Aviation Electronics Technician 1 - Historic Naval Ships Association

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Heads-up display (HUD), 5-5air-to-air mode of operation, 5-13air-to-ground mode of operation, 5-14analog-to-digital conversion mode, 5-9BITE functions, 5-10block diagram, 5-7circle mode, 5-81cruise mode of operation, 5-13declutter, 5-10deflection module, 5-10digital computer, 5-7display unit, 5-9input receivers, 5-6landing mode of operation, 5-14line mode, 5-8optical module, 5-9signal data processor, 5-6symbol generator, 5-7symbology, 5-10takeoff mode of operation, 5-13video module, 5-9Helicopter search store sytems, 7-14SH-3 helicopter sonobuoy launcher, 7-16SH-60 helicopter sonobuoy launcher, 7-16HF communications, 1-16antenna, 1-18block diagram, 1-19Control Box C-9245/ARC- 161, 1-17Coupler CU-2070/ARC, 1-18lightning arrester, 1-18receive function, 1-19Receiver-Transmitter RT-1000/ARC-161, 1-17Remote Control Unit TSEC/KY-75, 1-19RF Amplifier AM-6561/ARC-161, 1-17Security Unit TSEC/KY-75, 1-18transmit function, 1-19Horizontal situation indicator (HSI), 5-1control box, Copilot A279, 5-2control box, NAV/COMM A309, 5-3control box, Pilot A280, 5-2Indicator ID-1540/A, 5-1system description, 5-4IIFF systems, 3-15interrogator set, 3-20transponder set, 3-15Indicators, 5-1bearing-distance-heading indicator (BDHI), 5-4heading indicators, 5-1heads-up display (HUD), 5-5horizontal situation indicator (HSI), 5-1tactical display system (non-bud) (TDS), 5-15Infrared, 6-1detectors, 6-4foward-looking infrared system (FLIR), 6-7imaging system, 6-5optics, 6-4radiation, 6-3thermal imaging, 6-1Infrared detectors, 6-4elemental detectors, 6-4imaging detectors, 6-4photon effect, 6-5thermal effect, 6-5Infrared imaging system, 6-5detector array, 6-5front end optics, 6-7image processing, 6-7refrigeration system, 6-7scene dissection, 6-6single detector, 6-6INDEX-6
Infrared radiation, 6-3sources, 6-3Intercommunication system, 1-3Control Panel C-8760/AI, 1-3Control Panel LS-602/AI, 1-4Converter-Interconnecting Box CV-3048, 1-4Crew ICS Panel LS-601/AI, 1-4indicators, 1-5Manchester word decoding, 1-7Manchester word encoding, 1-6multiplex transmission, 1-8roll call, 1-8signal interfaces, 1-4word format, 1-5Interference coupling, 10-6complex coupling, 10-7conductive coupling, 10-6inductive-capacitive coupling, 10-7inductive-magnetic coupling, 10-6radiation coupling, 10-7Integrated circuit technology, 8-12characteristics, 8-13classifications, 8-12Interrogator set, 3-20Antema AS-2719/AP, 3-20Computer KIR-1A/TSEC, 3-21Control Box C-7383/APX-76A(V), 3-20Electronic Synchronizer SN-416A/APX-76A(V),3-21mode 4 transmission, 3-22modes 1, 2, and 3/A transmission, 3-21performance monitoring, 3-23Receiver-Transmitter3-21reception, 3-22RT-868A/APX-76A(V),Switch Amplifier SA-1568A/APX-76A(V), 3-21LLoran, 2-15MControl Box C-6604/ARN-81, 2-15Indicator IP-796/ARN-81, 2-15Receiver R-1336/ARN-81, 2-15system function, 2-15Mad Recorder RO-32, 4-24Magnetic anomaly detection, 4-15anomaly strength, 4-17compensation for noise, 4-19dc circuit noise, 4-18magnetic anomaly, 4-15maneuver noise, 4-18submarine anomaly, 4-17Magnetic anomaly detection set, 4-21Amplifier Power Supply AM-4535, 4-21Control Box C-6983, 4-21Magnetic Detector DT-323, 4-21Magnetic anomaly detection system, 4-20MAD Recorder RO-32, 4-24Magnetic Anomaly Detection Set AN/ASQ-81,4-21Magnetic Compensator Group AN/ASA-65, 4-22Selector Control Group AN/ASA-71, 4-23Submarine Anomaly Detection GroupAN/ASA-64, 4-22Magnetic compensator group, 4-22compensation coils, 4-23Control Indicator C-8935, 4-22Electronic Control Amplifier AM-6459, 4-22Magnetic Field Computer CP-1390,4-23Magnetic Field Indicator ID-2254, 4-23Magnetometer Assembly DT-355, 4-22INDEX-7
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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
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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 250 and 251: Electrostatic discharge, 10-15compo
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:
Page 300 and 301: 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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