0.35 MACH “ TO LOW T ERRAIN”
E X WARNIN G
ARE A DUE TO PENDED AIRSPE ED
“TO LOW GEAR”
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8
MACH
This mode s activated upon clearing 700 feet AGL after takeoff. Below 0.35 Mach, “TOO LOW GEAR” is announced. Above 0.35 Mach, TOO LOW TERRAIN” is announced. Warning is inhibited below 50 feet.
INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
GROUND PROXIMITY WARNING SYSTEM WARNING ANNUNCIATION
MODE 4B - TERRAIN CLEARANCE (Descent in Wrong Configuration -Gear Down, Flaps Not in Landing Position)
PROXIMITY TO TERRAIN – FLAPS UP
1250
RADIO ALTITUDE – FEET
RADIO ALTITUDE – FEET
and then retracted, “TOO LOW GEAR” will be announced at 200 feet AGL if still retracted. Warning is inhibited below 50 feet and reverts to Mode 3 (with both gear and flaps down).
MODE 5 - DESCENT BELOW GLIDESLOPE
1250
1000
750
500
250
0
This Mode is activated upon clearing 700 feet
VISUAL INDICATION - GPWS light on. AGL after takeoff. Below 0.29 Mach, with the flaps AURAL/VOCAL ANNUNCIATION -not extended for landing, “TOO LOW FLAPS” is “TOO LOW FLAP” (Repeated in 0.75 announced. seconds interval cycle.)
Above 0.29 Mach, “TOO LOW TERRAIN” is
“TOO LOW TERRAIN” (Repeated inannounced. If gear is extended and then retracted 0.75 seconds interval cycle.)
“GL IDESLOP E”
1.3
1000
750
500
250
0
VISUAL INDICATION - BELOW G/S light on. AURAL/VISUAL ANNUNCIATION -“GLIDESLOPE”.
This mode warns of excessive low ILS glide slope deviation when aircraft is below 1000 eet radio altitude and a valid ILS frequency iisreceived. When the glideslope advisory
MD801630
1234
DOTS “FLY-UP
region is penetrated, a soft warning is given by illumination of the BELOW G/S light and voice annunciation “GLIDESLO PE”. As the altitude is decreased and the DOTS “FLY-UP” glideslope deviation is increased, the glideslope voice warning audio output level and repeat rate will increase.
INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
GROUND PROXIMITY WARNING SYSTEM WARNING ANNUNCIATION
MD-80 Rev. 12/01/00 #29 Continental Flight Manual
INSTRUMENTATION AND NAVIGATION – FUNCTIONAL SCHEMATIC
PITOT / STATIC SYSTEMS
INSTRUMENTATION AND NAVIGATION - FUNCTIONAL SCHEMATIC
CENTRAL AIR DATA COMPUTER / PITOT / STATIC INTERFACE
MD-80 Rev. 12/01/00 #29 Continental Flight Manual
INSTRUMENTATION AND NAVIGATION - FUNCTIONAL SCHEMATIC
NAVIGATION SYSTEMS
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(184)
