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Speed brakes are not approved for extension with flaps at 39° (DOWN) or with
landing gear extended.
2. Use Of FLIGHT POWER SHUTOFF:
Do NOT pull FLIGHT POWER SHUTOFF handle with speed brakes extended.
OPERATING MANUAL
EXPANDED LIMITATIONS 01-27-00
Page 1
September 13/00
Revision 1
01-27-50: Ground Spoilers
Takeoff is permitted with ground spoilers inoperative, provided anti-skid is operative and
20° flaps are used for takeoff.
OPERATING MANUAL
01-27-00 EXPANDED LIMITATIONS
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September 13/00
Revision 1
FUEL
01-28-10: Usable Fuel Capacities
1. Unbalanced Fuel:
For maximum unbalanced fuel, see Figure 1: Permissible Fuel Unbalance For All
Flight Operations. Before the unbalance exceeds that shown, proceed with fuel
balancing.
2. Usable Fuel Capacities:
Left Tank 14,750 lb (6,690 kg) 2,185 gal (8,271 L)
Right Tank 14,750 lb (6,690 kg) 2,185 gal (8,271 L)
Total 29,500 lb (13,380 kg) 4,370 gal (16, 542 L)
NOTE:
It is possible to upload fuel in excess of 29,500
pounds. This is permitted as long as the maximum
ramp weight and/or the maximum takeoff weight is not
exceeded, and the loaded airplane center of gravity is
within limits.
OPERATING MANUAL
EXPANDED LIMITATIONS 01-28-00
Page 1
October 11/01
Revision 5
Permissible Fuel Unbalance For All Flight Operations
Figure 1
OPERATING MANUAL
01-28-00 EXPANDED LIMITATIONS
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October 11/01
Revision 5
01-28-20: Boost Pumps
During cruise, one (1) boost pump per side may be selected OFF provided:
• The fuel contains an anti-icing additive, or:
• Fuel tank temperature is above 0°C.
See Section 01-12-30, Engine Fuel Grades.
CAUTION
THE ENGINE WILL RUN ON SUCTION FUEL FEED
ONLY AT OR BELOW 20,000 FEET. ABOVE 20,000
FEET, THE ENGINE WILL RUN ERRATICALLY AND
FLAME OUT IF THE CROSSFLOW VALVE IS NOT
OPEN WITH AT LEAST ONE BOOST PUMP ON.
OPERATING MANUAL
EXPANDED LIMITATIONS 01-28-00
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October 11/01
Revision 5
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
01-28-00 EXPANDED LIMITATIONS
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October 11/01
ICE AND RAIN PROTECTION
01-30-10: Wing Anti-Icing
Operation of wing anti-icing is required if icing conditions are imminent, or immediately
upon detection of ice formation on wings, winglets, or windshield edges.
01-30-20: Cowl Anti-Icing
1. Requirements of Use:
Operation of the cowl anti-icing system is required for taxi and takeoff when Static
Air Temperature (SAT) is below +8° C and visible moisture, precipitation, or wet
runway are present. Engine operation at 85% LP for one (1) minute is
recommended just prior to takeoff and at intervals of not more than sixty (60)
minutes under these temperature and moisture conditions.
2. Low Cowl Anti-Ice Pressure:
Depart icing conditions if COWL PRESSURE LOW message illuminates and cowl
anti-ice pressure cannot be maintained at or above 4 psi.
NOTE:
The COWL PRESSURE LOW message illuminates at
4 psi on SN 1190 and Subs, and SN 1000 through
1189 with ASC 243. It illuminates at 10 psi on SN 1000
through 1189 without ASC 243. Cowl anti-ice is
effective at 4 psi or greater.
3. Use In Flight:
Use of cowl anti-icing system is required in flight as indicated in Figure 1:
Temperature Range For Cowl Anti-Icing, when visible moisture or precipitation is
present, or when signs of icing are observed. Ice accretion may be observed on
wings or windshield edges.
OPERATING MANUAL
EXPANDED LIMITATIONS 01-30-00
Page 1
May 31/00
Revision 0
Temperature Range For Cowl Anti-Icing
Figure 1
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May 31/00
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INDICATING / RECORDING
01-31-10: Electronic Checklist
1. For SPZ-8000 Equipped Airplanes:
Electronic Checklist Document Number 1159AV41201-20 corresponds to this
revision of the Gulfstream Aerospace GIV Airplane Flight Manual and Gulfstream
Aerospace GIV Operating Manual.
2. For SPZ-8400 Equipped Airplanes:
Electronic Checklist Document Number 1159AV41202-20 corresponds to this
revision of the Gulfstream Aerospace GIV Airplane Flight Manual and Gulfstream
Aerospace GIV Operating Manual.
3. Acceptable Checklists:
Electronic Checklist Document Numbers 1159AV41201-8 and 1159AV41202-10
are acceptable for use until the checklist modules can be updated.
4. Verifying Checklist Version:
Checklist version can be verified by selecting TITLE PAGE of Electronic Checklist.
OPERATING MANUAL
　
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