Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 8-3
Section IV - Sub-section 8
GEAR DOWN PERFORMANCE
Pilot’s Operating Manual
P/N 140-590032-0007
Revision A3: Apr, 2008
INTRODUCTION
This Sub-section provides gear down flight planning data for climb, cruise and descent and is
for use in planning abnormal operations only. Normal operations require landing gear retraction
capability to meet AFM takeoff and climb performance. Data is provided up to the maximum
permissible altitude of 20,000 feet with the landing gear extended.
Climb time, fuel and distance are tabulated versus take-off weight and altitude at the top of the
climb. The gear down climb speed profile commences at 160 KIAS at 1000 feet and accelerates
to 210 KIAS at 5000 feet (maintaining airspeed below V
LE
/V
LO
minus 10 kts, 210 KIAS). Data
is provided for a range of temperatures from ISA -15° C to ISA +20° C.
Cruise data is tabulated for 210 KIAS at altitudes from 1000 feet to 20,000 feet. Data is provided
for a range of temperatures from ISA -15° C to ISA +20° C.
Descent data is tabulated against arrival weight. The descent speed is 210 KIAS down to the
1500 foot arrival altitude. The effect of temperature variation on descent fuel, distance, and time
is negligible.
P/N 140-590032-0007
Revision A5: Feb, 2012