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< 2 4,000 74.6 67.2 60.1 54.4 49.7 45.7 NA NA
< 6 2,000 74.6 70.7 63.2 57.2 52.3 48.2 NA NA
< 10 0 74.6 74.6 66.8 60.3 55.1 50.8 46.9 NA
-15 15,000 51.6 45.2 NA NA NA NA NA NA
-13 14,000 53.4 46.9 NA NA NA NA NA NA
-9 12,000 57.5 50.6 45.1 NA NA NA NA NA
-5 10,000 61.7 54.4 48.6 NA NA NA NA NA
0 -1 8,000 66.2 58.3 52.2 47.2 NA NA NA NA
3 6,000 70.9 62.5 55.8 50.6 46.1 NA NA NA
7 4,000 74.6 66.8 59.7 54.1 49.4 45.4 NA NA
11 2,000 74.6 71.1 63.5 57.5 52.6 48.4 NA NA
15 0 74.6 74.5 66.6 60.1 54.9 50.7 46.9 NA
-10 15,000 50.8 NA NA NA NA NA NA NA
-8 14,000 52.6 46.2 NA NA NA NA NA NA
-4 12,000 56.9 50.2 NA NA NA NA NA NA
0 10,000 61.1 53.8 48.1 NA NA NA NA NA
5 4 8,000 65.4 57.6 51.6 46.6 NA NA NA NA
8 6,000 70.0 61.7 55.1 50.0 45.5 NA NA NA
12 4,000 74.6 66.5 59.5 53.9 49.2 45.2 NA NA
16 2,000 74.6 70.4 62.9 56.9 52.1 47.9 NA NA
20 0 74.6 74.1 66.2 59.8 54.7 50.4 46.7 NA
-5 15,000 49.5 NA NA NA NA NA NA NA
-3 14,000 51.2 NA NA NA NA NA NA NA
1 12,000 55.8 49.2 NA NA NA NA NA NA
5 10,000 59.9 52.8 47.1 NA NA NA NA NA
10 9 8,000 64.1 56.5 50.6 45.6 NA NA NA NA
13 6,000 69.3 61.0 54.6 49.5 45.0 NA NA NA
17 4,000 74.1 65.3 58.5 53.0 48.4 NA NA NA
21 2,000 74.6 69.5 62.1 56.2 51.4 47.3 NA NA
25 0 74.6 73.4 65.6 59.3 54.2 50.0 46.2 NA
NOTES: 1. Maximum climb weights are limited by the design MAX TOGW of 74,600 lb for the GIV-SP and
73,200 for the GIV.
2. Increase MAX TOGW by 300 lb for each 10 knots of headwind up to a maximum of 40 knots.
Data not valid for tailwinds.
3. Cowl anti-ice bleeds are assumed ON for temperatures below 10° C; wing anti-ice bleeds
prohibited.
Quick Reference Handbook
REVISION 7 GIV-SP PERFORMANCE
May 30/02 (GIV-SP AIRPLANES ONLY) Page PA - 43
GIV-SP Climb Limited Weights, Flaps 20°, Standard Instrument
Departure, ctd… GIV-OIS-07
GIV TAKEOFF GROSS WEIGHT LIMITED BY REQUIRED SID CLIMB GRADIENT
4000 FT AGL, FLAPS 20, ONE ENGINE OPERATING, ctd…
DELTA AIRPORT AIRPORT
ISA AMBIENT PRESS TAKEOFF GROSS WEIGHT (1000 LB)
TEMP TEMP ALTITUDE REQUIRED SID CLIMB GRADIENT (FT/NM)
(DEG C) (DEG C) (FT) 200 300 400 500 600 700 800 900
0 15,000 48.0 NA NA NA NA NA NA NA
2 14,000 49.6 NA NA NA NA NA NA NA
6 12,000 54.7 48.1 NA NA NA NA NA NA
10 10,000 59.1 52.1 46.5 NA NA NA NA NA
15 14 8,000 63.3 55.8 50.0 45.0 NA NA NA NA
18 6,000 67.9 59.9 53.6 48.5 NA NA NA NA
22 4,000 72.7 64.1 57.4 52.0 47.5 NA NA NA
26 2,000 74.6 68.5 61.3 55.5 50.8 46.7 NA NA
30 0 74.6 72.6 64.9 58.7 53.7 49.4 45.7 NA
5 15,000 46.3 NA NA NA NA NA NA NA
7 14,000 47.9 NA NA NA NA NA NA NA
11 12,000 53.9 47.4 NA NA NA NA NA NA
15 10,000 57.8 51.0 45.5 NA NA NA NA NA
20 19 8,000 62.0 54.7 48.9 NA NA NA NA NA
23 6,000 66.5 58.7 52.6 47.5 NA NA NA NA
27 4,000 71.1 62.7 56.1 50.9 46.4 NA NA NA
31 2,000 74.6 66.5 59.5 53.9 49.3 45.2 NA NA
35 0 74.6 70.0 62.6 56.7 51.8 47.7 NA NA
10 15,000 45.4 NA NA NA NA NA NA NA
12 14,000 47.0 NA NA NA NA NA NA NA
16 12,000 52.7 46.3 NA NA NA NA NA NA
20 10,000 56.6 49.9 NA NA NA NA NA NA
25 24 8,000 60.8 53.6 47.9 NA NA NA NA NA
28 6,000 65.0 57.4 51.4 46.4 NA NA NA NA
32 4,000 68.9 60.8 54.4 49.3 NA NA NA NA
36 2,000 72.5 64.0 57.3 52.0 47.4 NA NA NA
40 0 74.6 66.7 59.7 54.1 49.5 45.5 NA NA
15 15,000 NA NA NA NA NA NA NA NA
17 14,000 45.2 NA NA NA NA NA NA NA
21 12,000 51.5 45.2 NA NA NA NA NA NA
25 10,000 55.3 48.8 NA NA NA NA NA NA
30 29 8,000 59.2 52.2 46.6 NA NA NA NA NA
33 6,000 62.8 55.4 49.7 NA NA NA NA NA
37 4,000 66.1 58.3 52.3 47.3 NA NA NA NA
41 2,000 69.0 60.9 54.6 49.5 45.1 NA NA NA
45 0 71.9 63.5 56.9 51.6 47.1 NA NA NA
NOTES: 1. Maximum climb weights are limited by the design MAX TOGW of 74,600 lb for the GIV-SP and
73,200 for the GIV.
2. Increase MAX TOGW by 300 lb for each 10 knots of headwind up to a maximum of 40 knots.
Data not valid for tailwinds.
3. Cowl anti-ice bleeds are assumed ON for temperatures below 10° C; wing anti-ice bleeds
prohibited.
Quick Reference Handbook
GIV-SP PERFORMANCE REVISION 7
Page PA - 44 (GIV-SP AIRPLANES ONLY) May 30/02
GIV-SP Climb Limited Weights, Flaps 20°, Standard Instrument
Departure, ctd… GIV-OIS-07
GIV TAKEOFF GROSS WEIGHT LIMITED BY REQUIRED SID CLIMB GRADIENT
5000 FT AGL, FLAPS 20, ONE ENGINE OPERATING
DELTA AIRPORT AIRPORT
ISA AMBIENT PRESS TAKEOFF GROSS WEIGHT (1000 LB)
TEMP TEMP ALTITUDE REQUIRED SID CLIMB GRADIENT (FT/NM)
(DEG C) (DEG C) (FT) 200 300 400 500 600 700 800 900
< -20 15,000 51.6 NA NA NA NA NA NA NA
< -18 14,000 53.0 46.6 NA NA NA NA NA NA
　
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