曝光台 注意防骗
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occurs after takeoff, extend gear soon for at least 7 minutes.
When in fuse plug melt zone, clear runway immediately. Unless required, do not set parking brake. Do not
approach gear or attempt to taxi for one hour. Tire, wheel and brake replacement may be required. If overheat
occurs after takeoff, extend gear soon for at least 12 minutes.
Brake Temperature Indicator (if installed) on First Officer’s Instrument Panel may be used 10 to 15 minutes
after brake application, to determine recommended cooling time.
June 4, 2004
737 Flight Crew Operations Manual
Performance Inflight -
Advisory Information
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.12.10
Intentionally
Blank
June 4, 2004
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
Engine Inoperative Section 13
737-300/CFM56-3_20K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
PI.13.1
PI.13 Performance Inflight --Engine Inoperative ENGINE INOP
Engine Inoperative Initial Max Continuous %N1
Based on .74M, engine bleed for packs auto and anti-ice off
%N1 Adjustment for Engine Bleeds
TAT
(°C)
PRESSURE ALTITUDE (1000 FT)
27 29 31 33 35 37
20 92.9 92.9 92.8 92.8 92.8 92.7
15 93.3 93.3 93.2 93.2 93.2 93.1
10 93.7 93.7 93.6 93.6 93.6 93.5
5 94.0 94.0 93.9 93.9 93.9 93.8
0 94.3 94.3 94.2 94.2 94.2 94.1
-5 93.7 94.6 94.5 94.5 94.5 94.4
-10 92.8 93.9 94.7 94.7 94.7 94.6
-15 91.9 93.0 93.9 95.0 95.0 94.9
-20 91.0 92.0 93.0 94.1 95.3 95.4
-25 90.1 91.1 92.0 93.2 94.4 94.9
-30 89.2 90.2 91.1 92.2 93.4 94.0
-40 87.4 88.3 89.2 90.3 91.5 92.0
-50 85.5 86.4 87.3 88.3 89.5 90.0
BLEED
CONFIGURATION
PRESSURE ALTITUDE (1000 FT)
27 29 31 33 35 37
ENGINE A/I ON -1.0 -1.0 -1.0 -1.0 -1.0 -1.0
ENGINE AND WING A/I ON -3.1 -3.0 -3.0 -3.0 -3.0 -3.0
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.13.2
ENGINE INOP
Engine Inoperative Max Continuous %N1
33000 FT to 23000 FT Pressure Altitudes
Based on engine bleed for packs auto and anti-ice off
Anti-Ice Adjustments
33000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .58 89.6 91.6 93.5 94.4 94.0 93.5 93.2
220 .63 89.4 91.4 93.3 94.8 94.3 93.8 93.5 93.1
240 .68 89.1 91.0 93.0 94.8 94.6 94.0 93.7 93.4
260 .74 88.3 90.2 92.2 94.0 94.7 94.2 93.9 93.5 93.2
31000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .55 88.8 90.8 92.7 94.2 93.9 93.4 93.1
220 .61 88.7 90.6 92.4 94.4 94.2 93.7 93.4 93.1
240 .66 88.3 90.2 92.1 94.0 94.5 93.9 93.6 93.3 92.9
260 .71 87.8 89.7 91.7 93.5 94.6 94.1 93.8 93.5 93.1
29000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .53 88.1 90.0 91.9 93.8 93.7 93.2 92.9 92.6
220 .58 87.9 89.8 91.8 93.6 94.1 93.6 93.3 92.9 92.6
240 .63 87.6 89.5 91.4 93.3 94.4 93.8 93.5 93.2 92.8
260 .68 87.1 89.1 91.0 92.8 94.5 94.0 93.7 93.4 93.0 92.6
27000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .51 87.3 89.3 91.2 93.0 93.5 93.0 92.8 92.4
220 .56 87.1 89.1 91.0 92.8 93.9 93.4 93.1 92.8 92.4
240 .60 86.9 88.9 90.7 92.6 94.3 93.8 93.5 93.1 92.7 92.3
260 .65 86.5 88.4 90.3 92.1 93.9 93.9 93.7 93.3 92.9 92.5
25000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .49 86.6 88.5 90.4 92.2 93.4 93.0 92.7 92.4 92.0
220 .53 86.4 88.3 90.2 92.0 93.7 93.3 93.0 92.7 92.3 91.9
240 .58 86.2 88.1 90.0 91.8 93.6 93.6 93.3 93.0 92.6 92.2
260 .63 85.8 87.7 89.6 91.4 93.2 93.8 93.6 93.2 92.9 92.4 92.0
23000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .47 85.8 87.7 89.6 91.4 93.2 92.8 92.6 92.3 91.9 91.6
220 .51 85.6 87.5 89.4 91.2 93.0 93.1 92.9 92.5 92.2 91.8
240 .56 85.4 87.3 89.2 91.0 92.8 93.4 93.2 92.8 92.5 92.1 91.7
260 .60 85.2 87.1 88.9 90.8 92.5 93.8 93.5 93.1 92.8 92.4 92.0
BLEED
CONFIGURATION
PRESS ALT (1000 FT)
23 25 27 29 31 33
ENGINE ANTI-ICE ON -1.0 -1.0 -1.0 -1.0 -1.0 -1.0
ENGINE AND WING ANTI-ICE ON -3.1 -3.1 -3.1 -3.0 -3.0 -3.0
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.13.3
ENGINE INOP
Engine Inoperative Max Continuous %N1
21000 FT to 14000 FT Pressure Altitudes
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