Page 4-3
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 4
CRUISE - ENROUTE
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
INTRODUCTION
Cruise true airspeed, fuel flow and indicated airspeed are tabulated in this Sub-section for a range of
temperatures from ISA -10° C to ISA + 20° C , for three procedures:
• High speed Cruise (V
MO
/M
MO
/Maximum Cruise Thrust).
• Intermediate Cruise (280 KIAS/0.75 IMN).
• Long Range Cruise (230/220 KIAS/0.70 IMN).
Graphical charts of nautical air miles per lb of fuel versus weight and speed appear in this Sub-section
with altitudes being covered from 20,000 ft to 41,000 ft in ISA conditions.
The enroute fuel check, located at the back of this Sub-section, allows quick estimation of the fuel
required to complete the flight to a destination.
