Aviation Electronics Technician 1 - Historic Naval Ships Association

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NNavigation basics, 2-1airborne navigation, 2-7altitudes, 2-7compass rose, 2-5dead reckoning, 2-6direction, 2-5distance, 2-5earth’s size and shape, 2-2electronic assisted navigation, 2-6great circles and small circles, 2-2latitude, 2-3longitude, 2-4OOmega, 2-16Antenna Coupler AS-2623/ARN-99(V), 2-17operating frequencies, 2-16operational theory, 2-16Power Control Panel 960767,2-16Receiver-Converter OR-90/ARN-99(V), 2-17PPeripheral avionics systems, 8-16data link, 8-16navigation, 8-16ordnance/weapons, 8-16search/track radar, 8-16RRadar, 3-1fire control radar, 3-9IFF systems, 3-15search radar, 3-1Radar altimeter, 2-10Height Indicator ID-1760A/APN- 194,2-10Low-Altitude Alarm BZ-157A, 2-11low altitude warning light, 2-11Receiver-Transmitter RT-1042/APN-194, 2-11Radar altimeter warning set (RAWS), 2-11Radio communications, 1-1data link system, 1-20frequency band usage, 1-2HF communciations, 1-16intercommunication system (ICS), 1-3teletype system, 1-22types of, 1-1UHF communications, 1-13VHF communications, 1-11Radio communications types, 1-1radiotelegraph, 1-1radiotelephone, 1-1teletypewriter, 1-1Radio interference reduction components, 10-7bandpass filters, 10-13band-rejection filters, 10-14capacitive filter application, 10-10capacitive filtering, ac circuits, 10-10capacitive filtering, switching devices, 10-11capacitors, 10-8capacitors, selection of, 10-10coaxial feedthrough capacitors, 10-8high-pass filters, 10-13inductive-capacitive filters, 10-12low-pass filters, 10-12resistive-capacitive filters, 10-11Receiver noise interference, 10-1atmospheric static, 10-1broadband interference, 10-2cosmic noise, 10-2narrow-band interference, 10-3precipitation static, 10-2INDEX-8
SSearch radar, 3-1Antenna AS-2146/APS-115, 3-5antema characteristics, 3-5Antenna Control Box C-75 11A/APS-115, 3-2antenna elevation parking control, 3-5Antenna Position Programmer MX-7930/APS-115, 3-3Control Panel C-7512/APS-115, 3-5functional description, 3-8Radar Interface Unit (RIU) MX-7974/ASA-69,3-7Radar Scan Converter Control C-7557/ASA-69,3-6Receiver-Transmitter RT-889/APS-115, 3-3signal flow diagram, 3-8transmitter characteristics, 3-4Selector control group, 4-23Control Panel C-7693/ASA-71, 4-23Control Subassembly MX-8109/ASA-71, 4-24Sonar principles, 4-1absorption and scattering, 4-2depth and temperature, 4-4divergence, 4-3Doppler effect, 4-6echo-ranging, 4-1reflection, 4-2refraction, 4-3reverberation, 4-2sound beam speed, 4-3Sonobuoys, 4-24ATAC/DLC buoys, 4-27BT buoys, 4-26CASS buoys, 4-26deployment, 4-24DIC ASS buoys, 4-26DIFAR buoy block diagram, 4-26Sonobuoys–ContinuedDIFAR buoys, 4-25frequency channels, 4-24LOFAR buoys, 4-25markings, 4-25operating life, 4-25operation principles, 4-24RO buoys, 4-26SAR buoys, 4-26water entry and activation, 4-25Sonobuoy Receiver AN/ARR-72, 4-27Static electricity, 10-15causes of, 10-16effects of, 10-17triboelectric effect, 10-16Submarine anomaly detection group, 4-22TTACAN, 2-13air-to-air mode of operation, 2-15Antenna Assembly AS-26281A, 2-14Control Box C-9054/ARN-84, 2-14ground station, 2-13interruptive self-test, 2-15readiness monitoring, 2-15receive mode of operation, 2-14Receiver-Transmitter RT-1022/ARN-84, 2-14RF Transmission Line Switch SA-1818/A, 2-14Signal Data Converter CV-2837/ARN-84, 2-14station identification, 2-13transmit-receive mode of operation, 2-15Tactical display system (non-bud) (TDS), 5-15block diagram, 5-17copilot/cotac display, 5-15display generator unit, 5-15pilot display, 5-15senso ARU display, 5-16system interface, 5-16TACCO and SENSO displays, 5-16INDEX-9
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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
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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 252 and 253: Heads-up display (HUD), 5-5air-to-a
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
Page 302 and 303: 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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