Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-9
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
WORKED EXAMPLE
The pages that follow contain a worked example using the FUEL LOADING PLAN. The example is
based on the flight profile in Figure 1. The reader is progressively guided through the Parts of the FUEL
LOADING PLAN with text describing each Part before moving to the next Part.
DATA
The data used for the worked example is listed below:
Departure Airfield Elevation ...........................................................2000 ft
Runway Length................................................. 5800 ft dry
Runway Slope................................................... Zero
No Clearway, Stopway or Obstacles
Temperature ..................................................... 66
°
F
Wind Component.............................................. Zero
Distance to Destination ........................................................................... 1900 nm
En Route Wind........................................................................................ 20 kt tailwind
En Route Temperature............................................................................ ISA +5° C
High Speed Procedure Required
Destination Airfield Elevation ...........................................................2000 ft
Runway Length................................................. 4350 ft dry
Runway Slope................................................... Zero
Temperature ..................................................... 77
°
F
Wind Component.............................................. Zero
Holding Allowance 30 Minutes at 5000 ft ISA +5° C
Diversion Distance............................................................ 120 nm
Wind ................................................................. 20 kt headwind
Temperature ..................................................... ISA +5° C
Alternate Airfield Elevation ........................................................... Sea Level
Runway Length................................................. 4000 ft dry
Runway Slope................................................... Zero
Temperature ..................................................... 86
°
F
Wind Component.............................................. 10 kt headwind
Payload 4 Passengers Plus 120 lb Baggage