Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

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Page 2-10
Pilot’s Operating Manual
Revision A1: Nov, 2002
Sub-section 2
PREFLIGHT
Hawker 800XP Pro Line 21
Section IV - FLIGHT PLANNING DATA
CALCULATION
Part 1 - PERMISSIBLE WEIGHTS (from AFM)
Permissible Take-off Weight
Temperature
°
C = 5 (
°
F -32) = 19° C
9
Since there are no obstacles the permissible take-off weight will be the lowest of:
1. Maximum take-off weight from AFM Section 2 = 28,000 lb.
2. WAT limited weight from AFM Sub-section 5.15.
3. Field Length limited weight from AFM Sub-section 5.20.
From AFM Sub-section 5.15 for departure airfield it can be seen that the WAT and tire speed limits at
both flap settings are greater than 28,000 lb.
From AFM Sub-section 5.20, assuming Flaps 15
°
:
Allowable take-off weight = Greater than 28,000 lb.
Permissible take-off weight = 28,000 lb.
Permissible Landing Weight at Destination
Temperature
°
C = 5 (77 -32) = 25° C
9
From AFM Section 2 Maximum Landing Weight = 23,350 lb.
From AFM Sub-section 5.45 Landing WAT limit = 25,170 lb.
From AFM Sub-section 5.50, the maximum weight for a landing field length of 4350 ft = 21,500 lb.
Permissible landing weight at the destination is therefore the lowest of these three weights,
i.e.
21,500 lb.