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= NM
GSO + GSR1
Total Fuel Quantity
Average Fuel Flow
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PB - 18 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Twin Engine Alternate Airport
Flight Plan Fuel CCM
Conditions:
• Standard Day, No Wind
• Zero Fuel Gross Weight Of 44,100 Lb
• 1500 Lb Reserve Fuel Included
• Five (5) Minute Approach Fuel Allowance Included
Distance
To
Alternate
(NM)
Flight
Level
Enroute
Time
(Hr:Min)
TAS
(Knots)
True
Mach
Number
CAS
(Knots)
Fuel
Quantity
(Pounds)
100 230 0:24 329 .542 233 2770
120 250 0:27 338 .562 232 2920
140 310 0:29 378 .645 235 3050
160 350 0:32 412 .715 240 3170
180 370 0:33 427 .745 240 3280
200 410 0:36 437 .762 224 3380
220 430 0:39 442 .770 216 3480
240 450 0:42 442 .770 206 3580
260 450 0:44 442 .770 206 3680
280 450 0:47 442 .770 206 3780
300 450 0:50 442 .770 206 3880
320 450 0:53 442 .770 206 3990
340 450 0:56 442 .770 206 4090
360 450 0:59 442 .770 206 4190
380 450 1:01 442 .770 206 4270
400 450 1:03 442 .770 206 4370
420 450 1:06 442 .770 206 4490
440 450 1:09 442 .770 206 4590
460 450 1:12 442 .770 206 4670
480 450 1:15 442 .770 206 4790
500 450 1:18 442 .770 206 4890
520 450 1:20 442 .770 206 4970
540 450 1:23 442 .770 206 5090
560 450 1:26 442 .770 206 5200
580 450 1:29 442 .770 206 5290
600 450 1:31 442 .770 206 5380
Quick Reference Handbook
REVISION 7 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PC - 1
Non-SP GIV Landing Field Length:
Anti-Skid System Operative - Flaps 39° AFM 5.11
CAUTION: THE GIV MAXIMUM LANDING WEIGHT IS 58,500 POUNDS.
NOTES:
1. ISA day, normal landing configuration.
2. For intended destination wet, multiply landing field lengths below by
1.15.
3. For unfactored landing distances, multiply field lengths below by
0.60.
4. Field lengths seen below are based on no wind or runway slope, but
may be conservatively used with headwinds or uphill runway slopes.
Intended Destination Dry Landing Field Length (Feet)
For Airport Pressure Altitudes As Shown
Landing
Gross
Weight
(Lb)
Sea
Level
2000
Feet
4000
Feet
6000
Feet
8000
Feet
10000
Feet
45000 4870 5030 5190 5390 5640 6030
50000 5150 5330 5510 5730 6010 6450
55000 5430 5620 5820 6070 6380 6850
60000 5720 5920 6140 6410 6760 7270
65000 5990 6220 6460 6760 7120 7680
70000 6280 6520 6790 7100 7500 8090
75000 6460 6720 6990 7320 7740 8350
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PC - 2 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Landing Speed Schedule AFM 5.11
The following guidance is provided to assist in the use of the
charts in this section:
Tire speed limits occur when touchdown speeds exceeds 182.5
knots (210 MPH). Tire fuseplug release limits occur when Brake
Kinetic Energy (BKE) for a maximum effort landing (full brake
application at touchdown) exceeds 40 MFP, making fuseplug release
possible. If brake application is delayed following touchdown, the
resulting lower level of BKEs can be determined from GIV Airplane
Flight Manual Appendix C, GIV Brake Kinetic Energy and Carbon
Brake Cooling.
Limits shown in the charts that follow are conservative in nature and
represent a combination of worst-case conditions, i.e., maximum
temperature at a given altitude plus a 2% downhill runway slope.
These limits apply to a nil or headwind condition only.
NOTE: All speeds shown are KCAS.
Weight = 45000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 101 95 133 123 136 126 141 131 149 139
2000 101 95 133 123 136 126 142 132 149 139
4000 101 95 133 123 137 127 143 133 151 141
6000 102 95 134 124 138 128 144 134 152 142
8000 103 96 135 125 139 129 146 136 154 144
10000 104 97 136 126 141 131 147 137 156 146
12000 105 98 137 127 142 132 149 139 158 148
14000 106 99 139 129 143 133 150 140 160 150
15000 107 100 139 129 144 134 151 141 161 151
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Quick Reference Handbook
REVISION 7 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PC - 3
　
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