Hawker 850XP Pro Line 21 Airplane Flight Manual
Page 12
FAA Approved
Original Issue: Feb 28, 2006
Sub-section - 5.25
NET TAKE-OFF FLIGHT PATH
NET TAKE-OFF FLIGHT PATH
SECOND SEGMENT NET GRADIENT - FLAPS 0°
Figure 5.25.4 shows the second segment net gradient of climb at the mean height of this
segment.
Associated Conditions
NOTES:
1. To take account of engine antice bleed, add 10°
C to the actual air temperature
before entering the chart.
2. The wind grid is factored in such a way that an effect of not more than 50% of
headwinds and not less than 150% of tailwinds is obtained. Reported winds may
therefore be used directly in the grid.
Instructions for Use of Chart
The use of the chart is illustrated by the arrowed broken lines:
• Enter the chart with the air temperature and move up to the appropriate field pressure altitude.
• Proceed across to the weight grid reference line and then follow the guide lines to the
appropriate weight.
• Move horizontally to the line on the right.
• Finally proceed upwards to the wind reference line and through the wind correction grid to
obtain the net gradient.
Engines
One engine operating at maximum thrust with APR ON.
Engine Bleed Air
All air bleeds off; see NOTE 1 for the effect of engine antice bleed.
Flaps
0°
Landing Gear
Up
Airspeed
Take-off safety speed V
2
(refer to TABULATED TAKEOFF DATA Sub-
section 5.20)
For Training Purposes Only