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Two continuous element fire detector cables for each engine, are adjacent to the engines. They are wired into a closed series loop connected to a control unit that lights warning lights in the pilot's compartment in case of a fire. The fire detector right or left FIRE warning light illuminates if a temperature of approximately 765°F occurs in the corresponding engine compartment. The aft fuselage overheat sensing elements are routed in vertical recesses of the skin fairing on each side of continuity is checked and all four FIRE warning lights should go on. The system operates on 28 vac from the dc primary bus through two circuit breakers marked FIRE DET and two marked FIRE DET CONT On the dc circuit breaker panel. 219.The warning.lights will illuminate when temperature in the accessory gearbox or firewall area reaches 410°F, or if the hot section area temperature reaches Test Switch Panel 890°F. A fire control unit, installed for each fire detection system, Engine fuel pump warning light 33. Turnaodhank indicator 5. Inflight refueling probe light 19. Fuel Iour level warning light 34. Fuel quantity test switch 4. WingwheeIsdroop warning light 2:}, Course indicator 35. Rocket pack fire light 5.Angle o'l Attaclt Indicator Ignition Warning Light Tachometer AirspeedMach Number Indicator Low Level Fuel Radar Tracking Indicator Light Course lndicatnr—lDZSMARN Rate of Climb Indicator Fire warning Light Longitudinal Trim The large differences in performance.between night and day add support, and some level of quantification, to the idea that the most significant improvement to be made in warning lights may be adopting different light levels for night and day .What fire detection means, if any, is provided for the lower cargo compartment? 1—No equipment is installed to detect a Class D compartment fire. 2—The fire bell rings, but no warning light illuminates. 3—Flames can be observed through the 7 Gil Pressure Gage B. Tokealt [Trim] Position Indicator Light '9'. Exhaust Temperature Gage 10. Fuel Prossum Gage" 1 1 . Fire—warning Lights 1 2. Standby Campus: 13. Fire—wurning Light Test Button 14. Standby Compass light Switch Landing gear down indicator lights.(3) Illuminated. 42. Keylock switch ON. *43. Fire detection system Test. Verify warning horn sounds; simultaneously the red FAULT WARN light flashes and LH and RH FIRE WARN lights illuminate in