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时间:2010-10-11 23:22来源:蓝天飞行翻译 作者:admin
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Non-SP GIV Takeoff Climb Requirements: Climb
Limited Weights: Flaps 20° - Minimum Gradient AFM 5.3
Conditions:
• For FAA Climb Requirements
• 20° Flaps
• Normal ECS Bleeds
Takeoff Limited Weight (Pounds) For
Ambient Airport Pressure Altitudes As Shown
Temp:
°C
Sea
Level
2000
Feet
4000
Feet
6000
Feet
8000
Feet
10000
Feet
-10 & Below 73200 73200 73200 73200 73200 72700
-5 73200 73200 73200 73200 73200 72200
0 73200 73200 73200 73200 73200 71400
5 73200 73200 73200 73200 73200 69200
10 73200 73200 73200 73200 72000 66000
15 73200 73200 73200 73200 68400 62700
20 73200 73200 73200 70200 64800 59300
25 73200 73200 72300 66600 61300 56000
30 73200 73200 68500 63000 57800 52600
35 73200 70300 64900 59500 - -
40 72400 66600 61400 - - -
45 68700 63200 - - - -
50 65100 - - - - -
Quick Reference Handbook
REVISION 7 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PA -35
Non-SP GIV Takeoff Climb Requirements: Climb
Limited Weights: Flaps 10° - Minimum Gradient AFM 5.3
Conditions:
• For FAA Climb Requirements
• 10° Flaps
• Normal ECS Bleeds
Takeoff Limited Weight (Pounds) For
Ambient Airport Pressure Altitudes As Shown
Temp:
°C
Sea
Level
2000
Feet
4000
Feet
6000
Feet
8000
Feet
10000
Feet
0 & Below 73200 73200 73200 73200 73200 73200
5 73200 73200 73200 73200 73200 73200
10 73200 73200 73200 73200 73200 72200
15 73200 73200 73200 73200 73200 70500
20 73200 73200 73200 73200 72500 66500
25 73200 73200 73200 73200 68600 62800
30 73200 73200 73200 70400 64800 59200
35 73200 73200 72500 66700 - -
40 73200 73200 68700 - - -
45 73200 70400 - - - -
50 72500 - - - - -
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PA - 36 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Takeoff Climb Requirements:
Climb Limited Weights:
Flaps 20° - Standard Instrument Departure GIV-OIS-7
NOTE: For complete text and examples, see GIV Operating Manual Section
11-04-60 or Operational Information Supplement number GIV-OIS-07:
Standard Instrument Departure (SID) Climb Performance.
GIV TAKEOFF GROSS WEIGHT LIMITED BY REQUIRED SID CLIMB GRADIENT
1000 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 54.6 47.8 NA NA NA NA NA NA
< -18 14,000 56.6 49.6 NA NA NA NA NA NA
< -14 12,000 60.9 53.3 47.4 NA NA NA NA NA
< -10 10,000 65.3 57.2 51.0 45.8 NA NA NA NA
< -5 < -6 8,000 69.9 61.3 54.6 49.2 NA NA NA NA
< -2 6,000 74.6 65.5 58.3 52.6 47.9 NA NA NA
< 2 4,000 74.6 70.0 62.3 56.2 51.2 47.0 NA NA
< 6 2,000 74.6 73.0 65.0 58.5 53.4 49.1 45.3 NA
< 10 0 74.6 74.6 67.4 60.6 55.2 50.8 46.9 NA
-15 15,000 54.1 47.4 NA NA NA NA NA NA
-13 14,000 56.2 49.2 NA NA NA NA NA NA
-9 12,000 60.4 52.9 47.0 NA NA NA NA NA
-5 10,000 64.8 56.7 50.6 45.5 NA NA NA NA
0 -1 8,000 69.5 60.9 54.2 48.9 NA NA NA NA
3 6,000 74.3 65.1 58.0 52.3 47.6 NA NA NA
7 4,000 74.6 69.6 61.9 55.8 50.9 46.7 NA NA
11 2,000 74.6 73.6 65.5 59.0 53.8 49.4 45.6 NA
15 0 74.6 74.6 67.4 60.6 55.2 50.8 46.9 NA
-10 15,000 53.7 47.0 NA NA NA NA NA NA
-8 14,000 55.7 48.8 NA NA NA NA NA NA
-4 12,000 59.8 52.4 46.6 NA NA NA NA NA
0 10,000 64.0 56.1 50.0 NA NA NA NA NA
5 4 8,000 68.5 60.1 53.5 48.2 NA NA NA NA
8 6,000 73.4 64.3 57.2 51.7 47.0 NA NA NA
12 4,000 74.6 69.5 61.8 55.7 50.8 46.6 NA NA
16 2,000 74.6 72.8 64.8 58.4 53.2 48.9 45.2 NA
20 0 74.6 74.6 67.3 60.6 55.2 50.8 46.9 NA
-5 15,000 52.8 46.1 NA NA NA NA NA NA
-3 14,000 54.7 47.9 NA NA NA NA NA NA
1 12,000 58.6 51.4 45.6 NA NA NA NA NA
5 10,000 62.7 55.0 49.0 NA NA NA NA NA
10 9 8,000 67.2 58.9 52.5 47.3 NA NA NA NA
13 6,000 72.6 63.7 56.7 51.2 46.5 NA NA NA
17 4,000 74.6 68.2 60.7 54.8 50.0 45.8 NA NA
21 2,000 74.6 72.1 64.2 57.8 52.7 48.4 NA NA
25 0 74.6 74.6 67.3 60.6 55.2 50.8 46.9 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
 
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