(a)  ON PASSENGER AIRPLANES; the overhead crew rest area is monitored for smoke particles or equivalent contaminants by smoke sensors. The smoke detectors are connected to modular avionic & warning electronic assembly and electronics rack E2-5. The flight crew is notified by the master fire light, fire bell and warning EICAS message. The smoke detector unit provides an aural warning to alert cabin attendants in event of lavatory fire. The smoke detection system requires power from the airplane 28-volts dc bus 4.

 (6)  
Zone B Crew Rest Area Smoke Detection (When Installed) (26-14-30)

 (a)  ON AIRPLANES WITH ZONE B CREW REST SMOKE DETECTION; the crew rest area is monitored for smoke particles or equivalent contaminants by smoke sensors. The smoke detectors are connected to modular avionic & warning electronic assembly and electronics rack E2-5. The flight crew is notified by the master fire light, fire bell and warning EICAS message. The smoke detector unit provides an aural warning to alert cabin attendants in event of lavatory fire. The smoke detection system requires power from the airplane 28-volts dc bus 4.
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747-400
MAINTENANCE MANUAL

 (7)  
Zone F Crew Rest Area Smoke Detection (When Installed) (26-14-40)

 (a)  ON AIRPLANES WITH ZONE F CREW REST SMOKE DETECTION; the crew rest area is monitored for smoke particles or equivalent contaminants by smoke sensors. The smoke detectors are connected to modular avionic & warning electronic assembly and electronics rack E2-5. The flight crew is notified by the master fire light, fire bell and warning EICAS message. The smoke detector unit provides an aural warning to alert cabin attendants in event of lavatory fire. The smoke detection system requires power from the airplane 28-volts dc bus 4.

 (8)  
Aft Upper Deck Crew Rest Area Smoke Detection (When Installed) (26-14-50)

 (a)  ON FREIGHTERS; the crew rest area is monitored for smoke particles or equivalent contaminants by smoke sensors. The smoke detectors are connected to modular avionic & warning electronic assembly and electronics rack E2-5. The flight crew is notified by the master fire light, fire bell and warning EICAS message. The smoke detector unit provides an aural warning to alert cabin attendants in event of lavatory fire. The smoke detection system requires power from the airplane 28-volts dc bus 4.

 (9)  
Business Center Smoke Detection System (26-14-70)(When installed)

 (a)  The business center on the upper deck is monitored for presence of smoke or equivalent contaminants by a smoke detector unit. A smoke detector unit provides an aural warning to alert cabin attendants in event of a lavatory fire. The smoke detection system requires power from the airplane 28-volts dc bus 2 and
 4.

 (10)
 APU Fire Detection (26-15-00)

 (a)  The APU fire detection circuit is similar to that of the engine circuit, using two continuous dual-element sensors. The APU fire detection circuit has the addition of a control panel in the right-hand body gear wheel well. This panel has an APU fire warning horn to notify the ground service crew of an APU fire, and also has a red fire light and fire extinguishing controls. The flight crew will be notified of fire and fault condition by master fire warning light, fire bell, warning, advisory, and status EICAS messages.

 (11)
 Lower Cargo Compartment Smoke Detection (26-16-00)

 (a)  The forward lower cargo compartment has four (eight on Freighters) smoke detectors, and aft compartment has four smoke detectors (eight on Freighters). Each smoke detector has a beacon lamp which supplies a smoke (fire) indication to flight crew when smoke is present in the air. The system can be tested by a test switch on the P5 pilot's overhead panel. The flight crew will be notified of fire and fault condition by master fire light, fire bell, warning, and status EICAS messages.
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 26-10-00
 ALL  ú ú 05 Page 5 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
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