MD-80
Continental
Rev. 12/01/00 #29 Flight Manual
EMERGENCY EXITS AND EQUIPMENT – AFT ENTRANCE DOOR
Effective For Some Aircraft
EMERGENCY EXITS AND EQUIPMENT – AFT ENTRANCE DOOR
Effective For Some Aircraft
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual
EMERGENCY EXITS AND EQUIPMENT – TAILCONE JETTISON /
WALKWAY
Tailcone Jettison System Safety Decal Install On Airplanes With
Service Bulletin 52-175 Incorporated Or Production Equivalent
EMERGENCY EXITS AND EQUIPMENT – TAILCONE SLIDE
(Effective For S9ome Airplanes)
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual
EMERGENCY EXITS AND EQUIPMENT – TAILCONE SLIDE
(Effective For Some Aircraft)
WARNING AND CAUTION SYSTEMS
The warning and caution systems provide aural, visual, and / or tactile indications to warn of potentially unsafe operating conditions or airplane configurations and system malfunctions. Indications are generated by a Central Aural Warning System (CAWS), a visual warning and caution system, or a tactile warning system.
Central Aural Warning System (CAWS)
Aural warnings generated by a central control unit provide warning discrimination by means of varying the pitch, duration, and repetitive frequency of the aural signal. CAL aircraft are equipped with voice warnings in addition to the aural tones.
Additional information regarding the operation and testing of CAWS generated signals is provided in the aural / vocal warning and caution system section of this chapter and in applicable system chapters.
A CAWS FAIL annunciator light illuminates when the CAWS is powered but has failed a self test. Caution: if any CAWS c.b. is pulled, certain alerts are disabled – but the CAWS FAIL light may remain extinguished.
Visual Warning and Caution System
Visual warning and caution indications are provided in the engine fire handles and by annunciator lights. Where practical, individual lights are located adjacent to or in the controls or indicators for the respective system. Lights pertaining to systems with controls or indicators in more than one area are located on the forward overhead panel. The red master warning lights come on to indicate a condition that requires immediate attention. The amber master caution lights come on to indicate a condition that requires less than immediate attention.
Master Warning and Master Caution lights come on concurrently with their respective individual warning and caution lights and can be reset for subsequent indications. The individual warning or caution lights will remain on until the condition has been corrected. Certain individual amber caution lights are considered advisory and do not cause the master caution lights to come on.
Continental
Rev. 12/01/00 #29 Flight Manual
Tactile Warning System
In addition to the stall warning lights, the dual stall warning system actuates a stick shaker to warn of an impending stall. Refer to Instrumentation and Navigation chapter.
APU Fire Warning Horn
An aural warning for APU fire is provided by an exterior horn located adjacent to the APU ground control panel in the tailcone. Refer to Fire Warning and Protection chapter for detailed description.
ANNUNCIATOR PANEL, MASTER WARNING AND CAUTION LIGHTS
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual
Aural/Vocal Warning and Caution Systems (Sheet 1)
WARNING INDICATED AURAL/VOCAL WARNING CHARACTER VISUAL INDICATION CONDITION INDICATED DEACTIVATE TEST
ENGINE Continuous bell L, or R ENG FIRE Fire or Aural/vocal warning LOOPS
FIRE * sound for one second, followed by handle(s); respective LOOPS A and B overheat in engine silenced by pushing FIRE BELL OFF TEST switch (A and
words “FIRE LEFT lights; and FIRE nacelle. button or pulling the B).
ENGINE” or “FIRE DETECTOR LOOP fire handle out.
RIGHT ENGINE” for light, and MASTER MASTER
one second, followed CAUTION lights. CAUTION lights
by continuous bell reset by pushing
sound for one light cap.
second. Cycle Remaining visual
continuous until indications will
condition corrected or remain on until fire
warning deactivated. is extinguished.
APU FIRE * Continuous extremely APU FIRE and FIRE Fire or MASTER LOOPS
loud exterior horn. Cockpit indications DETECTOR LOOP lights, MASTER overheat in APU WARNING / CAUTION light TEST switch (A and
are intermittent horn sound for one second, followed by words “APU FIRE” for one second, followed by intermittent horn sound for one second. The words “APU FIRE” will automatically cancel after three (3) cycles. WARNING / CAUTION lights, APU LOOP A and B lights, and APU FIRE light (on external APU ground control panel). compart-ment. reset by pushing light caps. The APU FIRE, FIRE DETECTOR LOOP and APU loop lights and external fire warning horn will stay on until fire is extinguished. B).
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