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RATED EPR 1.69 1.70 1.71 1.73 1.74 1.75 1.76 1.77 1.77 1.77
-- 60,000 LB --
VFS = 168 KCAS FLD LNGTH ****** ****** ****** ****** ****** 13,570 13,030 12,310 11,710 11,250
VSE = 175 KCAS V1 KCAS ****** ****** ****** ****** ****** 147 146 146 145 146
VREF = 150 KCAS VR KCAS ****** ****** ****** ****** ****** 147 147 147 146 146
MAX TEMP = -5°C V2 KCAS ****** ****** ****** ****** ****** 151 151 151 151 151
-- 58,000 LB --
VFS = 165 KCAS FLD LNGTH ****** ****** ****** ****** 13,140 12,550 12,070 11,420 10,860 10,440
VSE = 172 KCAS V1 KCAS ****** ****** ****** ****** 144 143 143 142 142 142
VREF = 147 KCAS VR KCAS ****** ****** ****** ****** 144 144 144 144 144 144
MAX TEMP = 4°C V2 KCAS ****** ****** ****** ****** 148 148 148 148 148 148
-- 56,000 LB --
VFS = 162 KCAS FLD LNGTH ****** 13,960 13,140 12,690 12,130 11,620 11,180 10,590 10,070 9,680
VSE = 169 KCAS V1 KCAS ****** 142 141 141 140 140 139 139 139 139
VREF = 144 KCAS VR KCAS ****** 142 142 141 141 141 141 141 141 141
MAX TEMP = 15°C V2 KCAS ****** 146 146 146 146 146 146 146 146 146
-- 54,000 LB --
VFS = 159 KCAS FLD LNGTH ****** 12,690 12,100 11,700 11,210 10,750 10,350 9,810 9,330 8,970
VSE = 166 KCAS V1 KCAS ****** 138 138 137 137 136 136 135 135 135
VREF = 142 KCAS VR KCAS ****** 139 139 139 139 138 138 138 138 138
MAX TEMP = 15°C V2 KCAS ****** 143 143 143 143 143 143 143 143 143
-- 52,000 LB --
VFS = 156 KCAS FLD LNGTH ****** 11,670 11,160 10,790 10,350 9,930 9,570 9,070 8,640 8,300
VSE = 163 KCAS V1 KCAS ****** 135 134 134 133 133 132 132 132 132
VREF = 139 KCAS VR KCAS ****** 136 136 136 136 136 135 135 135 135
MAX TEMP = 15°C V2 KCAS ****** 140 140 140 140 140 140 140 140 140
-- 50,000 LB --
VFS = 153 KCAS FLD LNGTH ****** 10,730 10,280 9,950 9,550 9,170 8,840 8,380 7,980 7,670
VSE = 160 KCAS V1 KCAS ****** 131 131 130 130 130 129 129 129 129
VREF = 136 KCAS VR KCAS ****** 133 133 133 133 133 133 132 132 132
MAX TEMP = 15°C V2 KCAS ****** 138 138 138 138 138 138 138 138 138
-- 48,000 LB --
VFS = 150 KCAS FLD LNGTH ****** 9,860 9,460 9,160 8,790 8,450 8,150 7,730 7,370 7,080
VSE = 156 KCAS V1 KCAS ****** 128 127 127 127 126 126 125 125 125
VREF = 133 KCAS VR KCAS ****** 130 130 130 130 130 130 130 130 130
MAX TEMP = 15°C V2 KCAS ****** 135 135 135 135 135 135 135 135 135
-- 46,000 LB --
VFS = 147 KCAS FLD LNGTH ****** 9,060 8,690 8,420 8,090 7,780 7,500 7,120 6,790 6,520
VSE = 153 KCAS V1 KCAS ****** 124 124 124 123 123 122 122 122 122
VREF = 131 KCAS VR KCAS ****** 128 127 127 127 127 127 127 127 127
MAX TEMP = 15°C V2 KCAS ****** 132 132 132 132 132 132 132 132 132
CAUTION: DO NOT REDUCE TAKEOFF EPR BY MORE THAN .15 OR BELOW A MINIMUM VALUE OF 1.56.
NOTES: HEADWIND: Increase available field length 2% for each 5 knots (up to 40 knots).
TAILWIND: Not permitted using this data at this pressure altitude.
UPHILL SLOPE: Decrease available field length 20% for each 1% (up to 2%).
DOWNHILL SLOPE: Not permitted using this data at this pressure altitude.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
FAA APPROVED B-1
31 May 2000 GIV-SP
APPENDIX B
CONFIGURATION DEVIATION LIST
PURPOSE
This Configuration Deviation List (CDL) contains additional certificate limitations for operation
of the Gulfstream GIV without certain secondary airframe and engine parts as listed herein. The
certificate limitations in Section 1 are applicable except as amended herein. All FAA approved
limitations must be followed when operating with a configuration deviation.
APPLICABILITY
This list does not include parts which do not affect the airworthiness of the airplane, such as
galley equipment, entertainment systems, passenger convenience items, etc., and is based on the
configuration of the airplane as originally manufactured. Secondary airframe parts changed or
added during completion or while the airplane is in operation should be addressed by
supplementary revisions to the list.
MULTIPLE ITEMS
No more than one part for any subsystem in this list may be missing, unless specifically
designated combinations are indicated herein. Unless otherwise specified herein, parts from
different subsystems may be missing. The performance penalties are cumulative. The decision
of the pilot in command of the flight, to have allowable missing parts corrected prior to flight,
will take precedence over the provisions contained in this publication.
If an additional part is lost in flight, the airplane may not depart the airport at which it landed
following this event until it again complies with the limitations of this appendix. This does not
　
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