CDC 2A354P

Which F-15C/D APG-70 radar set component combines the functions of the APG-63 receiver and radio frequency oscillator (RFO) into one LRU

Which F-15C/D APG-70 radar air-to-air search mode uses the "intermediate" PRF to detect targets in intermediate-range and short-range

Which F-15C/D APG-70 radar air-to-ground mode does the pilot use prior to making a bomb run

1. (001) On the F–15 APG–63 radar system, what did engineers put in place to protect the receiver from damage due to high-powered transmissions?

001) What types of pulse repetition frequency (PRF) does the F–15 APG–63 radar system primarily use for transmission?

(001) On the F–15 APG–63 radar system, which component provides manual control of radar set power, operating modes, and mode parameters?

(001) On the F–15 APG–63 radar system, which component process clutter rejection?

001) On the F–15 APG–63 radar system while in-flight, the waveguide pressure has fallen below how many pounds per square inch absolute (PSIA) if the ASP 25 latches orange?

001) On the F–15 APG–63 radar system, while performing an operate initiated built in test (IBIT) on the ground, what is displayed if the radar thinks it is airborne and transmits?

(001) On the F–15 APG–63 radar system, which radar mode is available in all ranges except 10 nautical miles?

001) Which F–15 APG–63 radar mode is the primary air-to-air (A/A) search mode and is used for detection and acquisition of both closing- and opening-rate airborne targets?

10. (001) Which F–15 APG–63 radar scan mode can maintain up to 10 target track files while continuing to detect and display up to 18 more (half-intensity) observation targets?

11. (001) On the F–15 APG–63 radar system during track, which medium range missile (MRM) range symbol indicates the range at which the target cannot ―turn and run‖ to evade your missile?

12. (001) Which F–15 APG–63 radar window display is a four-character numeric readout that moves along the left side of the display next to the antenna (031) elevation caret?

13. (002) The F–15C/D APG–70 radar set is made up of how many major line replaceable units (LRU)?

14. (002) Which F–15C/D APG–70 radar set component performs the same role as the APG–63 radar’s 541?

18. (003) Which F–15E APG–70 radar set component establishes the basic operating radio frequency (RF) for the transmitter?

19. (003) Which F–15E APG–70 air-to-ground (A/G) radar mode provides a slant range measurement used for target altitude determination, for target designation, or for position updates?

20. (003) Which F–15E APG–70 A/G radar mode are the displays and functions are limited to the left multipurpose display (MPD) in both cockpits?

21. (003) An automatic sequence of tests run in a non-interference manner any time the F–15E APG–70 radar is on is called

22. (004) On the F–15 APG–63(V)1 radar, which component stores the radar operational flight program (OFP) and protects the radar from overheating?

23. (004) Which F–15 APG–63(V)1 radar air-to-ground (A/G) mode provides general navigation?

24. (005) Which F–15E Combined Altitude Radar Altimeter (CARA) system component generates the transmitted signal and processes the received reflections to measure altitude?

25. (005) What is the full altitude range that the F–15E Combined Altitude Radar Altimeter (CARA) system accurately measures?

26. (005) Which component provides the F–15E Combined Altitude Radar Altimeter (CARA) system symbology and video to the multipurpose display system?

27. (006) What is the primary master mode on the A through D models of the F–15?

28. (006) The A through D models of the F–15 flight director adapter (FDA), which interfaces the central computer (CC) with the navigation systems, is part of what system?

29. (006) What unit is the primary source of aircraft pitch, roll, heading, acceleration, velocity, and present position information?

30. (006) On the F–15, what is the backup arrangement of the H009 MUX buses?

31. (006) On the F–15, each H009 MUX bus channel has two twisted shielded pairs of wires. One pair carries 1 Mb/sec digital data to/from peripherals. What does the other pair carry?

32. (006) On F–15A through D model aircraft, the avionics 1553 MUX bus consists of

33. (006) On the F–15, what is the purpose of MUX bus resistor assemblies?

34. (006) On the F–15, the central computer (CC) performs a MUX test to determine whether faulty communication is the result of a faulty MUX bus or a

35. (006) Which of the overload warning system (OWS) display data is recorded in flight by the central computer?

36. (006) The very high-speed integrated circuit (VHSIC) central computer operational flight program (OFP) consists of how many program functions?

37. (006) Which operational flight program (OFP) function handles tactical air navigation (TACAN), navigation (NAV), and instrument landing system (ILS) steer mode processing for display on the horizontal situation indicator (HSI)?

38. (006) Which operational flight program (OFP) function handles the processing for the overload warning system (OWS)?

39. (006) When using a central computer (CC) logic diagram, what does the return point of a routine indicate?

40. (006) How are memory data addresses and outputs displayed on the navigation control indicator (NCI)?

41. (006) When auditing the central computer using the multipurpose color display (MPCD), the preferred readout format is

42. (007) The F–15 overload warning reset switch is used with the navigation control indicator (NCI) to clear overload conditions from the memory of which component?

43. (007) Which F–15 overload warning system (OWS) component processes the OWS information displayed on the multiple indicator control panel (MICP), heads-up display (HUD), and is heard in the headset?

44. (007) Which F–15 component sends signals telling the central computer (CC) whether wing tanks and/or conformal fuel tanks (CFT) are loaded on the aircraft?

45. (007) If the F–15 programmable signal data processor or the overload warning system (OWS) stops working, where does the central computer (CC) receive current G data?

46. (007) The F–15 central computer (CC) sends overload warning system (OWS) information to which of the below line replaceable units (LRU)?

47. (007) What is displayed in window 8 on the F–15 HUD if the overload warning system (OWS) is not operational?

48. (008) When there are no detected failures, which mode of operation is the F–15E Advanced Display Core Processor (ADCP) operating in when power is applied to the aircraft?

49. (008) Which mode of operation will the F–15E Advanced Display Core Processor (ADCP) operate when a simple failure is detected that does not reduce functionality or when a severe failure occurs and causes a main and essentials bus split?

50. (008) Which mode of operation will the F–15E Advanced Display Core Processor (ADCP) operate when it detects a loss of 115 volts alternating current (VAC) and both generators are off line?

50. (008) Which mode of operation will the F–15E Advanced Display Core Processor (ADCP) operate when it detects a loss of 115 volts alternating current (VAC) and both generators are off line?