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VREF = 139 KCAS VR KCAS ****** ****** ****** ****** ****** ****** 135 135 135 135
MAX TEMP = -7°C V2 KCAS ****** ****** ****** ****** ****** ****** 140 140 140 140
-- 50,000 LB --
VFS = 153 KCAS FLD LNGTH ****** ****** ****** ****** 9,550 9,170 8,840 8,380 7,980 7,670
VSE = 160 KCAS V1 KCAS ****** ****** ****** ****** 130 130 129 129 129 129
VREF = 136 KCAS VR KCAS ****** ****** ****** ****** 133 133 133 132 132 132
MAX TEMP = 4°C V2 KCAS ****** ****** ****** ****** 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 2001
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
preclude the issuance of a ferry permit to allow the airplane to be flown to a point where the
necessary repairs or replacements can be made.
ACTION REQUIRED
MAINTENANCE LOG
The operator shall list in the airplane logbook an appropriate notation covering the missing
part(s) on each flight.
DAMAGE INSPECTION
The operator shall make a thorough check of the airplane to ascertain that other areas have not
been damaged or affected.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
B-2 FAA APPROVED
31 May 2001
PLACARDING
The operator shall make a placard by duplicating the complete CDL item from this publication
and cut it to size to show only the subject item. Install this placard in a conspicuous location in
the cockpit.
If the missing part requires a reduction of VMO/MMO, an approved placard for the reduced
VMO/MMO must be installed adjacent to the airspeed indicator and any additional restrictions
must be placarded for the pilots to easily see.
PERFORMANCE AND FLIGHT PLANNING
The effects of the missing parts will be included in the calculations for takeoff, landing and
cruise. Performance penalties for multiple items are cumulative.
LIMITATIONS
1. The numbering and designation of systems in CDL appendix is based on ATA Specification
No. 100. The parts within each system are identified by functional description and, when
necessary, by part numbers.
2. When the airplane is operated using this appendix, it must be operated in accordance with the
　
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