P/N 140-590035-0005TC2
Jun 2, 2009
Page 3 of 12
TEMPORARY CHANGE
P/N 140-590035-0005TC2
SECTION 5 - PERFORMANCE
Sub-section 5.25 - NET TAKE-OFF FLIGHT PATH - APR ON
NET TAKE-OFF FLIGHT PATH
SECOND SEGMENT NET GRADIENT - FLAPS 0°
Under Associated Conditions, read the following after NOTE 2:
3. For a turning climb, up to and including a 15° bank angle, decrease net climb
gradient by 1.0 percentage point.
Instructions for Use of Chart
The use of the chart is illustrated by the broken arrowed 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 guidelines to the
appropriate weight.
• Move horizontally to the line on the right.
• Proceed upwards to the wind reference line and through the wind correction grid to
obtain the net gradient.
• Finally correct for bank angle, if required, by applying the associated bank angle
correction (e.g. Charted Net Gradient - Correction = 4.5% - 1.0% = 3.5%).
FAA Approved Airplane Flight Manual, P/N 140-590035-0005.
All Hawker 850XP airplanes.
To provide a correction factor for turning climbs.
PUBLICATION AFFECTED:
AIRPLANE EFFECTIVITY:
DESCRIPTION OF CHANGE:
FILING INSTRUCTIONS:
Insert Temporary Change 2 into the Airplane Flight Manual
Section 5 - PERFORMANCE as follows:
Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON
• Page 1 of 12 to face AFM Page 8.
• Page 3 of 12 to face AFM Page 12.
Sub-section 5.40: EN-ROUTE DATA
• Page 5 of 12 to face AFM Page 2.
Sub-section 5.55: GROSS PERFORMANCE
• Page 7 of 12 to face AFM Page 4.
• Page 9 of 12 to face AFM Page 8.
• Page 11 of 12 to face AFM Page 12.
For Training Purposes Only
