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< 6 2,000 74.6 74.6 69.7 62.4 56.4 51.7 47.7 NA
< 10 0 74.6 74.6 72.2 64.7 58.5 53.5 49.4 45.9
-15 15,000 59.6 51.6 45.5 NA NA NA NA NA
-13 14,000 61.8 53.5 47.2 NA NA NA NA NA
-9 12,000 66.4 57.5 50.7 45.4 NA NA NA NA
-5 10,000 71.1 61.6 54.3 48.7 NA NA NA NA
0 -1 8,000 74.6 65.9 58.2 52.1 47.3 NA NA NA
3 6,000 74.6 70.5 62.2 55.7 50.5 46.3 NA NA
7 4,000 74.6 74.6 66.4 59.5 53.8 49.3 45.6 NA
11 2,000 74.6 74.6 70.2 62.9 56.9 52.0 48.1 NA
15 0 74.6 74.6 72.2 64.7 58.5 53.4 49.3 45.9
-10 15,000 59.1 51.1 45.1 NA NA NA NA NA
-8 14,000 61.3 53.0 46.8 NA NA NA NA NA
-4 12,000 65.7 56.9 50.2 NA NA NA NA NA
0 10,000 70.3 60.8 53.7 48.1 NA NA NA NA
5 4 8,000 74.6 65.1 57.4 51.4 46.7 NA NA NA
8 6,000 74.6 69.6 61.4 55.0 49.8 45.7 NA NA
12 4,000 74.6 74.6 66.3 59.4 53.7 49.2 45.5 NA
16 2,000 74.6 74.6 69.5 62.2 56.3 51.5 47.6 NA
20 0 74.6 74.6 72.2 64.6 58.5 53.4 49.3 45.9
-5 15,000 58.1 50.2 NA NA NA NA NA NA
-3 14,000 60.1 52.0 45.9 NA NA NA NA NA
1 12,000 64.4 55.8 49.2 NA NA NA NA NA
5 10,000 68.8 59.6 52.6 47.2 NA NA NA NA
10 9 8,000 73.6 63.8 56.3 50.4 45.8 NA NA NA
13 6,000 74.6 68.9 60.8 54.5 49.4 45.3 NA NA
17 4,000 74.6 73.7 65.1 58.3 52.8 48.4 NA NA
21 2,000 74.6 74.6 68.8 61.6 55.7 51.0 47.2 NA
25 0 74.6 74.6 72.1 64.6 58.5 53.4 49.3 45.9
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 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PA -49
Non-SP GIV Climb Limited Weights, Flaps 10°, Standard
Instrument Departure, ctd… GIV-OIS-7
GIV TAKEOFF GROSS WEIGHT LIMITED BY REQUIRED SID CLIMB GRADIENT
1000 FT AGL, FLAPS 10, 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 56.8 49.2 NA NA NA NA NA NA
2 14,000 58.8 50.9 NA NA NA NA NA NA
6 12,000 63.0 54.6 48.2 NA NA NA NA NA
10 10,000 68.0 58.9 51.9 46.6 NA NA NA NA
15 14 8,000 72.8 63.0 55.6 49.9 45.3 NA NA NA
18 6,000 74.6 67.6 59.7 53.5 48.5 NA NA NA
22 4,000 74.6 72.4 63.9 57.3 51.9 47.6 NA NA
26 2,000 74.6 74.6 68.1 61.0 55.1 50.5 46.7 NA
30 0 74.6 74.6 71.7 64.2 58.1 53.1 49.0 45.6
5 15,000 55.5 48.1 NA NA NA NA NA NA
7 14,000 57.5 49.8 NA NA NA NA NA NA
11 12,000 62.1 53.8 47.5 NA NA NA NA NA
15 10,000 66.6 57.6 50.9 45.7 NA NA NA NA
20 19 8,000 71.3 61.8 54.6 48.9 NA NA NA NA
23 6,000 74.6 66.3 58.6 52.5 47.7 NA NA NA
27 4,000 74.6 70.7 62.5 56.0 50.8 46.6 NA NA
31 2,000 74.6 74.1 65.5 58.7 53.2 48.8 45.1 NA
35 0 74.6 74.6 68.4 61.3 55.5 50.8 47.0 NA
10 15,000 54.7 47.3 NA NA NA NA NA NA
12 14,000 56.7 49.1 NA NA NA NA NA NA
16 12,000 60.8 52.6 46.5 NA NA NA NA NA
20 10,000 65.1 56.4 49.8 NA NA NA NA NA
25 24 8,000 69.8 60.5 53.4 48.0 NA NA NA NA
28 6,000 74.6 64.9 57.3 51.4 46.7 NA NA NA
32 4,000 74.6 67.8 60.0 53.8 48.8 NA NA NA
36 2,000 74.6 70.7 62.5 56.0 50.9 46.7 NA NA
40 0 74.6 73.6 65.1 58.3 52.9 48.5 NA NA
15 15,000 53.4 46.2 NA NA NA NA NA NA
17 14,000 55.4 47.9 NA NA NA NA NA NA
21 12,000 59.5 51.5 45.6 NA NA NA NA NA
25 10,000 63.7 55.2 48.8 NA NA NA NA NA
30 29 8,000 67.9 58.9 52.0 46.7 NA NA NA NA
33 6,000 71.3 61.9 54.7 49.1 NA NA NA NA
37 4,000 74.4 64.6 57.1 51.3 46.7 NA NA NA
41 2,000 74.6 67.2 59.4 53.3 48.5 NA NA NA
45 0 74.6 69.9 61.9 55.4 50.4 46.3 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
NON-SP GIV PERFORMANCE REVISION 7
Page PA - 50 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Climb Limited Weights, Flaps 10°, Standard
Instrument Departure, ctd… GIV-OIS-7
GIV TAKEOFF GROSS WEIGHT LIMITED BY REQUIRED SID CLIMB GRADIENT
2000 FT AGL, FLAPS 10, 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
　
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