曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
2. Determine the Takeoff Power Setting from the Max Takeoff % N1 –
EEC Normal Mode Inoperative tables. Be sure to use the correct table
for Engine Bleeds ON or OFF.
Do not use FMC computed Takeoff % N1 values.
3. Assumed Temperature Thrust Reduction not permitted. Use full
Takeoff Thrust.
· Without ACCULOAD:
1. Determine the normal runway limit and climb limit weights from the
Runway Analysis data.
2. Determine the appropriate weight corrections for each from the
Performance Adjustment table.
3. Subtract these weight corrections from the normal runway limit and
climb limit weights.
4. Select the lesser of these two limit weights. This is the maximum
allowable takeoff weight (EEC NORM Mode Inoperative). Actual
weight must be equal to or less than this limit weight. Manual
adjustments for Bleeds ON can be made as discussed in the Bleed
Configuration paragraph earlier in this section.
5. Determine V1, Vr and V2 in the normal manner then apply the
adjustments from the Takeoff V Speed Adjustment table.
6. Determine the Takeoff Power Setting from the Max Takeoff % N1 –
EEC Normal Mode Inoperative tables. Be sure to use the correct table
for Engine Bleeds ON or OFF.
Do not use FMC computed Takeoff % N1 values.
7. Assumed Temperature Thrust Reduction not permitted. Use full
Takeoff Thrust.
Sec. 5 Page 42 737
Rev. 11/15/02 #41 Continental Flight Manual
BCD EEC Normal Mode Inoperative Example (Without
ACCULOAD)
Runway Limit Weight (Normal): .............181,000 lbs.
Climb Limit Weight (Normal): ................183,300 lbs.
Actual Weight:..........................................166,000 lbs.
Engine Bleed: ...........................................Bleeds OFF
Airport Elevation:.....................................Sea Level
Temperature: ............................................30°C
Takeoff Flap Setting: ................................Flaps 5
1. From the Performance Adjustments table (EEC Normal Mode Inoperative):
Runway Limit adjustment:........................11,600 lbs.
Climb Limit adjustment:...........................12,300 lbs.
2. Subtract the corrections:
Runway Limit ...........................................Climb Limit
181,000 lbs...............................................183,300 lbs.
-11,600 lbs............................................... -12,300 lbs.
169,400 lbs...............................................171,000 lbs.
3. The limit weight for this takeoff under these conditions is the Runway Limit
of 169,400 lbs. Since the actual takeoff weight is 166,000 lbs. (below the
limit weight), takeoff is allowed Bleeds OFF.
4. Normal V1, Vr and V2 are 147, 149 and 156 knots respectively.
5. From the Takeoff V Speeds Adjustment table (EEC Normal Mode
Inoperative):
V1 adjustment:..........................................+1 knot
Vr adjustment: ..........................................+1 knot
V2 adjustment:.......................................... 0 knot
6. The corrected V Speeds are 148, 150 and 156 knots respectively.
7. From the Max Takeoff % N1 table (EEC Normal Mode Inoperative):
Takeoff Power Setting (Bleeds OFF): 98.8% N1
737 Sec. 5 Page 43
Flight Manual Continental Rev. 11/15/02 #41
C EEC Normal Mode Inoperative Performance Adjustments
Normal Limit
Weight (LB)
Weight Decrement (LB)
Runway Limit Climb Limit
< 130000 8000 8400
130000-140000 8600 8800
140000-150000 9500 9800
150000-160000 10300 10500
160000-170000 11100 11300
170000-190000 11600 12300
C MAX TAKEOFF % N1 - EEC Normal Mode Inoperative
Engine Bleeds ON
VALID FOR
ENGINE ANTI-ICE
ON OR OFF
OAT
AIRPORT
PRESSURE
ALTITUDE - FEET
oC oF -2000 0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000
54 129 93.3 94.4
50 122 93.8 94.9 95.1 95.2
45 113 94.6 95.6 95.8 95.9 96.1 96.2
40 104 95.2 96.4 96.5 96.6 96.7 96.8 97.0 96.9 96.6
35 95 95.8 97.2 97.3 97.4 97.5 97.6 97.7 97.6 97.3 97.0 96.9
30 86 95.4 98.1 98.1 98.2 98.2 98.3 98.3 98.2 98.1 97.8 97.7 97.7
25 77 94.6 97.3 97.9 98.5 98.6 98.5 98.5 98.5 98.5 98.4 98.4 98.5
20 68 93.8 96.6 97.1 97.7 98.0 98.3 98.6 98.6 98.7 98.6 98.6 98.6
15 59 93.0 95.8 96.4 97.0 97.3 97.6 97.9 98.3 98.7 98.9 98.9 98.9
10 50 92.3 95.0 95.6 96.2 96.5 96.8 97.2 97.5 97.9 98.3 98.8 99.3
5 41 91.5 94.2 94.8 95.4 95.8 96.1 96.4 96.8 97.2 97.6 98.1 98.5
0 32 90.7 93.4 94.1 94.7 95.0 95.3 95.7 96.0 96.4 96.8 97.3 97.8
-10 14 89.0 91.8 92.5 93.1 93.4 93.8 94.1 94.5 94.9 95.3 95.8 96.2
-20 -4 87.4 90.2 90.8 91.5 91.8 92.2 92.6 93.0 93.4 93.7 94.2 94.6
-30 -22 85.7 88.5 89.2 89.8 90.2 90.6 91.0 91.4 91.8 92.1 92.6 93.0
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
737 FLIGHT MANUAL 737飞行手册2(116)