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flight crew.
When FMS navigation is in use, the appropriate Pilot’s Manual listed below is to be available to
the flight crew:
• Flight Management System for the Gulfstream IV (Software Version 4.1), Honeywell
Publication Number A28-1146-115, Dated August 1996 (or later approved revision). This
publication is equivalent to Honeywell Publication Number A28-1146-081.
• FMZ Series Flight Management System for the Gulfstream IV, Honeywell Publication
Number A28-1146-126, dated August 1998 (or later approved revision).
• FMZ Flight Management System for the Gulfstream IV (Software Version 5.2), Honeywell
Publication Number A28-1146-135, dated May 1999 (or later approved revision).
• FMZ Flight Management System for the Gulfstream IV (Software Version 6.0), Honeywell
Publication Number A28-1146-141, dated February 2002 (or later approved revision).
• For airplanes SN 1470 and subs with the CD-820 FMS Control Display Unit installed, the
CD-820 Pilot’s Manual, Honeywell Publication Number A28-1146-149-01, Revision 1,
dated September 2001 (or later approved revision), is to be immediately available to the
flight crew.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-37
30 May 2002
1-34-40: Flight Management System (FMS):
The Flight Management System (FMS) shall not be used for Navigation above 85° North or
South Latitude for airplanes with software version NZ-9001. FMS Navigation above 85° North
or South Latitude is approved for airplanes with software version NZ-9101, NZ-9111, NZ4.0,
NZ4.1, NZ5.X or NZ6.X.
Verify that the database is current. If the database is out of date, flight may be continued
providing the latitude/longitude of each waypoint is verified by the crew. A current database is
required in order to fly GPS approaches.
Verify that the navigation computer software version is NZ-9001, NZ-9101, NZ-9111, NZ4.0,
NZ4.1, NZ5.X or NZ6.X.
Verify that the performance computer software version is PZ-9003, A-PZ-9101, F-PZ-9101,
A-PZ-9302, F-PZ-9302, A-PZ-9401, A-PZ-9402, F-PZ-9401 or F-PZ-9402.
FMS navigation based solely on Global Positioning System (GPS) sensor data is not permitted
unless the navigation computer software version is NZ4.1, NZ5.X, NZ6.X or later approved
version.
FMS is approved for vertical and lateral Flight Director/Autopilot coupled IFR RNAV, VOR,
VOR/DME, ADF, GPS and TCN approaches under the following conditions:
• FMS APPROACH annunciator is illuminated.
• A published RNAV, VOR, VOR/DME, ADF, GPS or TACAN approach procedure is
used.
• One pilot monitors raw data of referenced NAVAID for VOR, VOR/DME, ADF,
GPS or TACAN approach without NZ4.1, NZ5.X, NZ6.X or later approved version
installed.
• FMS navigation mode is GPS, GPS/DME/DME, DME/DME or VOR/DME.
• DR or DGRAD annunciators are not illuminated.
• Minimum altitude for autopilot coupled IMC VNAV operations is 300 ft. AGL or 50
ft. below Minimum Descent Altitude (MDA) whichever is higher.
NOTE: Additional information regarding FMS approach procedures can be found in GIV AFM
Supplement 2000-03 for airplanes with NZ4.1, NZ5.X, NZ6.X or later approved
version installed.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-38 FAA APPROVED
13 September 2000
1-34-50: Performance Computer:
Use of the Performance Computer for takeoff and landing field performance is permitted except
as noted below. The Performance Computer’s calculations shall be checked for reasonableness.
The AFM Performance Section shall be available for cross-reference as necessary.
The use of the Performance Computer is prohibited for airplanes SN 1000 and subsequent for
takeoff operations utilizing 10° Flaps at Airport Field Elevations above 9,000 feet P.A. with PZ
Software Version PZ-9003, A-PZ-9101, or F-PZ-9101.
There are no operational limitations when using performance data contained in the Airplane
Flight Manual or PZ Software Version A-PZ-9302, F-PZ-9302, A-PZ-9401, A-PZ-9402, F-PZ-
9401 or F-PZ-9402.
1-34-60: SPZ-8400 Flight Director
Selection of the TO/GA mode at speeds greater than 60 knots on the ground is not permitted.
Selection of TO/GA at airspeeds above 60 KCAS and the airplane on the ground will result in
GA speed targets and pitch guidance.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-39
30 May 2002
1-34-70: Traffic Alert And Collision Avoidance System (TCAS)
PILOT’S MANUALS
The Honeywell Traffic Alert and Collision Avoidance System (TCAS) Pilot’s Guide, Publication
　
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