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2. Gear not  Aural/Vocal 
condition corrected or  down and  warning silenced 
warning deactivated.  locked, any  by pushing GEAR 
throttle fully  HORN OFF 
retarded,  button, provided 
air speed  flaps are set, but 
less than  at less than 26o. 
210 kts. 
STABILIZER IN MOTION *  1. Momentary horn sound for one second. (Sound starts between 0.5o to 1.0o of stabilizer movement and repeats every 0.5o of motion.)  None. (Stabilizer LONG TRIM indicator may be crosschecked.)  Horizontal stabilizer in motion. Movement is by action of the primary trim control.  Warning silenced when stabilizer is stopped.  Operate primary trim controls. 
2. Momentary horn sound starts after 0.5o to 1.0o of stabilizer movement  Horizontal stabilizer in motion. Movement is  Operate alternate trim controls. 
and repeats every 0.5o of stabilizer movement . “STABILIZER MOTION” voice warnings will sound when either the autopilot or a runaway trim motor moves the stabilizer more than 2o in 30 seconds and will continue to sound as long as stabilizer moves. Cycle continues until stabilizer movement ceases.  by action of the alternate trim control. 

* Vocal warning on some aircraft, other aircraft no vocal warning.
Aural/Vocal Warning and Caution Systems (Sheet 4)
WARNING INDICATED  AURAL/VOCAL WARNING CHARACTER  VISUAL INDICATION  CONDITION INDICATED  DEACTIVATE  TEST 
AUTO- (Activated during  Flashing red AP light  Autopilot  Press AP release  None. 
PILOT *  automatic landing mode only.) Warbling horn sound for one second, followed by word “AUTOPILOT” for one second, followed by warbling horn sound. Cycle continues until condition corrected.  on flight mode annunciators.  disengaged.  button on either control wheel 
OVER -SPEED *  Clacker sound for one second, followed by appropriate word for one second, followed by clacker sound for one second. Cycle continues until condition corrected.  MAX SPD WARN TEST switch. 
Word -“OVERSPEED”  None.  VMO/MMO exceeded.  Correct overspeed condition. 
Word - “SLAT  None.  280 KIAS  Correct 
OVERSPEED”  (Mach 0.57) exceeded with slats extended.  overspeed condition or retract slats. 
CABIN ALTITUDE *  Modulating horn (same as TAKEOFF WARNING and SPOILER/FLAP EXTENDED) for one second, followed by word “CABIN ALTITUDE” for one second, followed by modulating horn sound for one second. Cycle continues until condition is corrected or until five seconds when warning is automatically reset.  CABIN ALT light and MASTER WARNING lights.  Cabin altitude has exceeded allowable limit.  Reduce cabin altitude to 10,000 feet or below.  None. 
GROUND PROXIMITY WARNING  “SINK RATE, SINK RATE” “WHOOP WHOOP-PULL UP”  Red GPWS light.  Excessive sink rate.  Recover from condition indicated.  GND PROX WARN Switch TEST 
“TERRAIN-TERRAIN” “WHOOP WHOOP-PULL UP”  Red GPWS light.  Excessive terrain closure rate-airplane not in landing configuration. 

* Vocal warning on some aircraft, other aircraft no vocal warning.

MD-80
Continental
Rev. 12/01/00 #29 Flight Manual
Aural/Vocal Warning and Caution Systems (Sheet 5)
WARNING INDICATED  AURAL/VOCAL WARNING CHARACTER  VISUAL INDICATION  CONDITION INDICATED  DEACTIVATE  TEST 
“DON’T SINK, DON’T SINK”  Red GPWS light.  Altitude loss after takeoff.  Recover from condition indicated.  GND PROX WARN Switch TEST 
GROUND PROXIMITY WARNING (Continued)  “TOO LOW GEAR” “TOO LOW TERRAIN”  Red GPWS light.  Terrain clearance -Descending in wrong configuration - Gear up. 
“TOO LOW FLAP” “TOO LOW TERRAIN”  Red GPWS light  Terrain clearance -Descending in wrong configuration - Gear down, flaps not in landing position 
“GLIDESLOPE”  Amber BELOW G/S light.  Descent Below Glideslope. 
STALL WARNING *  Stall warning horn will sound for one second followed by word “STALL.” Cycle will continue until condition corrected.  Red STALL warning light.  Airspeed approaching stall condition for flap/slat configuration.  Correct stall condition.  STALL TEST Switch. 
Tactile warning by stick shaker. Both columns will vibrate simultaneously. 

* Vocal warning on some aircraft, other aircraft no vocal warning.
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