Chapter Three Review - Cont'd

STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS

CHAPTER THREE

38. The engine fire protection system includes ___________ and ___________ detection

systems, as well as a __________________________.

39. Should a fire or overheat condition occur, the rise in temperature is detected by the

____________________, which illuminates the respective left or right fire warning light and

_________________________________________.

40. The fire detection system is tested using the _____________________________ located on

the overhead panel.

41. Once the system is validated the blue _________ light adjacent to the rotary switch will

illuminate.

42. Both fire warning switchlights illuminate in the event of an engine fire. (T/F)

43. Crewmembers are able to direct the discharge of either extinguisher bottle, or both bottles,

to a selected engine. (T/F)

44. The discharge of a single fire extinguisher bottle will not blow the discharge indicator

indicating a discharged system. (T/F)

45. ________________________ act as annunciators for engine fire detection.

46. What happens when the engine fire switchlight is pressed?

ENGINES

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