Aviation Electronics Technician 1 - Historic Naval Ships Association

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Antisubmarine warfare weapons systems, 7-11basic ASW weapons systems, 7-11fixed-wing kill store systems, 7-17fixed-wing release and control system, 7-18fixed-wing search store systems, 7-13helicopter kill store system, 7-18helicopter search store sytems, 7-14Automatic carrier landing system, 9-1block diagram, 9-2components, 9-1principles of operation, 9-3safety provisions, 9-5Automatic carrier landing system components, 9-1Approach Indexer 128AV653- 1,9-3Approach Power Compensator AN/ASN-54, 9-3Attitude Reference Indicator ID-1791/,4, 9-3Automatic Flight Control System AN/ASW-42,9-1Digital Data Communication Set AN/ASW-25B,9-1Discrete Message Indicator 1284V66836, 9-3Instrument Landing System AN/SPN-41, 9-1Landing Control Central System AN/SPN-42, 9-2Radar Beacon AN/APN-154B, 9-3Receiving-Decoding Group AN/ARA-63, 9-1warning indexer panel, 9-3Automatic carrier landing system operation, 9-3landing sequence, 9-4mode I landing operation, 9-4Automatic direction finder (ADF), 2-12ADF mode of operation, 2-12antenna mode of operation, 2-12Control Panel C-6899/ARN-83, 2-12Loop Antenna AS-1863/ARN-83, 2-12loop mode of operation, 2-12Receiver R-1391/ARN-83, 2-12sense antenna, 2-12BBearing-distance-heading indicator (BDHI), 5-4functions, 5-5indicator parts, 5-4Block diagramsAPS-115 signal flow, 3-8basic television system, 5-17data link, 1-21DIFAR sonobuoy, 4-26digital data processor, 8-3FLIR azimuth drive, 6-18FLIR control servomechanism bite, 6-22FLIR elevation drive, 6-19FLIR positioning/stabilization, 6-13FLIR power supply-video converter BITE, 6-17FLIR receiver-converter BITE, 6-14FLIR receiver-converter heat exchanger, 6-12FLIR system, 6-8FLIR TTSC, 6-24FLIR video indicator, 6-27FLIR video processing, 6-15heads-up display, 5-7HF radio system, 1-19tactical display system interface, 5-17teletype, 1-24Trainer 11D13A, 3-9UHF radio system, 1-15Bonding, 10-14lightning protection, 10-15purposes, 10-14CCamera tubes, 5-22image isocon, 5-23image orthicon, 5-22plumbicon, 5-25secondary electron conduction (SEC), 5-25vidicon, 5-24INDEX-2
Computer input/output units, 8-9devices, 8-11input devices, 8-11output devices, 8-12parallel transmission, 8-10parallel versus serial transmissions, 8-10serial transmission, 8-11Computer programming fundamentals, 8-13executive routines, 8-14flow charting, 8-15jump and return jump instructions, 8-14maintenance programs, 8-15program construction, 8-15subroutines, 8-14Computers, 8-1applications, 8-2integrated circuit technology, 8-12makeup, 8-1peripheral avionics systems, 8-16programming fundamentals, 8-13types, 8-2Computer types, 8-2analog, 8-2digital, 8-2general-purpose, 8-3special-purpose, 8-3DData link system, 1-20block diagram, 1-21comm interface No. 2, 1-21Control-Monitor Panel C7790/ACQ-5, 1-21Converter-Control CV-2528/ACQ-5, 1-20modes of operation, 1-22Power Supply PP-6140/ACQ-5, 1-21terms, 1-22Digital computers, 8-2data processor, 8-3input/output, 8-9operation, 8-3Digital data processor, 8-3arithmetic-logic unit, 8-5block diagram, 8-3control unit, 8-4internal data storage unit, 8-5Digital data storage, 8-5magnetic cores, 8-6magnetic disks, 8-8magnetic drums, 8-7magnetic tapes, 8-8semiconductor memories, 8-6thin film, 8-7Doppler, 2-18EAntenna AS-1350/APN- 153(V), 2-18Control Indicator C-4418A/APN-153(V), 2-18operational theory, 2-18Receiver Transmitter RT-680A/APN-153(V),2-18test indications, 2-19Electrical noise, 10-3ac generators and motors, 10-3beacons, 10-4coded-pulse equipment, 10-4dc motors, 10-3inverters, 10-4nonlinear elements, 10-5power lines, 10-6propeller systems, 10-5radar, 10-4receiver oscillators, 10-5relays, 10-4thyratrons, 10-4transponders, 10-4INDEX-3
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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
Page 198 and 199: 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 250 and 251: 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
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
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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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