曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

FUEL LOADING of the Weight and Balance Computation Form.
10. Enter the sums of the values on line 3 and 4 onto line 5 RAMP WEIGHT of the Weight and
Balance Computation Form.
11. Divide the ramp moment index by the ramp weight and multiply by 100 (1000) to determine
the ramp weight center-of-gravity.
12. Check the ramp weight by locating the weight and center-of-gravity on the Example Centerof-
Gravity Limits Envelope Graph (See Figures 30 - 31).
NOTE
Approved points are located below the maximum ramp weight line.
13. Enter the taxi fuel weight and moment index on line 6 LESS FUEL FOR TAXIING of the
Weight and Balance Computation Form. A standard 85 pound (38.56 kilogram) burn-off is
assumed. The moment index for taxi is the difference between the moment index of the fuel
loaded and the moment index of the fuel remaining on-board after taxi.
14. Enter the differences between the values on lines 5 and 6 onto line 7 TAKEOFF WEIGHT of
the Weight and Balance Computation Form.
15. Divide the takeoff moment index by the Takeoff Weight and multiply by 100 (1000) to
determine the takeoff center-of-gravity. Enter the takeoff center-of-gravity on line 7 of the
Weight and Balance Computation Form.
16. Check the takeoff weight by locating the weight and center-of-gravity on the Example
Center-of-Gravity Limits Envelope Graph (See Figures 30 - 31).
NOTE
Approved points are located inside the enveloped below the maximum takeoff weight
line.
(Continued Next Page)
6-52 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - EXAMPLES
FAA APPROVED
U.S.
Sample Loading Problem (Continued)
17. Determine the estimated weight of the fuel to be used in flight. The moment index of the fuel
used in flight is the difference between the moment index of the fuel remaining after taxi and
the moment index of the fuel remaining after reaching the destination.
18. Enter the weight and moment index of the fuel used in flight on line 8 LESS FUEL TO
DESTINATION of the Weight and Balance Computation Form.
19. Enter the differences between the values on lines 7 and 8 onto line 9 LANDING WEIGHT of
the Weight and Balance Computation Form.
20. Divide the landing moment index by the landing weight and multiply by 100 (1000) to
determine the landing center-of-gravity. Enter the landing center-of-gravity on line 9 of the
Weight and Balance Computation Form.
21. Check the landing weight by locating the weight and center-of-gravity on the Example
Center-of-Gravity Limits Envelope Graph (See Figures 30 - 31).
NOTE
Approved points are located inside the envelope below the Maximum Landing Weight
line.
510WB-00 6-53
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - EXAMPLES
FAA APPROVED
U.S.
EXAMPLE WEIGHT AND BALANCE COMPUTATION
FORM - U.S. UNITS
Figure 28*
6-54 510WB-01
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - EXAMPLES
FAA APPROVED
U.S.
EXAMPLE WEIGHT AND BALANCE COMPUTATION
FORM - METRIC UNITS
Figure 29*
510WB-01 6-55
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - EXAMPLES
FAA APPROVED
U.S.
EXAMPLE CENTER-OF-GRAVITY LIMITS ENVELOPE
GRAPH - U.S. UNITS
Figure 30
6-56 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - EXAMPLES
FAA APPROVED
U.S.
EXAMPLE CENTER-OF-GRAVITY LIMITS ENVELOPE
GRAPH - METRIC UNITS
Figure 31
510WB-00 6-57/6-58

MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
AIRPLANE REPORTS - TABLE OF CONTENTS
FAA APPROVED
U.S.
AIRPLANE REPORTS
TABLE OF CONTENTS
Page
Equipment List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-61
Forms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-61
Airplane Weighing Form - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-62
Airplane Weighing Form - Metric Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-63
Weight and Balance Computation Form - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-64
Weight and Balance Computation Form - Metric. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-65
Center-of-Gravity Limits Envelope Graph - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-66
Center-of-Gravity Limits Envelope Graph - Metric Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-67
Weight and Balance Record - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-68
　
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