GND PROX WARN Switch......................................................OVRD

During landing flare, do not reduce approach thrust until landing
flare has been initiated and sink rate has been reduced.
* * * *
MD-80 Sec. 3 Page 55
Flight Manual Continental Rev. 05/15/95  #23

STALL INDICATION FAILURE LIGHT ON

Note: One stick shaker or stall recognition system may be activated.
IF Stall Warning Indications Are Active:

Airspeed and Attitude..............................................................CHECK

Ensure that airspeed and attitude are adequate for existing configuration.
STALL TEST Switch.................................................SYS 1 OR SYS 2

Moving the STALL TEST switch to SYS 1 or SYS 2 will dim the STALL lights.
CAPTAIN And FIRST OFFICER STALL WARNING Circuit Breakers (X & Z-23).......................PULL OPEN
OR
STALL TEST Switch.....................................................................OFF

CAPTAIN And FIRST OFFICER STALL WARNING Circuit Breakers (X & Z-23)...................................RESET ONE AT A TIME
Identify and isolate the malfunctioning system. Leave the circuit breaker pulled for the malfunctioning system. Confirm operation of the working system by testing. Continue flight with remaining system operating.

* * * *
IF Stall Warning Indications Are Not Active:
Both Systems ................................................................................TEST

IF One System Test Is Unsuccessful:

CAPTAIN Or FIRST OFFICER STALL WARNING Circuit Breaker (X Or Z-23) (Affected System)..................................PULL OPEN
OR
Continue flight with the failed system deactivated.
* * * *
Both Systems Test Successful:
Continue normal operation. A false indication has occurred.

* * * *

Sec. 3 Page 56 MD-80
Rev. 08/01/98 #27 Continental Flight Manual

STICK SHAKER ON
(OTHER STALL INDICATIONS NOT ACTIVE)

CAPTAIN’S and FIRST OFFICER’S STALL WARNING Circuit Breakers (X & Z-23)............................PULL OPEN
CAPTAIN’S STALL WARNING Circuit Breaker (X-23) ........... RESET

IF  Stick Shaker is Off: 
OR  Continue normal operation.  * * * * 
IF  Stick Shaker is On: 
CAPTAIN’S STALL WARNING Circuit Breaker (X-23) .................................................. PULL OPEN 
FIRST OFFICER’S STALL WARNING Circuit Breaker (Z-23)............................................................ RESET 

UNSCHEDULED AUTOMATIC SLAT EXTENSION

Note:  Automatic slat extension will occur only if FLAP/SLAT handle is at settings from 0° / T.O. to 13° / T.O. EXT.
Caution: Do not exceed 240 KIAS (fully extended slat limit speed). Do
not move FLAP/SLAT handle until safe altitude has been attained. 
IF  After Takeoff: 
FLAP / SLAT Handle ............................................................UP / RET 
IF  On Approach For Landing: 
FLAP / SLAT Handle .................................................. 15.
/ T.O. EXT 
IF  SLAT AUTO / DISAGREE Lights Are Off: 
Continue normal operation. 

 * * * * 
IF  SLAT AUTO / DISAGREE Lights Are On: 
Do not exceed 240 KIAS. 
* * * * 

MD-80 Flight Manual  Continental  Sec. 3 Page 57 Rev. 05/15/95  #23 
FUEL 
AUX FUEL PUMP PRESS LOW LIGHT ON WITH FUEL REMAINING IN AUX TANK 

AUX TRANS Pump Switches (Affected Tank) ............. BOTH AUTO

IF Fuel Transfer is Normal:

Resume normal operation.
* * * *
OR

IF Fuel Transfer is Not Normal:
AUX TRANS Pump Switches (Affected Tank)... HOLD IN TEST
IF Fuel Transfer is Normal:

OR
Continue to hold switches in TEST until tank is empty.
* * * *

IF Fuel Transfer is Not Normal:
IF FWD AUX Tank is Affected:

The remaining fuel in the forward aux tank is unusable.  If CG at takeoff was 7% MAC or more, all aft aux fuel may be used if needed using normal speeds and configurations. If CG at takeoff was less than 7% MAC and aft aux fuel must be used, land with flaps 40. and increase approach and landing speeds by 10 KIAS.
* * * *
OR

IF AFT AUX Tank is Affected:
The remaining fuel in aft aux tank is unusable.  Fuel in forward aux tank may be used if required to complete the flight.
* * * *
Sec. 3 Page 58 MD-80
Rev. 05/15/95 #23 Continental Flight Manual

AUX TANK - PREMATURE TRANSFER OF FUEL

AUX TRANS Pump Switches ........................................................ OFF

- - WHEN CENTER TANK QUANTITY DEPLETES TO 13,000 LBS - -
　
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