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ADDITIVE MINIMUM MAXIMUM
Hitec 515 4 (11 mg/1) 7.5 (21 mg/1)
Apollo PRI 19 3 (9 mg/1) 8 (23 mg/1)
Tolad 245 7.5 (21 mg/1) 12 (34 mg/1)
DuPont DCI-4A 3 (9 mg/1) 8 (23 mg/1)
Hitec 580 3 (9 mg/1) 8 (23 mg/1)
NOTE: Minimum requirement is to ensure that sufficient additive is available when it is
required to act as a lubricity aid.
2. Anti-Icing Additive
DEF STAN 68-252 or MIL-I-27686E, or any direct equivalent in concentrations not
exceeding 0.15 percent by volume.
3. Static Dissipator Additive
Shell A.S.A. 3 in concentrations of not more than 1.00 part per million.
Stadis 450 maximum concentration not more than 3.00 parts per million.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-20 FAA APPROVED
31 May 2000
4. Anti-Microbiological Additive
A. Methyl Cellosolve may be used. Refer to GIV Maintenance Manual, Chapter 28 for
additive application procedures.
B. Biobor JF may be used. Refer to GIV Maintenance Manual, Chapter 28 for additive
application procedures.
C. Kathon FP 1.5 may be used. Refer to GIV Maintenance Manual, Chapter 28 for additive
application procedures.
NOTE: Under certain conditions solid matter may be precipitated from fuel containing
Biobor JF or Kathon FP 1.5 during flight. The fuel differential pressure signals
should be carefully monitored in flight immediately following its use in the airplane
tanks. See Rolls Royce Tay Maintenance Manual M-TAY-1RR for recommended
procedures to be followed when using Biobor JF or Kathon FP 1.5.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-21
31 May 2000
1-12-50: Oil Grades (Engine/Starter/APU):
WARNING: LUBRICATING OIL IS TOXIC TO SKIN, EYES, AND RESPIRATORY
TRACT. SKIN AND EYE PROTECTION IS REQUIRED. AVOID
REPEATED OR PROLONGED CONTACT. USE IN A WELL
VENTILATED AREA.
CAUTION: USE ONLY BRAND NAMES SPECIFICALLY AUTHORIZED. USE OF ANY
UNAPPROVED OIL REQUIRES AUTHORIZATION OF EQUIPMENT
MANUFACTURER.
NOTE: Mixing of oils is not recommended but brands may be mixed if operationally essential.
Complete drainage of one oil and replacement with a different brand is not considered
mixing of oils.
Oil of the brands below, when reclaimed to approved Rolls-Royce standards for
appropriate viscosity grade, are approved for use in TAY engine.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-22 FAA APPROVED
31 May 2000
The following oils are approved for common usage in the engine and APU.
Table 1
Common Lubricating Oils List
(3 centistoke oils)
Manufacturer/Oil
Aeroshell Turbine Oil 390
Castrol 3 C Gas Turbine Oil
Castrol 325 Gas Turbine Oil
Exxon 2389
Table 2
Common Lubricating Oils List
(5 centistoke oils)
Manufacturer/Oil
Royco/Aeroshell Turbine Oil 500
Aeroshell Turbine Oil 560
Exxon Turbo Oil 2380
Mobil Jet II
Mobil 254
Castrol 5000 Gas Turbine Oil
Refer to the following manuals for oils approved for specific usage in Engine, Starter, or APU:
ENGINE: U.K. CAA Approved Rolls-Royce Tay Operating Instructions (F-TAY-1RR) and
associated Service Bulletins.
STARTER: Garrett Starter Maintenance Manual 80-10-53.
APU: Garrett Maintenance Manual No. 49-21-89 for APU Model No. GTCP36-100(G)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-23
31 May 2000
1-21-00: AIR CONDITIONING AND BLEED AIR
1-21-10: Cabin Pressurization Control System:
Maximum cabin pressure differential permitted is 9.80 psi. Maximum cabin pressure differential
permitted for taxiing, takeoff or landing is 0.3 psi.
1-21-20: Bleed Air System:
Do not operate above 41,000 ft. without both engine bleeds ON and each engine being bled by
either the air conditioning system or engine cowl anti-ice. See Section 3, AIR CONDITIONING
SYSTEM SHUTDOWN OR INOPERATIVE Procedure.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-24 FAA APPROVED
31 May 2000
1-22-00: AUTO FLIGHT
1-22-10: Mach Trim Compensation/Electric Elevator Trim:
Mach Trim Compensation must be ON during all flight operations except as provided for in
Section 3, MACH TRIM COMPENSATION FAILURE. If Mach Trim Compensation is
inoperative, MMO is reduced to 0.75 MT.
When failure of Mach Trim Compensation is coupled with Yaw Damper failure, observe speed
limitations for both failures and limit altitude to 41,000 ft.
1-22-20: Autothrottle:
Use of autothrottle is not permitted for takeoff or go-around when wing anti-ice is used.
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