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LANDING GEAR
01-32-10: Brake System
Takeoff is prohibited with BRAKE FAIL or BRAKE PEDAL messages displayed that
cannot be cleared as described in Section 04-03-10: Crew Alerting System (CAS)
Caution Messages and Procedures.
01-32-20: Anti-Skid System (Brake By Wire)
Takeoff is permitted with anti-skid inoperative, provided ground spoilers are operative,
20° flaps are used, and the cowl and wing anti-ice systems are not used.
01-32-30: Anti-Skid System (HMAB)
FOR AIRPLANES SN 1183, AND SN 1214 AND SUBS:
Takeoff is permitted with Anti-Skid inoperative, provided Ground Spoilers are operative,
20° Flaps are used, and the Cowl and Wing Anti-Ice systems are not used.
01-32-40: Landing Lights
Ground operation of the landing lights is limited to five (5) minutes.
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NAVIGATION
01-34-10: Airborne Weather Radar
WHEN OPERATING WEATHER RADAR ON THE GROUND, THE FOLLOWING
LIMITATIONS APPLY:
1. Operation During Refueling:
Do NOT operate radar during refueling of the airplane or when within 300 feet (92
meters) of other refueling operations.
2. Operation At Other Times:
• With 24 inch antenna: Do NOT operate radar within 49 ft (15 meters) of
ground personnel
• With 18 inch antenna: Do NOT operate radar within 33 ft (10 meters) of
ground personnel
01-34-20: Inertial Reference System (IRS)
1. For SPZ-8000 Equipped Airplanes:
When operating in “ATT-REF” mode, do NOT use IRS heading information unless
airplane heading is manually entered via the ISDU or the appropriate IRS status
page on the FMS CDU.
NOTE:
For SPZ 8000 equipped airplanes, heading will appear
as “000” when the IRS is selected to “ATT-REF”.
2. For SPZ-8400 Equipped Airplanes:
NOTE:
HDG FAIL will appear on the HSI until a valid airplane
heading is manually entered via the ISDU or the
appropriate IRS status page on the FMS CDU.
Honeywell HG1075AE Series IRS equipment installed in the Gulfstream IV has
been certified for alignment to 78° Latitudes. For alignment between 70° and 78°
Latitude, fifteen (15) minute alignment time is required. For flight above 73° N and
60° S Latitude, Electronic Flight Information System (EFIS) heading information
must be switched from magnetic (MAG) to TRUE due to loss of valid MAG
heading from the IRS. Above 73° N and 60° S Latitude with TRUE heading
information displayed, ILS, MLS, TCN and VOR navigation capability is
unavailable unless special procedures in GIV Operating Manual, Section 2A-34-
00: Navigation, are followed.
01-34-30: Pilot’s Manuals
For SPZ-8000 equipped airplanes, the Honeywell SPZ-8000 Digital Integrated Flight
Control System (Phase II) Pilot’s Manual for the Gulfstream IV, Honeywell Publication
Number A28-1146-064, Revision 5, dated October 1999 (or later approved revision) is to
be immediately available to the flight crew.
For SPZ-8400 equipped airplanes, the Honeywell SPZ-8400 Digital Automatic Flight
Control System Pilot’s Manual for the Gulfstream IV, Honeywell Publication Number A28-
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Revision 7
1146-0097, Revision 2, dated October 1999 (or later approved revision) is to be
immediately available to the 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 Serial Number (SN) 1470 and subsequent with the CD-820 FMS
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湾流4操作手册 Gulfstream IV Operating Manual 1(16)
