65-12A607. AC 65-12A608. AC 65-12A609. AC 65-12A610. AC 65-12A611. AC 65-12A612. AC 65-12A613. AP614. EA-ITP-P2615. EA-ITP-P2616. EA-ITP-P2617. EA-ITP-P2

60

618. EA-ITP-P2619. EA-ITP-P2620. EA-ITP-P2621. EA-ITP-P2622. EA-ITP-P2623. EA-ITP-P2624. EA-ITP-P2L04:625. EA-ITP-P2626. EA-TEP-2627. AP628. EA-ITP-P2629. EA-ITP-P2630. EA-ITP-P2631. EA-ITP-P2632. EA-ITP-P2633. APM01:634. AC 65-12A635. EA-ITP-P2636. AC 65-12A637. AP638. AP639. AP640. AP641. EA-TEP-2642. EA-TEP-2643. EA-TEP-2644. APM02:645. EA-ITP-P2646. AC 65-12A647. AC 65-12A648. AC 65-12A649. AC 65-12A650. AC 65-12A651. EA-ITP-P2652. AP653. EA-ITP-P2 & AC 65-12A654. AC 65-12A655. AP656. AC 65-12A657. AC 65-12A658. AC 65-12A659. AC 65-12A660. AC 65-12A661. AC 65-12A662. AC 65-12A663. AC 65-12A664. AC 65-12A665. AC 65-12A666. AC 65-12A667. AC 65-12A668. AP669. AP670. AC 65-12A671. EA-ITP-P2672. AC 65-12A

61

673. AC 65-12A674. AC 65-12A675. AC 65-12A676. AC 65-12A677. AC 65-12A678. AP679. AC 65-12A680. AC 65-12A681. AC 65-12AM03:682. AC 65-12A683. AP684. AC 65-12A685. AC 65-12A686. AC 65-12A687. AC 65-12A688. AC 65-12A689. AC 65-12A690. AC 65-12A691. AC 65-12A692. AC 65-12A693. AC 65-12A694. AC 65-12A695. AC 65-12A696. AC 65-12A697. AP & EA-ITP-P2698. APM04:699. AC 65-12A700. AC 65-12A701. AC 65-12A702. AC 65-12A703. AP704. AC 65-12A705. AP706. AC 65-12A707. AC 65-12A708. AC 65-12A709. AP710. AC 65-12A711. AC 65-12A712. AC 65-12A713. AC 65-12A714. AC 65-12A715. AC 65-9A716. AC 65-12A717. AC 65-12A718. AC 65-12A719. AC 65-12A720. AC 65-12A721. AC 65-12A722. EA-ITP-P2723. AC 65-12A724. AC 65-12A725. AC 65-12A726. EA-TEP-2727. EA-ITP-P2728. AC 65-12A

62

729. EA-ITP-P2730. EA-ITP-P2731. EA-ITP-P2N01:732. AC 65-9A733. AC 65-12A734. FAR 23.995735. AC 65-9A736. AC 65-9A737. AC 65-9A738. AC 65-9A739. AC 65-9A740. AC 65-9A741. AC 65-9A742. AC 65-9A743. APN02:744. AP745. FAR 23.119746. AC 65-9A747. AC 43.13-1A748. AC 65-9A749. FAR 23.955750. AC 65-9A751. AC 65-9A752. AC 65-9A753. AC 65-9A754. AC 65-12A755. AC 65-9A756. AP757. AP 65-9A758. AC 65-9A759. AC 65-9A760. AC 65-9A761. AP762. AP763. AC 65-12A764. AC 65-12A765. AP & AC 65-12A766. EA-ITP-P2767. EA-ITP-P2768. EA-ITP-P2769. EA-ITP-P2770. EA-ITP-P2771. EA-ITP-P2O01:772. AP773. AC 65-9A774. AC 65-12A775. AC 65-12A776. AC 65-12A777. AC 65-12A778. AC 65-12A779. AC 65-12AO02:780. AC 65-12A781. AC 65-12A782. AC 65-12A

63

783. EA-ITP-P2784. AC 43.13-1A785. AC 65-12A786. AC 65-12A787. AC 65-12A788. AC 65-12A789. AC 65-12A790. AC 65-12A791. AC 65-12A792. AC 65-12A793. AC 65-12A794. EA-ITP-P2795. AC 65-12A796. EA-TEP-2797. EA-TEP-2798. EA-TEP-2799. EA-TEP-2800. EA-TEP-2801. EA-TEP-2802. EA-TEP-2O03:803. AP804. AC 65-12A805. AC 65-12A806. AP807. AC 65-12A808. EA-ITP-P2809. EA-ITP-P2810. AC 65-9A811. EA-ITP-P2812. AC 65-12A813. AC 65-12AP01:814. AC 65-12A815. AC 65-12A816. AC 65-12A817. AC 65-12A818. AC 65-12A819. AC 65-12A820. AC 65-12A821. EA-ITP-P2822. EA-ITP-P2823. AC 65-12AP02:824. AC 65-12A825. AC 65-12A826. EA-ITP-P2827. AC 65-12A828. AC 65-12A829. AC 65-12A830. AC 65-12A831. AP832. AC 65-12A833. AP834. AP835. AC 65-12A836. AC 65-12A837. AC 65-12A

64

838. AC 65-12A839. AP840. ABS841. AC 65-12A842. AC 65-12A843. AC 65-12A844. AC 65-12A845. AC 65-12AQ01:846. AC 65-12A847. EA-ITP-P2848. EA-ITP-P2849. AC 65-12A850. AC 65-12A851. AC 65-12A852. AC 43.13-1A853. AC 43.13-1A854. AC 65-12AQ02:855. AC 65-12A856. AC 65-12A857. AC 65-12A858. AC 43.13-1A859. AC 65-12A860. AC 65-12A861. AC 65-12A862. AC 65-12A863. AC 65-12A864. AC 65-12A865. AC 65-12A866. AC 65-12A867. AC 43.13-1A868. AC 43.13-1A869. AC 43.13-1A870. AC 43.13-1A871. EA-ITP-P2872. AC 43.13-1AQ03:873. EA-TEP-2874. EA-TEP-2875. EA-TEP-2876. EA-TEP-2877. EA-TEP-2878. EA-TEP-2879. EA-TEP-2880. EA-TEP-2R01:881. AC 65-12A882. AC 65-12A883. AC 65-12A884. AC 65-12A885. AC 65-12A886. AC 65-12A887. AC 65-12A888. EA-APC889. EA-ITP-P2R02-R03:890. AC 65-12A891. AP

65

892. AC 65-12A893. AC 65-12A894. AC 43.13-1A895. AC 43.13-1A896. AC 65-12A897. AC 65-12A898. AC 65-12AR04:899. AC 65-12A900. AC 65-12A901. AC 65-12A902. AC 65-12A903. AC 65-12A904. AC 65-12A905. AC 65-12A906. AC 65-12A907. AC 65-12A908. AC 65-12A909. AC 65-12A910. AC 65-12A911. AC 65-12AR05:912. AC 65-12A913. AC 65-12A914. AC 65-12A915. AC 65-12A916. AC 65-9A917. AC 65-12A918. AC 65-12A919. AP920. AC 65-12A921. AC 65-12A922. AC 65-12A923. AC 65-12A924. AC 65-12A925. AC 65-12A926. AC 65-12A927. AC 65-12A928. AC 65-12A929. AC 65-12A930. AC 65-12A931. AC 65-12A932. AC 65-12A933. AC 65-12A934. AC 65-12A935. AC 65-12A936. AC 65-12A937. AC 65-12A938. AC 65-12A939. AC 65-12A940. AC 65-12A941. AC 43.13-1A942. EA-APC943. EA-AP944. AP945. AC 65-12A946. EA-ITP-P2947. EA-ITP-P2

66

948. EA-ATD-2949. AC 65-12A950. AC 65-12A951. AC 65-12A952. AC 65-12A953. AC 65-12A954. AP955. AC 65-12A956. AC 65-12A957. AC 65-12A958. AC 65-12A959. FAR 65.81 & 43 App A960. AC 65-12A961. AP962. EA-ITP-P2963. EA-ITP-P2964. EA-ITP-P2965. EA-ITP-P2R06:966. EA-ITP-P2967. AC 65-12A968. AC 65-12A969. AC 65-12A970. AC 65-12A971. EA-APC972. AC 43.13-1A973. AC 65-12A974. AC 65-12A975. AC 65-12A976. EA-APC977. AC 65-12A978. AC 65-12A979. EA-APC980. AC 65-12A981. AC 65-12A982. AC 65-12AR07:983. AC 43.13-1A984. AC 43.13-1A985. AP986. AP987. EA-ITP-P2988. EA-ITP-P2989. AP990. AP991. FAR 43 App A & FAR 65.81992. AP993. AP994. AP995. AP996. FAR 43 App ATO1:997. EA-363998. EA-363999. EA-3631000. DAT & EA-ATD-21001. EA-TEP-21002. EA-363

67

1003. EA-3631004. EA-3631005. EA-TEP-21006. EA-363

68

COMPUTER TESTING DESIGNEES

The following is a list of the computer testing designees authorized to give FAA knowledge tests. This list should behelpful in choosing where to register for a test or for requesting additional information.

Aviation Business Services1-800-947-4228outside U.S. (415) 259-8550

Drake Prometric1-800-359-3278outside U.S. (612) 896-7702

Sylvan Learning Systems, Inc.1-800-967-1100outside U.S. (410) 880-0880, Extension 8890

The latest listing of computer testing center locations may be obtained through FedWorld, (703) 321-3339, in theFAA library file named TST_SITE. For technical assistance, contact the FedWorld help desk at (703) 487-4608.