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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 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.
7. Single Engine Inoperative and TCAS:
With a single engine inoperative, select TA only as the TCAS operating mode.
01-34-80: Enhanced Ground Proximity Warning System (EGPWS)
1. 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).
2. Clearance:
Pilots are authorized to deviate from their current Air Traffic Control (ATC)
clearance to the extent necessary to comply with an EGPWS warning.
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3. Navigation:
Navigation is not to be predicated upon the use of the Terrain Display.
4. Database:
The EGPWS database, displays and alerting algorithms currently account for
man-made obstructions.
5. 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 database.
6. TAWS:
The production EGPWS installation meets the requirements for Class A TAWS as
defined in Advisory Circular AC 25-23.
01-34-90: Lasertrak Navigation Display Unit (NDU)
The Honeywell GC1230AC10/11/20/21 Lasertrak Navigation Display Unit Pilot’s Manual,
publication 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 (NDU).
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 ND in the compass mode; it cannot be
coupled to the flight guidance system.
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OXYGEN SYSTEM
01-35-10: Oxygen Departure Pressures
The quantity of oxygen required varies with the flight profile. The method of determining
minimum oxygen quantity is shown in Figure 1.
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Oxygen Duration At Various Cabin Altitudes
Figure 1
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ENGINE INSTRUMENTS AND CREW ALERTING SYSTEM (EICAS)
01-45-10: General EICAS Range Markings Colors
• Normal Range Values: White
• Caution Range Values: Amber
• Warning Range Values: Red
01-45-20: Powerplant EICAS Indications
1. Arc Color Values:
　
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