Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 5-3
Pilot’s Operating Manual
Original Issue: Feb, 2002
Sub-section 5
NORMAL DESCENT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
INTRODUCTION
Descent Fuel, Distance and Time are tabulated in this Sub-section against Arrival Weight.
The data is presented for a descent at 0.76 IMN/285/250 KIAS in ISA conditions.
The descent procedure specifies a constant 1000 ft/min rate of descent down to 37,000 ft, where the
thrust is reduced to idle for the remainder of the descent to 1500 ft.
The effect of temperature on descent fuel, distance and time is negligible and the descent ends at the
arrival weight at 160 KIAS and 1500 ft altitude.
No allowances are included for Approach or Landing.