Aviation Electronics Technician 1 - Historic Naval Ships Association

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ASSIGNMENT 6Textbook Assignment: “Indicators,” chapter 5, pages 5-1 through 5-27.6-1. Which of the following systemssupply information displayed on theHSIs and BDHIs?1. Communication systems2. Radar systems only3. Navigation systems only4. Radar/navigation systems6-2. In the HSI group, which, if any, ofthe following components areinterchangeable between thepilot’s, copilot’s, and NAV/COMM’sstation?1. HSI group controls only2. HSI group indicators only3. HSI group controls andindicators4. None of the above6-3. On the ID-1540/A horizontalsituation indicator, what is thereference line for reading theaircraft’s heading on the compasscard?1. The lubber line2. The bearing line3. The marker line4. The range lineIN ANSWERING QUESTIONS 6-4 THROUGH 6-8,SELECT FROM COLUMN B THE FUNCTION OF THEHSI ITEMS LISTED IN COLUMN A. SOME ITEMSIN COLUMN B WILL BE USED MORE THAN ONCE.A. HSI ITEMS6-4. Bearing pointer 1. Indicates theNo. 1lubber line6-5. COURSE indicator 2. Points to thebearing of6-6. To-From the selectedindicatorB. FUNCTIONSnavigationalpoint6-7. Bearing pointerNo. 2 3. Displays thecourse arrow6-8. Aircraft symbol setting in adigitalreadout indegrees4. Indicateswhether theselectedcourse isgoing towardor away fromthe selectedbeaconstation6-9. What component controls the inputsto the pilot’s HSI?1. A2082. A2793. A2804. A30938
6-10. The HDG selector switch on thepilot’s HSI control selects whichof the following heading signalsources for display on the HSIcompass card?1. INS-1 and INS-22. INS-1 and STBY GYRO3. INS-2 and STBY GYRO4. Vertical gyro and STBY GYRO6-11. On the pilot’s HSI control, theATTD selector controls which of thefollowing sources of attitudesignals for the pilot’s FDI sphere?1. INS-1 and INS-22. INS-1 and STBY GYRO3. INS-2 and STBY GYRO4. Vertical gyro and STBY GYRO6-12. On the pilot’s HSI control, withthe BRG 1 switch in DA, the COURSEHSI-FDI selector switch must be inwhat position to receive signalsfrom the central computer?1. TACAN2. VOR-1/ILS3. VOR-24. TAC NAV6-13. The BRG 1 switch selects the sourceof the bearing signal displayed onthe bearing pointer 1 on which ofthe following HSIs?1. Pilot’s, copilot’s, and TACCO’s2. Pilot’s, NAv/COMM’S, andTACCO‘s3. Copilot’s, NAV/COMM’S, andTACCO‘s4. Pilot’s, copilot’s, andNAV/COMM’s6-14. On the copilot’s HSI control, theATTD selector controls which of thefollowing sources of attitudesignals for the copilot’s FDIsphere?6-15. The BRG 2 switch on the copilot’sHSI control selects the source ofthe bearing signal displayed on thebearing pointer 2 on which of thefollowing HSIs?1. Pilot’s and copilot’s2. Copilot’s and NAV/COMM’s3. Copilot’s and TACCO’s4. TACCO’s and NAV/COMM’s6-16. When there is a failure with theheading function in the centralrepeater system, what indicatorilluminates on the NAV/COMM HSIcontrol?1. DIST NO-GO2. ATTD BEARING NO-GO3. INS NO-GO4. HEADING NO-GO6-17. Which of the following signals areselected for display on theNAV/COMM HSI by the NAV/COMM HDGswitch?1. MAG and TRUE heading signals2. INS-1 and INS-2 heading signals3. INS-1 and MAG heading signals4. INS-2 and TRUE heading signals6-18. What indication appears on the HSIwith VOR-1 selected if the inputsignal from VOR-1 becomesunreliable?1. VOR-1 NO-Go2. NAV NO-GO3. VOR-1 flag4. NAV flag6-19. What signal will be supplied to theHSI by the UHF-DF/OPTI and the ADFsystems when either is selected?1. Bearing signal2. To-From signal3. Course deviation signal4. NAV flag signal1. INS-1 and INS-22. INS-1 and STBY GYRO3. INS-2 and STBY GYRO4. Vertical gyro and STBY GYRO39
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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
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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-
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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
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Causes of Static ElectricityGenerat
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composed of carbon particles, impre
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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
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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
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
Page 300 and 301: 6-20. On the HSI, when a tactical m
Page 302 and 303: 6-42. What control(s) the symbolbri
Page 304 and 305: 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: ASSIGNMENT 8Textbook Assignment:
Page 314 and 315: 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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Aviation Electronics Technician 1 - Historic Naval Ships Association

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