Page 2-7
Sub-section 2
PREFLIGHT
Section IV - FLIGHT PLANNING DATA
Pilot’s Operating Manual
Initial Issue: Feb, 2002
FUEL LOADING PLAN
Hawker 800XP Pro Line 21
t
t
Part 1 PERMISSIBLE WEIGHTS lb
(from AFM)
Permissible
Take-off Weight
APR ‘ON’
Permissible
Landing Weight
DESTINATION
ALTERNATE
Maximum Zero Fuel Weight
Part 2 ZERO FUEL WEIGHT lb
Operating Weight (from Weight
and Balance Manual)
Passengers (No. of Pax x
standard weight allowance)
Baggage
Zero Fuel Weight
Check does not exceed
Part 3A FLIGHT PLAN DISTANCES
Sector
Distance nm
Diversion
Distance nm
Still Air Time
min.
Still Air Time
min.
Mean Still
Air
Speed=
Mean Still
Air
Speed=
Equivalent
Sector Still Air
Distance nm
Equivalent
Diversion Still
Air Distance nm
Part 3B FLIGHT PLAN Weights lb
Times min and fuels lb
Zero Fuel Weight
Approach fuel
Taxi-in fuel
Diversion Arrival Weight
Diversion fuel
Weight at end of Hold
Holding fuel for min.
at altitude.
Additional fuel Reserves
(if required)
Destination Arrival Weight
Interpolation ‘scratchpad’
ISA
Arr. wt
Time
Fuel
Time
Fuel
ISA
Arr. wt
Interpolation
values
Interpolated
at
ISA
Arr. wt
Time
Fuel
Time
Fuel
ISA
Arr. wt
Sector
Time
Sector Fuel
Take-off Weight
Part 4 FUEL SUMMARY
Approach,
Taxi-in
Diversion
Holding
Additional Reserves (if required)
Sector
Taxi-out
TOTAL FUEL REQUIRED
Part 5 LOADING CHECK (optional)
Zero Fuel Weight
Values
must not
exceed:
Total Fuel required
RAMP WEIGHT
28120 lb
Taxi-out fuel
ACTUAL TAKE-OFF WEIGHT
Should equal
Fuel to Destination
DESTINATION LANDING
WEIGHT
Diversion fuel
LANDING WEIGHT AT
ALTERNATE
Trip Date:
.................................
From:
.................................................
Destination:
....................................................
Alternate:
...............................................
FUEL LOADING PLAN
1
2
3
4
5
4
5
6
7
8
9
60 x
6
7
60 x
8
9
10
11
12
13
14
10
11
12
13
15
5
15
5
+
15
14
10
+
13
16
17
14
-
16
11
17
-
11
1
2
3
Содержание Hawker 800XP
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