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available to the pilots. The Honeywell SPZ-8400 Digital Automatic
Flight Control System Pilot’s Manual for the Gulfstream IV,
publication 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 and 900 feet descending.
With 7.0 software installed (SN 1434 and subsequent), all RA and
TA aural messages are inhibited at a radio altitude less than 500 feet
±100 feet.
(3) Clearance:
The pilot is authorized to deviate from ATC to the extent necessary
to comply with a Resolution Advisory (RA).
(4) Traffic Advisories:
The pilot must not initiate evasive maneuvers based solely on
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information from a Traffic Advisory (TA). Traffic Advisory information
should be used only as an aid to visual acquisition of traffic.
(5) 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.
(6) Clear Of Conflict:
Prompt return to the ATC cleared altitude must be accomplished
when “CLEAR OF CONFLICT” is announced.
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TCAS / ACAS System Simplified Block Diagram
Figure 22
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TCAS / ACAS Display on DU #4
Figure 23
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TCAS / ACAS Display in MAP Mode
Figure 24
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TCAS / ACAS RA Display on the PFD
Figure 25
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Radio Tuning Unit (RTU)
Figure 26
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TCAS / ACAS
Transponder Antenna
Locations
Figure 27
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OXYGEN
2A-35-10: General
The Gulfstream IV is designed to operate at altitudes up to and including 45,000 feet.
Both the airplane structure and pressurization system are designed using fail-safe
criteria in order to minimize any possibility of exposing the crew and passengers to these
critical altitudes. Should the need arise, however, high-pressure gaseous oxygen
systems are installed to provide oxygen to all occupants. There are two types of oxygen
systems installed on the GIV airplanes: the crew and passenger oxygen system and the
portable oxygen system. On airplanes 1500 and subsequent, however, there are also
production provisions for a therapeutic oxygen system.
In accordance with Federal Aviation Administration regulations, there must be at least
one portable oxygen system (commonly referred to as a “walkaround” cylinder or bottle)
aboard the airplane for flight crew use while disconnected from the airplane system. The
exact type of system and its location are selected by the operator and installed by the
outfitting agency. Specific information describing the portable oxygen system would thus
be supplied to the operator by the outfitting agency. Provisions exist to place this data in
Chapter 2C, Outfitted Systems, of this manual.
2A-35-20: Crew and Passenger Oxygen Systems
1. General Description:
Two types of production standard gaseous oxygen systems are installed in
Gulfstream IV airplanes. Airplanes Serial Number (SN) 1000 through 1289 have
only for a single-cylinder crew oxygen system installed. For these airplanes, the
outfitting agency selected by the operator installs the passenger oxygen system
and performs modifications, if any, to the crew oxygen system. Specific
information describing the outfitted oxygen system would thus be supplied to the
operator by the outfitting agency. Provisions exist to place this data in Chapter 2C,
　
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