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The ABS takeoff mode is armed by selecting T.O. on the AUTO BRAKE selector switch and placing the ARM/DISARM switch in the ARM position. The speedbrake/spoilers lever must be retracted and flaps must be selected to less than 26 degrees.
Takeoff aural warning horn will sound if either spoilers or ABS is armed and the other system is not armed. The ABS takeoff mode is activated during a rejected takeoff upon deployment of ground spoilers. If a rejected takeoff is initiated below 70 knots, the ABS reverts to landing mode operation and MIN braking is applied. At speeds greater than 70 knots, maximum dual-system automatic braking is applied immediately without any time delay. Pilot takeover can be initiated by either advancing throttle levers 1 or 2 beyond +22 degrees of travel or by depressing the brake pedals beyond 25 percent of travel. Both conditions will cause the ABS to disarm, the ARM/DISARM switch will fall to the disarm position, and the ABS lights on the glareshield will illuminate.
Note:  If spoilers fail to deploy automatically, manual spoiler deployment will activate ABS.
An ABS malfunction will cause the system to automatically disarm. The ARM-DISARM switch will fall to the DISARM position, and the ABS lights, AUTO BRAKE FAIL light, and the MASTER CAUTION lights will illuminate. To rearm the ABS system after it has automatically disarmed, the AUTO BRAKE selector switch must be placed to the OFF position and then back to the deceleration setting and the ARM/DISARM switch must be placed to the ARM position. If the fault has cleared, the system will rearm.
Continental
Rev. 12/01/00 #29 Flight Manual
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LANDING GEAR - MAJOR COMPONENT LOCATION
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

LANDING GEAR - MAJOR COMPONENT LOCATION
TAIL BUMPER AND COMPRESSION INDICATOR

LANDING GEAR - MAIN GEAR LATCH VISUAL POSITION CHECK
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

LANDING GEAR - CONTROLS AND INDICATORS GEAR HANDLE /
INDICATORS

LANDING GEAR - CONTROLS AND INDICATORS
BRAKES / NOSEWHEEL - STEERING / TAXI SPEED

MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

LANDING GEAR - CONTROLS AND INDICATORS - BRAKE ANTI-SKID

LANDING GEAR - CONTROLS AND INDICATORS
AUTOMATIC BRAKE SYSTEM

LANDING GEAR - CONTROLS AND INDICATORS
AUTOMATIC BRAKE SYSTEM

(Installed On Some Aircraft)
MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

LANDING GEAR - GROUND SHIFT MECHANISM FUNCTIONS
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ICE AND RAIN PROTECTION
TABLE OF CONTENTS
ICE AND RAIN PROTECTION..............................................................1
General............................................................................................ 1
Airfoil Ice Protection ........................................................................ 1
Engine Ice Protection ...................................................................... 2
UWAI System Description...............................................................3

Sec. 15 TOC-2
MD-80 Rev. 12/01/00  #29 Continental Flight Manual
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MD-80  Sec. 15 Page 1 
Flight Manual  Continental  Rev. 12/01/00  #29 
ICE AND RAIN PROTECTION 

General
The airplane ice protection systems employ hot air and electrical resistance heating for anti-icing and anti-fogging functions.  Rain removal is accomplished by chemical repellent and electrically operated windshield wipers.  Chemical repellent to be removed and replaced with permanent coatings on windshields.
Heated air for anti-icing of wing leading edge slats, fuselage strakes, air conditioning ram air scoop inlet, and for de-icing the leading edge of the horizontal stabilizer, is supplied by engine bleed air.  A crossfeed duct system permits airfoil heat to be supplied from either or both engines.
　
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