Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 3-3
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 3
CLIMB
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
INTRODUCTION
Climb fuel, distance and time are tabulated versus take-off weight and altitude at top of climb.
Fuel and time for takeoff and initial climb to 160 KIAS at 1000 ft are included. The data is presented for
temperatures in the range from ISA -15° C to ISA + 20° C.
TABLES ARE PRESENTED FOR TWO CLIMBS:
Normal Climb and Optimum Time-to-Height Climb. Both climb procedures commence at 160 KIAS at
1000 ft and accelerate to 250 KIAS at 5000 ft.
NORMAL CLIMB
(Reference the charts on pages 3-4 through 3-17)
From 5000 ft, the normal climb continues at 250 KIAS to 32,000 ft
at which IMN = 0.70. The final part of the climb to cruise altitude is at IMN = 0.70.
OPTIMUM TIME-TO-HEIGHT CLIMB (Reference the charts on pages 3-18 through 3-29)
From 5000 ft, the optimum time-to-height climb continues at 250 KIAS to 28,000 ft
at which IMN = 0.63. The final part of the climb to cruise altitude is at IMN = 0.63.
A GRAPH IS PRESENTED FOR PRESSURE RATE OF CLIMB:
NORMAL PROCEDURE PRESSURE RATE OF CLIMB
This data is provided in Figure 1 which shows the instantaneous rates of climb for varying altitudes,
climb weights and temperatures relative to ISA, with ANTICE OFF.