曝光台 注意防骗
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EVENT 5 10 15 20 25 30 35
LANDING
MAX AUTO 2.6 5.6 8.9 12.4 16.0 19.4 22.8
AUTOBRAKE 3 1.9 3.9 6.4 8.4 10.5 12.6 14.7
AUTOBRAKE 1 & 2 1.9 3.7 5.8 7.8 9.6 11.3 12.8
ADJUSTED BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
8 & BELOW 10 12 14 16 18 18.5 TO 23.7 23.8 & ABOVE
BRAKE TEMPERATURE INDICATOR READING
UP TO 2.1 2.8 3.2 3.6 4.2 4.8 4.9 TO 6.3 6.3 & ABOVE
INFLIGHT
GEAR DOWN
NO SPECIAL
PROCEDURE
REQUIRED
2 3 4 5 6 CAUTION FUSE PLUG
GROUND 19 32 43 53 61 MELT ZONE
Observe maximum quick turnaround limit.
Table shows energy per brake added by a single stop with all brakes operating. Energy is assumed to be
equally distributed among the operating brakes. Total energy is the sum of residual energy plus energy
added.
Add 1.0 million foot pounds for each taxi mile.
When in caution zone, wheel fuse plugs may melt. Delay takeoff and inspect after One hour. If overheat
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_22K
Copyright © The Boeing Company. See title page for details.
PI.22.10
Intentionally
Blank
June 4, 2004
737 Flight Crew Operations Manual
Performance Inflight - Chapter PI
Engine Inoperative Section 23
737-300/CFM56-3_22K
FAST-Doc PI/PD Template 9/1/99
Copyright © The Boeing Company. See title page for details.
PI.23.1
PI.23 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 95.2 95.2 95.2 95.2 95.1 95.1
15 95.8 95.8 95.8 958 95.7 95.7
10 96.1 96.1 96.1 96.1 96.0 96.0
5 96.6 96.6 96.6 96.6 96.5 96.5
0 97.1 97.1 97.1 97.1 97.0 97.0
-5 96.6 97.7 97.7 97.7 97.6 97.6
-10 95.7 96.9 98.1 98.7 98.0 98.0
-15 94.8 96.0 97.1 98.4 98.3 98.3
-20 93.9 95.1 96.2 97.4 98.4 98.7
-25 92.9 94.1 95.3 96.5 97.5 98.0
-30 92.0 93.2 94.3 95.5 96.5 97.0
-40 90.1 91.3 98.3 93.5 94.5 95.0
-50 88.1 89.3 90.3 91.5 92.4 93.0
BLEED
CONFIGURATION
PRESSURE ALTITUDE (1000 FT)
25 27 29 31 33 35 37
ENGINE A/I ON -0.9 -0.9 -0.9 -0.9 -0.9 -0.9 -1.0
ENGINE AND WING A/I ON -2.9 -2.9 -2.9 -2.8 -2.8 -2.8 -2.9
December 1, 2000
737 Flight Crew Operations Manual
Performance Inflight -
Engine Inoperative
737-300/CFM56-3_22K
Copyright © The Boeing Company. See title page for details.
PI.23.2
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 92.3 94.4 96.4 97.1 96.5 96.0 95.7
220 .63 92.2 94.3 96.3 97.8 97.1 96.4 96.1 95.7 95.3
240 .68 92.1 94.2 96.2 98.1 97.8 96.9 96.4 96.0
260 .74 91.4 93.5 95.5 97.4 98.0 97.0 96.6 96.1 95.6
31000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .55 91.5 93.5 95.5 97.0 96.4 95.8 95.5
220 .61 91.3 93.3 95.3 97.2 96.8 96.2 95.9 95.6 95.3
240 .66 91.1 93.1 95.1 97.1 97.4 96.7 96.3 95.9 95.5
260 .71 90.9 92.9 94.9 96.8 98.0 97.0 96.5 96.1 95.6
29000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .53 90.6 92.6 94.6 96.5 96.2 95.6 95.4 95.1
220 .58 90.4 92.4 94.4 96.3 96.6 96.1 95.8 95.5 95.1
240 .63 90.2 92.2 94.1 96.1 97.1 96.5 96.1 95.8 95.4
260 .68 90.0 92.0 93.9 95.9 97.7 96.9 96.4 96.0 95.6 95.1
27000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .51 89.8 91.8 93.8 95.7 96.0 95.5 95.2 94.9
220 .56 89.6 91.6 93.5 95.4 96.4 95.9 95.6 95.3 95.0 94.6
240 .60 89.3 91.3 93.2 95.1 96.9 96.3 96.0 97.7 95.3 95.0
260 .65 89.1 91.0 93.0 94.9 96.7 96.7 96.3 95.9 95.5 95.1
25000 FT PRESS ALT. TAT (°C)
KIAS M -50 -40 -30 -20 -10 0 5 10 15 20 25
200 .49 89.0 91.0 92.9 94.8 95.9 95.4 95.1 94.8 94.5
220 .53 88.8 90.7 92.7 94.6 96.3 95.7 95.4 95.1 94.8 94.5
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