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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.
01-34-40: Flight Management System (FMS)
1. General:
• 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 data base 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 If the database is out of date, flight may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 Global Positioning
System (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 upon GPS sensor data is not permitted
unless the navigation computer software version is NZ4.1, NZ5.X, NZ6.X
or later approved version.
2. Approaches Permitted:
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:
A. Conditions for Approval:
(1) FMS APPROACH annunciator is illuminated.
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(2) One of the following published approach procedures is used:
• RNAV
• VOR
• VOR/DME
• ADF
• GPS
• TACAN
(3) One pilot monitors raw data of referenced NAVAID for VOR, VOR/
DME, ADF, GPS or TACAN approach without navigation computer
software version NZ4.1, NZ5.X, NZ6.X or later approved version
installed.
(4) FMS navigation mode is one of the following:
• GPS
• GPS/DME/DME
• DME/DME
• VOR/DME
(5) DR or DGRAD annunciators are not illuminated.
(6) 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 Airplane Flight
Manual Supplement 2000-03 for airplanes with
navigation computer software version NZ4.1, NZ5.X,
NZ6.X or later approved version installed.
01-34-50: Performance Computer
Use of the performance computer for takeoff and landing field performance is permitted
except as noted in the following paragraph. The performance computer’s calculations
shall be checked for reasonableness. The Performance section of the GIV Airplane Flight
Manual 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 9000
feet Pressure Altitude (PA) with PZ software versions PZ-9003, A-PZ-9101 or F-PZ-
9101.
There are no operational limitations when using performance data contained in the GIV
Airplane Flight Manual or PZ software versions A-PZ-9302, F-PZ-9302, A-PZ-9401,
A-PZ-9402, F-PZ-9401 or F-PZ-9402.
01-34-60: SPZ-8400 Flight Director
1. Takeoff / Go-Around (TO/GA) Mode:
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 with the airplane on
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the ground will result in GA speed targets and pitch guidance.
01-34-70: Traffic Alert And Collision Avoidance System (TCAS)
1. Pilot’s Manuals:
The Honeywell Traffic Alert and Collision Avoidance System (TCAS) Pilot’s Guide,
Publication Number C28-3841-005-00, dated September 1999 (or later approved
revision) shall be immediately available to the pilots. The Honeywell SPZ-8400
Digital Automatic Flight Control System Pilot’s Manual for the Gulfstream IV
Document Number A28-1146-097-02, Revision 2, dated October 1999 (or later
approved revision) shall be immediately available to the pilots. This applies to
airplanes SN 1390 and subsequent.
2. TCAS Operating Constraints:
With 6.04A software installed, all Resolution Advisory (RA) and Traffic Advisory
(TA) aural messages are inhibited at a radio altitude less than 1,100 feet climbing
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