S 865-043
(4)
Stop for five minutes again.
S 975-044
(5)
Collect the first set of samples:
(a)
Read the weight on each wheel from the scales and write the data in Figure 507, in the WHEEL WEIGHT, SAMPLE 1 column.
(b)
Read the counts for each load sensor with WBC mode 22 and write the data in Figure 508, in the SENSOR COUNTS, SAMPLE 1 column.
S 865-145
(6)
Stop for a minimum of one minute.
S 975-103
(7)
Collect the second set of samples:
(a) Read the weight on each wheel from the scales and write the data in Figure 507, in the WHEEL WEIGHT, SAMPLE 2 column.
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AXLE WHEEL TION LOCA- WHEEL NO. WHEEL WEIGHT (lbs.) (AXLE WEIGHT) Y (ADD AVERAGES FOR AXLE) VALUE) (WEIGHT-ING V
SAMPLE 1 SAMPLE 2 SAMPLE 3 AVERAGE
FWD L WING OUTBD 1 4
INBD 2
AFT L WING OUTBD 3 4
INBD 4
L BODY FWD OUTBD 5 8
INBD 6
L BODY AFT OUTBD 7 8
INBD 8
R BODY FWD INBD 9 8
OUTBD 10
R BODY AFT INBD 11 8
OUTBD 12
R WING FWD INBD 13 4
OUTBD 14
R WING AFT INBD 15 4
OUTBD 16
MAIN LANDING GEAR
LOCATION WHEEL WHEEL NO. WHEEL WEIGHT (lbs.) ING (WEIGHT-VALUE) V
SAMPLE 1 SAMPLE 2 SAMPLE 3 Y (AVERAGE)
LEFT 17 1
RIGHT 18 1
NOSE LANDING GEAR
Wheel Weights at Normal Strut Pressures - Second Time
Figure 507
C26875
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AXLE TION LOCA-SENSOR NO. SENSOR SENSOR COUNTS COUNTS (SUM OF AVERAGES FOR AXLE) AXLE X (DELTA COUNTS) ZERO) (AXLE COUNTS -AXLE IDEAL
SAMPLE 1 SAMPLE 2 SAMPLE 3 AVERAGE
FWD L WING OUTBD 1
INBD 2
AFT L WING OUTBD 3
INBD 4
L BODY FWD OUTBD 5
INBD 6
L BODY AFT OUTBD 7
INBD 8
R BODY FWD INBD 9
OUTBD 10
R BODY AFT INBD 11
OUTBD 12
R WING FWD INBD 13
OUTBD 14
R WING AFT INBD 15
OUTBD 16
MAIN LANDING GEAR
SENSOR SENSOR SENSOR COUNTS (AVERAGE -(DELTA COUNTS) IDEAL ZERO) X
LOCATION NO. SAMPLE 1 SAMPLE 2 SAMPLE 3 AVERAGE
LEFT FWD 17F
LEFT AFT 17R
RIGHT FWD 18F
RIGHT AFT 18R
NOSE LANDING GEAR
Sensor Counts at Normal Strut Pressures - Second Time
Figure 508
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(b) Read the counts for each load sensor with WBC mode-22 and write the data in Figure 508, in the SENSOR COUNTS, SAMPLE 2 column. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 指示/记录系统 1(93)
