Mark V and Mark VII EGPWS Pilot’s Guide 
Operational Procedure  060-4241-000 
56  Rev H, August 2011 
Warning 
Alerts 
Note:  Navigation must not be based on the use of the Terrain 
Awareness and Alerting Display (TAD). 
Below Glideslope alerts consist of “soft” and “hard” alerts 
based on the degree of glideslope deviation and altitude. 
Respond to these alerts as necessary to correct the aircraft’s 
flightpath back to the Glideslope centerline or perform a 
Advisory callouts being advisory in nature are used to 
announce an event or condition (e.g., “Minimums”, 
"RunwayXX" - if RAAS enabled). 
Response to these callouts should be in accordance with 
standard operating procedures. 
Windshear 
Caution 
 
This alert generally occurs due to increasing performance 
windshear conditions (i.e., increasing headwind, decreasing 
tailwind, and/or updraft). This alert is generally considered 
advisory in that the crew response is to be alert to the 
possibility of subsequent significant airspeed loss and down 
itions. Coupled with other weather factors, the 
Windshear Caution should be considered in determining the 
advisability of performing a go-around. 
Wind and gust allowances should be added to the approach 
speed, increasing thrust if necessary. It may be necessary to 
disengage autopilot or auto-throttle. Avoid getting low on the 
approach glidepath or reducing the throttles to idle. 
Windshear 
Warning 
 
When a Windshear warning occurs, the following procedures 
should be followed: 
1. Immediately initiate the Windshear escape maneuver in 
accordance with established Windshear procedures. 
2. 
Aggressively apply maximum rated thrust, disengage 
autopilot and/or auto-throttle if necessary. 
3. Rotate smoothly to the go-around/take-off pitch attitude, 
allowing airspeed to decrease if necessary. Maintain wings 
level. Do not retract flaps or landing gear. 
4. If the aircraft continues to descend, increase pitch attitude 
smoothly and in small increments, bleeding air speed as 
necessary to stop descent. Use Stall Warning onset (stick 
shaker) as the upper limit of pitch attitude. 
5. Maintain escape attitude and thrust and delay retracting 
flaps or landing gear until safe climb-out is assured. 
Note: 
Engine overboost should be avoided unless the 
airplane continues to descend and airplane safety is in doubt.