Aviation Electronics Technician 1 - Historic Naval Ships Association

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Electrostatic discharge, 10-15component susceptibility, 10-17device handling, 10-18device packaging, 10-18elimination of, 10-17markings, 10-19personal apparel, 10-17personnel ground straps, 10-17prime generators, 10-17protective materials, 10-17static electricity, 10-15Electrostatic discharge program, 10-1bonding, 10-14electrical noise, 10-3electrostatic discharge, 10-15interference coupling, 10-6protective material, 10-17radio interference reduction components, 10-7receiver noise interface, 10-1static electricity, 10-15Electrostatic discharge protective material, 10-17antistatic material, 10-18conductive material, 10-17hybrid bags, 10-18FF-14 aircraft weapon systems, 7-1air combat maneuver (ACM) panel, 7-1AN/AWW-4 fuze function control system, 7-4armament control indicator panel, 7-2armament safety override switch, 7-4basic controls and components, 7-1control stick, 7-3decoy dispensing system, 7-4display control panel, 7-2jettison system, 7-4landing gear handle, 7-3F-14 aircraft weapon systems-ContinuedM61A1 20-mm automatic gun fire controlsystem, 7-4master light control panel, 7-3missile control system, 7-4multiple weapons release system, 7-4F/A-18 aircraft weapon systems, 7-5AGM-65 Maverick system, 7-10AGM-88 Harm system, 7-10AIM-7 Sparrow fire control system, 7-10AIM-9 Sidewinder fire control system, 7-11aircraft controller grip, 7-6AN/ALE-39 decoy dispensing system, 7-11AN/AWW-4 fuze function control system, 7-10AN/AWW-7B data link system, 7-10armament computer, 7-8armament safety override switch, 7-6basic controls and components, 7-5bomb release system, 7-10digital computers, 7-9digital display indicators (DDIs), 7-6ground power control panel, 7-5jettison system, 7-9landing gear control handle, 7-6M61A1 20-mm gun system, 7-11master arm control panel, 7-6rocket firing system, 7-10Walleye guided weapon system, 7-10Fighter aircraft weapon systems, 7-1F-14 aircraft, 7-1F/A-18 aircraft, 7-5Fire control radar, 3-9block diagram, 3-9bomb director mode, 3-10bomb director mode display, 3-15fire control (automatic search) display, 3-12INDEX-4
Fire control radar-Continuedfire control (automatic track) display, 3-14fire control (breakaway) display, 3-15fire control (lock on) display, 3-14fire control (manual search) display, 3-13fire control mode, 3-10operating modes, 3-9search display, 3-11search mode, 3-10system controls, 3-10Fixed-wing kill store systems, 7-17bomb bay system, 7-17P-3C wing launcher assembly, 7-18S-3A pylor/rack assembly, 7-18Fixed-wing release and control system, 7-18automatic mode, 7-19jettison, 7-20manual mode, 7-20operation, 7-19Forward-looking infrared system (FLIR), 6-7azimuth drive block diagram, 6-18azimuth drive computer track mode, 6-20azimuth drive forward mode, 6-20azimuth drive manual track mode, 6-20azimuth drive position mode, 6-19azimuth drive subsystem, 6-19block diagram, 6-8control box, 6-25control servomechanism assembly, 6-18control servomechanism BITE, 6-21control servomechanism BITE block diagram,6-22control servomechanism BITE 1 test, 6-23control servomechanism BITE 2 test, 6-23control servomechanism BITE 3 test, 6-23control servomechanism fault isolate test, 6-21Forward-looking infrared system (FLIR)—Continuedelevation drive block diagram, 6-19elevation drive subsystem, 6-21infrared to composite video conversion, 6-10infrared to video processing, 6-11positioning and stabilization, 6-12positioning/stabilization block diagram, 6-13power supply, 6-14power supply-video converter assembly, 6-14power supply-video converter BITE, 6-17power supply-video converter BITE blockdiagram, 6-17receiver-converter assembly, 6-9receiver-converter BITE, 6-13receiver-converter BITE block diagram, 6-14receiver-converter heat exchanger diagram, 6-12signal optical path, 6-10target track sight control, 6-25target track sight control block diagram, 6-24temperature control, 6-12video indicator, 6-26video indicator block diagram, 6-27video processing, 6-14video processing block diagram, 6-15Frequency band usage, 1-2Hfrequency spectrum, 1-2MF and HF band, 1-2VHF and UHF band, 1-2VLF and LF band, 1-2Heading indicators, 5-1bearing-distance-heading indicator (BDHI), 5-4horizontal situation indicator (HSI), 5-1INDEX-5
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PASS/FAIL ASSIGNMENT PROCEDURESIf y
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Student CommentsCourse Title:Aviati
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Table 1-1.-Radio-Frequency Spectrum
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Figure 1-3.-LS-602/AI control panel
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Figure 1-4.-Manchester encoding.thr
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they can complete a full cycle. The
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one-shot circuit output is directly
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Figure 1-7.-VHF-AM control box.Figu
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indicators in the following text. E
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Figure 1-11.-C-9245/ARC-161 control
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and the PWR/FILL switch is not in t
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panel is in OFF. If the DTS control
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the keyboard are sent directly. Rec
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the signal data converter, where it
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Navigation is both an art and a sci
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this axis at right angles to it (fi
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. Course is the intended horizontal
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The standard atmosphere is theoreti
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eadings are higher than actual. Thi
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The barometric switch in the RAWS a
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Major ComponentsThe AN/ARN-84(V) TA
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the outputs is used for the automat
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DOPPLERIn the following text we wil
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CHAPTER 3RADARAs an avionics superv
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the antennas will stop at the posit
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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
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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
Page 200 and 201: 4. Stores the results of manipulati
Page 202 and 203: An overall check of a computer can
Page 205 and 206: CHAPTER 9AUTOMATIC CARRIER LANDING
Page 207 and 208: stabilized deck-coordinated system
Page 209 and 210: Figure 9-3.-Mode I landing sequence
Page 211: Figure 9-5.-Lateral automatic wave-
Page 214 and 215: Precipitation StaticPrecipitation s
Page 216 and 217: l Sliding-contact interference. Thi
Page 218 and 219: the signal applied to it. These spu
Page 220 and 221: the following methods: short circui
Page 222 and 223: Figure 10-4.-Internal construction
Page 224 and 225: Figure 10-9.-Methods for using RC f
Page 226 and 227: Band-Rejection FiltersA band-reject
Page 228 and 229: Causes of Static ElectricityGenerat
Page 230 and 231: composed of carbon particles, impre
Page 233 and 234: APPENDIX 1REFERENCES USED TODEVELOP
Page 235: Chapter 7Airborne Weapons/Stores Lo
Page 238 and 239: CHAPTER 3A1.A2.A3.A4.A5.A6.A7.A8.A9
Page 240 and 241: A7. Linking two or more computers t
Page 242 and 243: FORMULASAIII-2
Page 244 and 245: AIII-4
Page 246 and 247: Comparison of Units in Electric and
Page 248 and 249: Antisubmarine warfare weapons syste
Page 252 and 253: Heads-up display (HUD), 5-5air-to-a
Page 254 and 255: NNavigation basics, 2-1airborne nav
Page 256 and 257: Teletype system, 1-22block diagram,
Page 259: Assignment QuestionsInformation: Th
Page 262 and 263: 1-11. What will the Sillumination o
Page 264 and 265: 1-35.1-36.1-37.1-38.UHF-1 does NOT
Page 266 and 267: 1-59. What arethat thetactical1. Fr
Page 268 and 269: ASSIGNMENT 2Textbook Assignment:
Page 270 and 271: IN ANSWERING QUESTIONS 2-22 THROUGH
Page 272 and 273: 2-43. What method does the AN/APN-1
Page 274 and 275: 2-64. What distance is the maximum
Page 276 and 277: 3-12.3-13.The antenna position prog
Page 278 and 279: 3-32. The 128 nautical mile range i
Page 280 and 281: IN ANSWERING QUESTION 3-53,FIGURE 3
Page 282 and 283: 3-74. What is the nominal peak powe
Page 284 and 285: 4-12. Sonar transmission losses can
Page 286 and 287: 4-31.4-32.4-33.When positive gradie
Page 288 and 289: 4-52. The function of the dual curs
Page 290 and 291: 4-71. The angle between a magnetic
Page 292 and 293: IN ANSWERING QUESTIONS 5-9 THROUGH
Page 294 and 295: 5-29. What component contains theop
Page 296 and 297: 5-51. What type of RF output signal
Page 298 and 299: ASSIGNMENT 6Textbook Assignment:
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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
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7-11. If the temperature of a black
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7-34.A scan mirror is indexed three
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7-56. What is the primary differenc
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ASSIGNMENT 8Textbook Assignment:
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8-21. With the landing gear handle
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8-42. With the F/A-18 AIM-9 Sidewin
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8-66. The jettison of wing stores I
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9-13. What method is used to change
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9-36. In magnetic core memories, a
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9-57. What typeaccess toof instruct
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10-12. To maintain the angle-of-att
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10-35. A receiver tuned to 2.4 kHze
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10-55. When rubbed against any of t
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Aviation Electronics Technician 1 - Historic Naval Ships Association

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