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NOTE:
It is recommended that Air Start Ignition be selected
ON for landing on a runway with standing water, slush
or snow.
NOTE:
Recommended Þnal approach speed is VREF plus 10
knots. If gusty wind conditions exist, add ½ of the
difference between the steady state winds and gust
(maximum of additional 10 knots of gust additive).
VREF will still be the target speed at the threshold.
03-05-60: EGPWS Alerts
1. EGPWS CAUTION:
When an EGPWS CAUTION occurs, adjust the airplane ßight path until the
CAUTION alert ceases.
2. EGPWS WARNING:
If an EGPWS WARNING occurs, follow the vertical escape maneuver procedure
described following this paragraph 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 SERVEAS
ASITUATIONALAWARENESS TOOLONLYAND MAY
NOT PROVIDE THE ACCURACY AND/OR FIDELITY
ON WHICH TOSOLELY BASE TERRAINAVOIDANCE
MANEUVERING DECISIONS.
VERTICAL ESCAPE MANEUVER PROCEDURE:
1. Autopilot...............................................................................DISCONNECT
2. Power .......INCREASE TO MAXIMUM THRUST (GO-AROUND POWER)
3. Pitch Attitude ..ROTATE AT 3° TO 4° PER SECOND TO INCREASE TO
HIGHEST POSSIBLE VALUE
A pitch attitude of 25 degrees has been demonstrated on the GIV at
maximum landing weight with ßaps DOWN (39¡).
WHEN STICK SHAKER IS ENCOUNTERED OR AS VREF IS APPROACHED:
4. Pitch Attitude................REDUCE PITCH RATE/ANGLE OF ATTACK TO
INTERCEPT VREF -20 KCAS
5. Flaps / Landing Gear ..DO NOT RETRACT UNTIL SAFE CLIMBOUT IS
ASSURED
OPERATING MANUAL
EXPANDED NORMAL PROCEDURES 03-05-00
Page 3
May 30/02
Revision 7
03-05-70: TCAS II Flight Procedures
1. Upon Initiation of a Resolution Advisory (RA):
Upon initiation of a Resolution Advisory (RA), the pilot ßying should focus attention
on ßying the commanded maneuver. The aircraft 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.
2. Compliance With a TCAS II RA:
Compliance with a TCAS II 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 aircraft, obvious TCAS system failure, etc.).
WARNING
NON-COMPLIANCE WITH A CROSSING RA BY
ONE AIRCRAFT 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
INTRUDERAIRCRAFT,ANDANY CHANGE INVERTICAL
SPEED THAT DOES NOT COMPLY WITH THE
RA MAY NEGATE THE EFFECTIVENESS OF THE
OTHER AIRCRAFTÕS COMPLIANCE WITH ITS RA.
NOTE:
The consequences of not following an RA may result
in additional RAs in which aural alerts and visual
annunciations may not agree with each other.
03-05-80: All Engines Operating Go-Around Procedure
1. TO / GA Button ..........................................................................................PRESS
NOTE:
The autothrottle system, 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)
OPERATING MANUAL
03-05-00 EXPANDED NORMAL PROCEDURES
Page 4
May 30/02
Revision 7
ONCE GO-AROUND ATTITUDE IS ESTABLISHED:
4. Flaps ..................................................................................................................20°
WHEN POSITIVE RATE OF CLIMB IS ATTAINED:
5. Landing Gear.....................................................................................................UP
WHEN VREF +20 IS ATTAINED:
6. Flaps...................................................................................................................UP
Maintain adequate speed for stall margin.
7. Power.............................................................................................AS REQUIRED
　
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