Aviation Electronics Technician 1 - Historic Naval Ships Association

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COURSE OBJECTIVESIn completion this nonresident trainingcourse, you will demonstrate a knowledge ofthe subject matter by correctly answeringquestions on the following: communications,navigation, radar, antisubmarinewarfare, indicators, infrared, weaponssystems, computers, automatic carrierlanding system, and the electrostaticdischarge program.vi
Student CommentsCourse Title:Aviation Electronics Technician 1 (Organizational)NAVEDTRA: 14030 Date:We need some information about you:Rate/Rank and Name: SSN: Command/UnitStreet Address: City: State/FPO: ZipYour comments, suggestions, etc.:Privacy Act Statement: Under authority of Title 5, USC 301, information regarding your military status isrequested in processing your comments and in preparing a reply. This information will not be divulged withoutwritten authorization to anyone other than those within DOD for official use in determining performance.NETPDTC 1550/41 (Rev 4-00)vii
Page 7: PASS/FAIL ASSIGNMENT PROCEDURESIf y
Page 12 and 13: Table 1-1.-Radio-Frequency Spectrum
Page 14 and 15: Figure 1-3.-LS-602/AI control panel
Page 16 and 17: Figure 1-4.-Manchester encoding.thr
Page 18 and 19: they can complete a full cycle. The
Page 20 and 21: one-shot circuit output is directly
Page 22 and 23: Figure 1-7.-VHF-AM control box.Figu
Page 24: indicators in the following text. E
Page 27 and 28: Figure 1-11.-C-9245/ARC-161 control
Page 29 and 30: and the PWR/FILL switch is not in t
Page 31 and 32: panel is in OFF. If the DTS control
Page 33 and 34: the keyboard are sent directly. Rec
Page 35: the signal data converter, where it
Page 38 and 39: Navigation is both an art and a sci
Page 40 and 41: this axis at right angles to it (fi
Page 42 and 43: . Course is the intended horizontal
Page 44 and 45: The standard atmosphere is theoreti
Page 46 and 47: eadings are higher than actual. Thi
Page 48 and 49: The barometric switch in the RAWS a
Page 50 and 51: Major ComponentsThe AN/ARN-84(V) TA
Page 52 and 53: the outputs is used for the automat
Page 54 and 55: DOPPLERIn the following text we wil
Page 57 and 58: CHAPTER 3RADARAs an avionics superv
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the antennas will stop at the posit
Page 61 and 62:
AS-2146/APS-115 AntennaThe radar an
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completes the processing of radar a
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In the on-line mode, the sensor sta
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Mode SwitchThe mode switch is pract
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purpose of the horizon line is to i
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Maximum range for tracking is 40,00
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transmit a reply when RF interrogat
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airspeed-altitude computer. All fra
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SIF reply code is identical to the
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In mode 4, the reply video pulse is
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sound wave. The frequency (in hertz
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to affect the rate of travel of the
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DOPPLER EFFECTWhen there is relativ
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Figure 4-7.-Transducer installed on
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The Sonar Detecting-Range Set AN/AQ
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Figure 4-16.-RO-358/ASQ-13A.mechani
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applies 115 volts ac to the transmi
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are known as angles of dip (fig. 4-
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feet in length and represents the f
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compensation is needed for the long
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labeled ALT COMP. This switch is us
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select which signal goes to which p
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the passive directional sonobuoy (f
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REVIEW QUESTIONSQ1. How was the wor
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TACAN signals. When localizer signa
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1. The HEADING NO-GO indicator illu
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Figure 5-7.-New optical sight with
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computer’s program determines whi
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ias circuit, horizontal and vertica
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Figure 5-9.-Symbology—Continued.5
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Figure 5-14.-Sparrow mode.Figure 5-
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TACTICAL DISPLAY SYSTEM INTERFACEFi
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electrical signal, which varies in
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noise-free at that level. The impor
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Like the random interlace, this sys
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The polarity of the signal develope
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The SEC tube has applications in ex
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CHAPTER 6INFRAREDThe term infrared
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Table 6-1.-Characteristics of IR Ra
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potential difference across a PN ju
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system increases, and the reliabili
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used in the Navy, their principles
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signals from the control servomecha
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Figure 6-15.-FLIR positioning/stabi
Page 151 and 152:
Figure 6-17.-Video converter video
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clamping signals from the sync gene
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shared by both azimuth and elevatio
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where they are converted into three
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go to the azimuth/elevation heat si
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TARGET TRACKING SIGHT CONTROLAs men
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control is injected in this module.
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CHAPTER 7WEAPONS SYSTEMSAs a result
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Figure 7-5.-Master light control pa
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Rocket firing systemWalleye systemA
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The wing-form display is displayed
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Figure 7-15.-Emergency jettison con
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The A/A weapon select switch select
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Part of the system consists of unpr
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Figure 7-22.-SH-3 (series) search a
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ottle and the ECU are mounted on to
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Figure 7-25.-Pylon/rack assembly.ci
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REVIEW QUESTIONSQ1. True or False.
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COMPUTER APPLICATIONSTYPES OF COMPU
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the most important. This data manip
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and other data that are to be used
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to represent the same data that was
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compatibility permits the computer
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most cases, the processing speed fa
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4. Stores the results of manipulati
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An overall check of a computer can
Page 205 and 206:
CHAPTER 9AUTOMATIC CARRIER LANDING
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stabilized deck-coordinated system
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Figure 9-3.-Mode I landing sequence
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Figure 9-5.-Lateral automatic wave-
Page 214 and 215:
Precipitation StaticPrecipitation s
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l Sliding-contact interference. Thi
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the signal applied to it. These spu
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the following methods: short circui
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Figure 10-4.-Internal construction
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Figure 10-9.-Methods for using RC f
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Band-Rejection FiltersA band-reject
Page 228 and 229:
Causes of Static ElectricityGenerat
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composed of carbon particles, impre
Page 233 and 234:
APPENDIX 1REFERENCES USED TODEVELOP
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Chapter 7Airborne Weapons/Stores Lo
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CHAPTER 3A1.A2.A3.A4.A5.A6.A7.A8.A9
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A7. Linking two or more computers t
Page 242 and 243:
FORMULASAIII-2
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AIII-4
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Comparison of Units in Electric and
Page 248 and 249:
Antisubmarine warfare weapons syste
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Electrostatic discharge, 10-15compo
Page 252 and 253:
Heads-up display (HUD), 5-5air-to-a
Page 254 and 255:
NNavigation basics, 2-1airborne nav
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Teletype system, 1-22block diagram,
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Assignment QuestionsInformation: Th
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1-11. What will the Sillumination o
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1-35.1-36.1-37.1-38.UHF-1 does NOT
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1-59. What arethat thetactical1. Fr
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ASSIGNMENT 2Textbook Assignment:
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IN ANSWERING QUESTIONS 2-22 THROUGH
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2-43. What method does the AN/APN-1
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2-64. What distance is the maximum
Page 276 and 277:
3-12.3-13.The antenna position prog
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3-32. The 128 nautical mile range i
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IN ANSWERING QUESTION 3-53,FIGURE 3
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3-74. What is the nominal peak powe
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4-12. Sonar transmission losses can
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4-31.4-32.4-33.When positive gradie
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4-52. The function of the dual curs
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4-71. The angle between a magnetic
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IN ANSWERING QUESTIONS 5-9 THROUGH
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5-29. What component contains theop
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5-51. What type of RF output signal
Page 298 and 299:
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6-20. On the HSI, when a tactical m
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6-42. What control(s) the symbolbri
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6-65. Which, if any, of the followi
Page 306 and 307:
7-11. If the temperature of a black
Page 308 and 309:
7-34.A scan mirror is indexed three
Page 310 and 311:
7-56. What is the primary differenc
Page 312 and 313:
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8-21. With the landing gear handle
Page 316 and 317:
8-42. With the F/A-18 AIM-9 Sidewin
Page 318 and 319:
8-66. The jettison of wing stores I
Page 320 and 321:
9-13. What method is used to change
Page 322 and 323:
9-36. In magnetic core memories, a
Page 324 and 325:
9-57. What typeaccess toof instruct
Page 326 and 327:
10-12. To maintain the angle-of-att
Page 328 and 329:
10-35. A receiver tuned to 2.4 kHze
Page 330:
10-55. When rubbed against any of t
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