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 - - 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：MD-80 Flight Manual 麦道80飞行手册 1(80)
