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3. Nutcracker........................................................................................................................TEST
CAUTION: DO NOT ARM GROUND SPOILERS IF NUTCRACKER SWITCH TEST IS
UNSUCCESSFUL.
4. Ground Spoilers ...........................................................................................................ARMED
5. Flaps........................................................................................................ SET FOR LANDING
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 1/2 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.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-34 FAA APPROVED
31 May 2000
2-05-60: EGPWS Alerts:
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/OF FIDELITY ON WHICH TO SOLELY BASE TERAIN AVOIDANCE
MANEUVERING DECISIONS.
VERTICAL ESCAPE MANEUVER
1. Disconnect the autopilot and increase power to maximum thrust (Go Around Power).
2. Rotate to 3 to 4 degrees per seconds to increase pitch attitude to the highest possible value.
(A pitch attitude of 25 degrees has been demonstrated on the GIV at maximum landing
weight with flaps DOWN (39°).
3. When stick shaker is encountered, or as VREF is approached, reduce pitch rate/angle of attack
to intercept VREF –20 KCAS.
4. DO NOT retract flaps or landing gear until safe climb-out is assured.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-35
31 May 2000
2-05-70: TCAS II Flight Procedures:
1. Upon initiation of an RA, the pilot flying should focus attention on flying 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 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
aircraft, 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.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-36 FAA APPROVED
31 May 2000
2-05-80: All Engines Operating Go Around Procedure:
In the event that an approach is discontinued, proceed as follows:
1. TO/GA Button ............................................................................................................... PRESS
NOTE: The A/T system, if engaged, automatically advances to go-around thrust, and the
autopilot, if engaged, will disengage.
2. Airspeed.............................................................................................................VREF +10 knots
　
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