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(26,536 kg)
1000 THRU 1213
ASC 190
49,000 lb
(22,226 kg)
75,000 lb
(34,020 kg)
74,600 lb
(33,838 kg)
66,000 lb
(29,937 kg)
1214 AND SUBS 49,000 lb
(22,226 kg)
75,000 lb
(34,020 kg)
74,600 lb
(33,838 kg)
66,000 lb
(29,937 kg)
NOTES: (1) Maximum takeoff weight, unless restricted by climb performance, brake energy,
or tire speed for approved altitudes and ambient temperature of by field length.
See Performance Section for WEIGHT LIMITATIONS.
(2) Maximum landing weight, unless restricted by climb requirements. See
Performance Section for WEIGHT LIMITATIONS.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-12 FAA APPROVED
31 May 2000
1-03-90: Center of Gravity Envelope:
The allowable CENTER OF GRAVITY (CG) range is a function of gross weight as shown in the
figure titled CENTER OF GRAVITY vs. GROSS WEIGHT ENVELOPE. Zero fuel gross
weight CG must be within the allowable Zero Fuel Gross Weight CG Envelope. The fueled
airplane CG will then be within limits for all fuel loadings.
FIGURE 1-4 CENTER OF GRAVITY vs. GROSS WEIGHT ENVELOPES
(FOR SN 1000 -1213)
FIGURE 1-5 CENTER OF GRAVITY vs. GROSS WEIGHT ENVELOPES
(FOR SN 1000-1213 WITH ASC 61)
FIGURE 1-6 CENTER OF GRAVITY vs. GROSS WEIGHT ENVELOPES
(SN 1214 AND SUBS. AND SN 1000-1213 WITH ASC 190)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-13
31 May 2000
Figure 1-4: Center of Gravity versus Gross Weight Envelopes
(SN 1000 – 1213)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-14 FAA APPROVED
31 May 2000
Figure 1-5: Center of Gravity versus Gross Weight Envelopes
(SN 1000 – 1213 with ASC 61)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-15
30 May 2002
Figure 1-6: Center of Gravity versus Gross Weight Envelopes
(SN 1214 and Subs and SN 1000 – 1213 with ASC 190)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-16 FAA APPROVED
31 May 2000
1-12-00: AIRPLANE SERVICING
1-12-10: Hydraulic Fluids:
Fire resistant Type 4 hydraulic fluids are approved for use.
Approved Type IV fluids:
HyJet IV
HyJet IV-A
Skydrol LD-4
Skydrol 500B-4
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-17
31 May 2000
1-12-20: APU Fuel Grades And Fuel Temperatures:
APU operation requires fuel at a viscosity of not more than 12 centistokes. The corresponding
fuel temperatures are as follows:
FUEL GRADE MINIMUM FUEL TEMPERATURE
ASTM D1655 Jet A -30°C
MIL-T-5624 Grade JP-5
MIL-T-83133 Grade JP-8
DEF STAN 91-86
DEF STAN 91-87
CAN 3-GP-24
ASTM D1655 Jet A-1 -40°C
ASTM D1655 Jet B
CAN 2.3.23
MIL-T-5624 Grade JP-4 -50°C
DEF STAN 91-88
DEF STAN 91-91
CAN 2.3.22
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-18 FAA APPROVED
31 May 2000
1-12-30: Engine Fuel Grades:
Fuel conforming to any of the following specifications is approved for use. Fuels conforming to
ASTM Specification ES2-74 are also eligible. Mixing of fuels is permissible.
KEROSENE TYPE
AMERICAN BRITISH CANADIAN
ASTM D1655-89, Jet A DEF STAN 91-87 CAN/CGSB-3.23-M86
ASTM D1655-89, Jet A-1 DEF STAN 91-91
MIL-T-83133A, Grade (JP-8)
FRENCH USSR I.A.T.A.
AIR 3405/C T-1, TS-1, RT (GOST 10277-
86)
1988 Kerosine Type
T-7 (GOST 12308-66)
WIDE CUT JP-4 TYPE
AMERICAN BRITISH CANADIAN
ASTM D1655-89, Jet B DEF STAN 91-88 CAN/CGSB-3.22-M86
MIL-T-5624N, Grade JP-4
FRENCH I.A.T.A.
AIR 3407/B 1987 JP-4
HIGH FLASH POINT JP-5 TYPE
AMERICAN BRITISH CANADIAN
MIL-T-5624N, Grade JP-5 DEF STAN 91-86 CAN 3-GP-24Ma
FRENCH
AIR 3404/C
NOTE: The use of Wide Cut fuel as agreed to by the Operator, Rolls-Royce, and the
appropriate Airworthiness Authority may result in a reduction in HP Fuel Pump Life.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-19
31 May 2000
1-12-40: Fuel Additives:
The following fuel additives (in addition to those included in DEF STAN Specifications) are
approved by Rolls-Royce, subject to limitations stated:
1. Corrosion Inhibitor/Lubricity Aids
Concentration Range - lb/42,035 gallons (US)/35,000 gallons (IMP)
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