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GIV-SP Twin Engine Flight Planning: Mach 0.80 - ISA
CCM
For airplanes SN 1214 and subsequent and SN 1000 thru 1213
with ASC 190 incorporated.
Quick Reference Handbook
GIV-SP PERFORMANCE REVISION 7
Page PB - 16 (GIV-SP AIRPLANES ONLY) May 30/02
GIV-SP Twin Engine Flight Planning: Mach 0.83 - ISA
CCM
For airplanes SN 1214 and subsequent and SN 1000 thru 1213
with ASC 190 incorporated.
Quick Reference Handbook
REVISION 7 GIV-SP PERFORMANCE
May 30/02 (GIV-SP AIRPLANES ONLY) Page PB -17
GIV-SP Equal Time Point And Point Of No Return CCM
DEPARTURE
AIRPORT
DESTINATION
AIRPORT
ETP PNR WIND
GS R1
GSO
GSR GSC
TRIP DISTANCE = D
The following formula is used to calculate the ground distance from the
departure airport to ETP:
GROUND DISTANCE TO ETP =
Where:
D = Total Trip Distance
GSC = Ground Speed To Continue To Destination At Altitude To Be
Flown
GSR = Ground Speed To Departure Airport At Altitude To Be Flown
The following formula is used to calculate the ground distance from the
departure airport to PNR:
GROUND DISTANCE TO PNR =
Where:
Endurance =
GSO = Normal Outbound Ground Speed At Cruise Altitude
GSR1 = Return Ground Speed At Normal Cruise Altitude
(D) (GSR)
= NM
GSC + GSR
(Endurance) (GSR1) (GSO)
= NM
GSO + GSR1
Total Fuel Quantity
Average Fuel Flow
Quick Reference Handbook
GIV-SP PERFORMANCE REVISION 7
Page PB - 18 (GIV-SP AIRPLANES ONLY) May 30/02
GIV-SP Twin Engine Alternate Airport Flight Plan Fuel
CCM
For airplanes SN 1214 and subsequent and SN 1000 thru 1213
with ASC 190 incorporated.
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 GIV-SP PERFORMANCE
May 30/02 (GIV-SP AIRPLANES ONLY) Page PC - 1
GIV-SP Landing Field Length:
Anti-Skid System Operative - Flaps 39° AFM 5.11
For airplanes SN 1214 and subsequent and SN 1000 thru 1213
with ASC 190 incorporated.
CAUTION: THE GIV-SP MAXIMUM LANDING WEIGHT IS 66000
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 4340 4470 4600 4760 4950 5260
50000 4570 4710 4860 5040 5260 5600
55000 4800 4950 5120 5310 5550 5930
60000 5030 5200 5380 5600 5860 6270
65000 5260 5440 5640 5880 6160 6610
70000 5500 5690 5910 6160 6480 6940
75000 5730 5940 6170 6440 6770 7270
Quick Reference Handbook
GIV-SP PERFORMANCE REVISION 7
Page PC - 2 (GIV-SP AIRPLANES ONLY) May 30/02
GIV-SP Landing Speed Schedule AFM 5.11
For airplanes SN 1214 and subsequent and SN 1000 thru 1213
with ASC 190 incorporated.
The following guidance is provided to assist in the use of the
charts in this section:
Tire speed limits occur when touchdown speeds exceeds 195.5
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