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 = 14 000 kg
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 2/10
FCOM 19 AUG 10
DATA
Applicable to: MSN,
4473
Dry Operating Weight = 42 500 kg and CG = 27 % (H-arm = 18.93 m)
Deviation or adjustment = + 100 kg in zone F
Cargo = 5 500 kg with the following distribution : cargo 1 = 2 000 kg ; cargo 3 = 1 500 kg ; cargo 4 =
1 500 kg ; cargo 5 = 500 kg
Passengers = 145 pax with the following distribution : cabin OA = 50 ; cabin OB = 55 ; cabin OC = 40
Fuel = 13 000 kg
DESCRIPTION
Applicable to: ,
, MSN,,
a. Enter Master data in (1).
b. Compute Dry Operating Weight Index using the formula indicated in (2) and report in (3).
c. Dry Operating Index = 43.96.
d. Enter weight deviation or adjustment in (4) and read corresponding index variation in (5) : + 1.70.
e. Calculate corrected index and report in (6) : 45.66.
f. Enter master data in table (7) and determine Zero Fuel Weight : 72 720 kg and Takeoff Weight :
89 720 kg.
g. Enter cargo weight and passenger number per compartment in (8).
h. Enter index scale (9) with corrected index and proceed through cargo and passenger scales (10).
i. From the final point draw a vertical line which intersects (12) the zero fuel weight horizontal line
(11).
j. Check if the intersection point is within the Zero Fuel Weight operational limits, if not rearrange
cargo loading.
k. Read in table (13) the fuel index correction : – 10 and carry forward in fuel scale (14).
l. From this point draw a vertical line which intersects (16) the takeoff weight horizontal line (15).
m. Check if the intersection point is within the Takeoff Weight operational limits.
n. Read zero fuel weight and CG position : 32 % and fill in table (17).
o. Read takeoff CG position : 28 % and fill in table (18).
CAUTION If there is no customized trim sheet for your airline in this section, do not use the
information enclosed herein for day to day operation as margins and load CG vary
with cabin and cargo layout.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 3/10
FCOM 19 AUG 10
DESCRIPTION
Applicable to:
a. Enter Master data in (1).
b. Compute Dry Operating Weight Index using the formula indicated in (2) and report in (3).
c. Dry Operating Index = 50.85.
d. Enter weight deviation or adjustment in (4) and read corresponding index variation in (5) : + 1.21.
e. Calculate corrected index and report in (6) : 51.06.
f. Enter master data in table (7) and determine Zero Fuel Weight : 54 680 kg and Takeoff Weight :
68 680 kg.
g. Enter cargo weight and passenger number per compartment in (8).
h. Enter index scale (9) with corrected index and proceed through cargo and passenger scales (10).
i. From the final point draw a vertical line which intersects (12) the zero fuel weight horizontal line
(11).
j. Check if the intersection point is within the Zero Fuel Weight operational limits, if not rearrange
cargo loading.
k. Read in table (13) the fuel index correction : – 4 and carry forward in fuel scale (14).
l. From this point draw a vertical line which intersects (16) the takeoff weight horizontal line (15).
m. Check if the intersection point is within the Takeoff Weight operational limits.
n. Read zero fuel weight and CG position : 31 % and fill in table (17).
o. Read takeoff CG position : 28.4 % and fill in table (18).
CAUTION If there is no customized trim sheet for your airline in this section, do not use the
information enclosed herein for day to day operation as margins and load CG vary
with cabin and cargo layout.
DESCRIPTION
Applicable to: MSN,
4473
a. Enter Master data in (1).
b. Compute Dry Operating Weight Index using the formula indicated in (2) and report in (3).
c. Dry Operating Index = 53.4.
d. Enter weight deviation or adjustment in (4) and read corresponding index variation in (5) : + 1.43.
e. Calculate corrected index and report in (6) : 54.83.
f. Enter master data in table (7) and determine Zero Fuel Weight : 60 280 kg and Takeoff Weight :
73 280 kg.
g. Enter cargo weight and passenger number per compartment in (8).
h. Enter index scale (9) with corrected index and proceed through cargo and passenger scales (10).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
LOADING
WEIGHT AND BALANCE - LOAD AND TRIM SHEET
A318/A319/A320/A321 FLEET PER-LOD-WBA-LTS P 4/10
FCOM 19 AUG 10
i. From the final point draw a vertical line which intersects (12) the zero fuel weight horizontal line
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 6(109)