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130 .56 .58 .59 .61
120 .54 .56 .58 .59 .61
110 .52 .54 .56 .57 .59
100 .50 .52 .54 .56 .57 .59 .61
90 .48 .49 .51 .53 .55 .57 .59 .60 .62
80 .45 .47 .48 .50 .52 .54 .56 .58 .60 .61
B LRC Mach Schedule - One Engine Inop
WEIGHT PRESSURE ALTITUDE - 1000 FT
1000 LB 12 14 16 18 20 22 24 26 28 30
160 .54
150 .52 .54 .57
140 .51 .53 .55 .57 .59
130 .49 .51 .53 .55 .57 .59
120 .47 .49 .51 .53 .55 .57 .59
110 .45 .47 .48 .51 .53 .55 .57 .59 .60
100 .43 .45 .46 .48 .50 .52 .55 .57 .59 .60
Sec. 5 Page 84 737
Rev. 11/15/02 #41 Continental Flight Manual
C LRC Mach Schedule - One Engine Inop
WEIGHT PRESSURE ALTITUDE - 1000 FT
1000 LB 12 14 16 18 20 22 24 26 28 30
180 .57 .59 .60
170 .55 .57 .59 .61
160 .53 .56 .58 .60 .61
150 .52 .54 .56 .59 .60 .62
140 .50 .52 .54 .56 .59 .60 .62
130 .48 .50 .52 .54 .57 .59 .60
120 .47 .48 .50 .52 .54 .57 .59 .61
110 .45 .46 .48 .50 .52 .54 .57 .59 .61
100 .43 .44 .46 .48 .50 .52 .54 .57 .59 .61
D LRC Mach Schedule - One Engine Inop
WEIGHT PRESSURE ALTITUDE - 1000 FT
1000 LB 12 14 16 18 20 22 24 26 28 30
180 .56 .57 .59
170 .55 .56 .58 .59
160 .53 .55 .57 .58 .59
150 .52 .54 .55 .57 .58 .60
140 .51 .52 .54 .55 .57 .59
130 .49 .51 .53 .54 .56 .57 .59
120 .48 .49 .51 .53 .54 .56 .57 .59
110 .46 .48 .49 .51 .52 .54 .56 .57 .59
100 .44 .46 .47 .49 .51 .52 .54 .56 .57 .59
737 Sec. 5 Page 85
Flight Manual Continental Rev. 11/15/02 #41
>>@ Alternate Planning – One Engine Inoperative
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
80,000 to
90,000
90,000 to
100,000
100,000 to
114,000
To
Alternate
Fuel – Lbs.
100 & Less :23 2040 2140 2280 19,000
150 :31 2710 2840 3030 19,000
200 :38 3390 3540 3770 19,000
300 :55 4740 4960 5270 19,000
400 1:11 6100 6380 6780 19,000
500 1:26 7470 7810 8290 19,000
600 1:42 8850 9250 9820 19,000
Conditions: Climb at 280/.74
Cruise at Single Engine LRC
Descent at .74/280
Note: 19000 ft. is used as an example only. Better fuel mileage will be
obtained by flying optimum altitudes.
B Alternate Planning – One Engine Inoperative
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
100,000 to
110,000
110,000 to
120,000
120,000 to
128,000
To
Alternate
Fuel – Lbs.
100 & Less :23 2040 2140 2220 21,000
150 :31 2690 2810 2910 21,000
200 :40 3340 3480 3600 21,000
300 :56 4640 4840 5000 21,000
400 1:13 5950 6200 6390 21,000
500 1:29 7260 7560 7790 21,000
600 1:46 8590 8930 9200 21,000
Conditions: Climb at 280/.78
Cruise at Single Engine LRC
Descent at .78/280
Note: 21000 ft. is used as an example only. Better fuel mileage will be
obtained by flying optimum altitudes.
Sec. 5 Page 86 737
Rev. 11/15/02 #41 Continental Flight Manual
C Alternate Planning – One Engine Inoperative
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
120,000 to
130,000
130,000 to
140,000
140,000 to
144,000
To
Alternate
Fuel – Lbs.
100 & Less :23 2310 2420 2460 19,000
150 :32 3050 3180 3230 19,000
200 :40 3790 3950 4010 19,000
300 :56 5290 5480 5560 19,000
400 1:13 6780 7030 7130 19,000
500 1:28 8290 8580 8690 19,000
600 1:44 9800 10140 10270 19,000
Conditions: Climb at 280/.78
Cruise at Single Engine LRC
Descent at .78/280
Note: 19000 ft. is used as an example only. Better fuel mileage will be
obtained by flying optimum altitudes.
D Alternate Planning – One Engine Inoperative
Distance Time
Landing Weight – Lbs. Cruise
Altitude
To
Alternate
To
Alternate
120,000 to
130,000
130,000 to
140,000
140,000 to
146,300
To
Alternate
Fuel – Lbs.
100 & Less :23 2330 2440 2510 19,000
150 :32 3080 3220 3300 19,000
200 :40 3830 3990 4100 19,000
300 :56 5350 5560 5690 19,000
400 1:11 6870 7130 7280 19,000
500 1:28 8400 8700 8890 19,000
600 1:44 9930 10290 10500 19,000
Conditions: Climb at 280/.78
Cruise at Single Engine LRC
Descent at .78/280
Note: 19000 ft. is used as an example only. Better fuel mileage will be
obtained by flying optimum altitudes.
737 Sec. 5 Page 87
　
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