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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 Revision 2,
dated October 1999 (or later approved revision) shall be immediately available to the pilots. This
applies to airplanes SN 1390 and subsequent.
TCAS OPERATING CONSTRAINTS
With 6.04A software installed, all RA and TA aural messages are inhibited at a radio altitude less
then 1,100 ft climbing and 900 ft descending.
With 7.0 software installed (SN 1434 and sub), all RA and TA aural messages are inhibited at a
radio altitude less than 500 ft ±100 ft.
CLEARANCE
The pilot is authorized to deviate from ATC to the extent necessary to comply with a Resolution
Advisory (RA).
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-40 FAA APPROVED
31 May 2001
TRAFFIC ADVISORIES
The pilot must not initiate evasive maneuvers based solely on information from a Traffic
Advisory (TA). Traffic Advisory information should be used only as an aid to visual acquisition
of traffic.
RESOLUTION ADVISORIES
Compliance with TCAS Resolution Advisories (RA) is required unless the pilot considers it
unsafe to do so. Maneuvers which are in the opposite direction of an RA are extremely
hazardous and are prohibited unless it is visually determined to be the only means to assure safe
separation.
CLEAR OF CONFLICT
Prompt return to the ATC cleared altitude must be accomplished when "CLEAR OF
CONFLICT" is announced.
SINGLE ENGINE INOPERATIVE AND TCAS
With a single engine inoperative, select TA only as the TCAS operating mode.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-41
11 October 2001
1-34-80: Enhanced Ground Proximity Warning System (EGPWS)
PILOT’S MANUALS
The Honeywell Enhanced Ground Proximity Warning System Pilot’s Guide, Publication Number
060-4241-000, Revision D, dated March 2000 (or later approved revision appropriate to the
software version below) must be immediately available to the pilots for -208 -208 (SN 1390 thru
1425) or -210 -210 (SN 1426 and subs).
CLEARANCE
Pilots are authorized to deviate from their current Air Traffic Control (ATC) clearance to the
extent necessary to comply with an EGPWS warning.
NAVIGATION
Navigation is not to be predicated upon the use of the Terrain Display.
DATA BASE
The EGPWS data base, displays, and alerting algorithms currently account for man-made
obstructions.
TERRAIN DISPLAY
The Terrain Display is intended to serve as a situational awareness tool only, and may not
provide the accuracy and/or fidelity on which to solely base terrain avoidance maneuvering.
Terrain Display shall be selected OFF when within 15 NM of landing at an airport when:
• The airport has no published instrument approach procedure (-104 -104 software version only).
• The longest runway is less than 3,500 ft in length.
• The airport is not in the EGPWS data base.
TAWS
The production EGPWS installation meets the requirements for Class A TAWS as defined in
Advisory Circular AC 25-23.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-42 FAA APPROVED
11 October 2001
1-34-90: Lasertrak NDU:
The Honeywell GC1230AC10, 11, 20, 21 Lasertrak Navigation Display Unit Pilot’s Manual,
number M28-2231-001-02 dated October 1999 (or later approved revision), is to be immediately
available to the crew whenever navigation is predicated on the use of the Honeywell Lasertrak
Navigation Display Unit.
The Honeywell SPZ-8000 Digital Automatic Flight Control System (Phase II) Pilot’s Manual for
the Gulfstream IV, number A28-1146-064, revision 5 dated October 1999 (or later approved
revision), or Honeywell SPZ-8400 Digital Automatic Flight Control System Pilot’s Manual for
the Gulfstream IV, number A28-1146-0097, revision 2 dated October 1999 (or later approved
revision), is to be immediately available to the crew whenever the Lasertrak NDU is used. It is
the crew’s responsibility to be familiar with the Pilot’s Manual.
Lasertrak can only be displayed on the PFD and on the ND in the compass mode; it cannot be
coupled to the flight guidance system.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-43
11 October 2001
1-35-00: OXYGEN SYSTEM
1-35-10: Oxygen Departure Pressures:
The oxygen supply of this airplane consists of one (1) 50 cubic ft. (1415 1iter) cylinder, located
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