737 Flight Crew Operations Manual
Warning Systems -
System Description
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
15.20.30 D6-27370-866-EGP
Tail Skid
The tail skid assembly consists of a cartridge assembly, tail skid, fairing (skirt) and
shoe. The fairing provides an enclosure for the actual tail skid structure. The shoe
is fitted to the bottom of the fairing.
AURAL ALERTS
VERTICAL
RESTRICTIONS/MANEUVER
MONITOR VERTICAL SPEED Present pitch attitude is outside the RA
pitch command area. Keep pitch
attitude away from red area.
MAINTAIN VERTICAL SPEED,
MAINTAIN
MAINTAIN VERTICAL SPEED,
CROSSING MAINTAIN
CLIMB, CLIMB Climb at the displayed pitch
DESCEND, DESCEND Descend at the displayed pitch
LEVEL OFF, LEVEL OFF Reduce climb or descent rate to 0 feet
per minute.
CLIMB, CROSSING CLIMB,
CLIMB, CROSSING CLIMB
Climb at displayed pitch. Airplane
climbs through traffic’s altitude.
DESCEND, CROSSING DESCEND
DESCEND, CROSSING DESCEND
Descend at displayed pitch. Airplane
descends through traffic’s altitude.
INCREASE CLIMB,
INCREASE CLIMB
Increase climb rate from initial pitch
attitude.
INCREASE DESCENT,
INCREASE DESCENT
Increase descent rate from initial pitch
attitude.
CLIMB – CLIMB NOW,
CLIMB – CLIMB NOW
Reversal maneuver from initial
descent RA.
DESCEND – DESCEND NOW,
DESCEND – DESCEND NOW
Reversal maneuver from initial climb
RA.
CLEAR OF CONFLICT RA encounter terminated. Maneuver
guidance no longer displayed.
September 15, 2016
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