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CAUTION: DO NOT MOVE REVERSE THRUST LEVERS OUT OF
THE FORWARD THRUST POSITION PRIOR TO TOUCHDOWN.
NOTE: Maintain a minimum 67% HP RPM until landing.
6. Air Start Ignition .......................................................AS REQUIRED
NOTE: It is recommended that Air Start Ignition be selected ON for
landing on a runway with standing water, slush, or snow.
NOTE: Recommended final approach speed is VREF plus 10 knots. If gusty
wind conditions exist, add ½ of the difference between the steady state wind
and gust (maximum of additional 10 knots of gust additive). VREF will still be
target speed at the threshold.
END
EGPWS Alerts AFM 2-05-60
EGPWS Caution:
When an EGPWS CAUTION occurs, adjust the airplane flight path until
the CAUTION alert ceases.
EGPWS Warning:
If an EGPWS WARNING occurs, follow the escape maneuver steps
below until all alerts cease. Unless operating in Visual Meteorological
Conditions (VMC) and / or the pilot determines based on all available
information, that turning in addition to the vertical escape maneuver is
the safest course of action, only the vertical escape maneuver is
recommended.
CAUTION: THE TERRAIN DISPLAY IS INTENDED TO SERVE AS A
SITUATIONAL AWARENESS TOOL ONLY, AND MAY NOT PROVIDE THE
ACCURACY AND / OR FIDELITY ON WHICH TO SOLELY BASE TERRAIN
AVOIDANCE MANEUVERING DECISIONS.
Vertical Escape Maneuver:
1. Autopilot....................................................................DISCONNECT
2. Power .....................MAXIMUM THRUST (GO-AROUND POWER)
3. Pitch Attitude ................................ROTATE TO 3 TO 4 DEGREES
PER SECOND TO ATTAIN HIGHEST POSSIBLE VALUE
A pitch attitude of 25 degrees has been demonstrated on the GIV
at maximum landing weight with flaps DOWN (39°).
Continued on next page →
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NE - 4 May 30/02
EGPWS Alerts, ctd… AFM 2-05-60
When stick shaker is encountered, or as VREF is approached:
4. Pitch Rate / Angle Of Attack.............................................................
....................................REDUCE TO INTERCEPT VREF -20 KCAS
5. Flaps / Landing Gear........................................................................
.......DO NOT RETRACT UNTIL SAFE CLIMB-OUT IS ASSURED
END
TCAS II Flight Procedures AFM 2-05-70
Upon initiation of an RA, the pilot flying should focus attention on flying
the commanded maneuver. The airplane should be smoothly
maneuvered to comply with the TCAS command and to promptly
return to ATC clearance when the “CLEAR OF CONFLICT” message
is received.
Compliance with a TCAS II resolution advisory (RA) is necessary
unless the pilot considers it unsafe to do so, or unless the pilot has
better information about the cause of the RA and can maintain safe
separation (e.g., visual acquisition of and safe separation from a
nearby airplane, obvious TCAS system failure, etc.).
WARNING: NON-COMPLIANCE WITH A CROSSING RA BY ONE
AIRPLANE MAY RESULT IN REDUCED VERTICAL SEPARATION;
THEREFORE, SAFE HORIZONTAL SEPARATION MUST ALSO BE
ASSURED BY VISUAL MEANS.
CAUTION: ONCE A NON-CROSSING RA HAS BEEN ISSUED, SAFE
OPERATION COULD BE COMPROMISED IF CURRENT VERTICAL SPEED
IS CHANGED, EXCEPT AS NECESSARY TO COMPLY WITH THE RA.
THIS IS BECAUSE TCAS II-TO-TCAS II COORDINATION MAY BE IN
PROGRESS WITH THE INTRUDER AIRPLANE, AND ANY CHANGE IN
VERTICAL SPEED THAT DOES NOT COMPLY WITH THE RA MAY
NEGATE THE EFFECTIVENESS OF THE OTHER AIRPLANE’S
COMPLIANCE WITH ITS RA.
NOTE: The consequences of not following an RA may result in
additional RAs in which aural alert and visual annunciations may not
agree with each other.
END
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NE - 5
All Engines Operating Go Around Procedure AFM 2-05-80
In the event that an approach is discontinued, proceed as
follows:
1. TO / GA Button.................................................................... PRESS
NOTE: The autothrottle, if engaged, automatically advances to
go-around thrust, and the autopilot, if engaged, will disengage.
2. Airspeed ..............................................................VREF +10 KNOTS
3. Power ..............................GO AROUND THRUST (IF REQUIRED)
4. Flaps....... 20° ONCE GO AROUND ATTITUDE IS ESTABLISHED
5. Landing Gear....................................................................................
......RETRACT WHEN POSITIVE RATE OF CLIMB IS ATTAINED
6. Flaps........................................ UP WHEN VREF +20 IS ATTAINED
　
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