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Performance Inflight -
Advisory Information
737-300/CFM56-3_20K
Copyright © The Boeing Company. See title page for details.
PI.12.8
ADVISORY INFORMATION
Advisory Information Recommended Brake Cooling Schedule
Reference Brake Energy Per Brake (Millions of Foot Pounds)
WIND CORRECTED BRAKES ON SPEED (KIAS)*
60 80 100 120 140
WEIGHT
(1000 KG)
OAT
(°C)
PRESS ALT PRESS ALT PRESS ALT PRESS ALT PRESS ALT
0 2 4 0 2 4 0 2 4 0 2 4 0 2 4
65
-20 7.0 7.5 8.1 11.3 12.2 13.1 16.2 17.7 19.1 21.9 24.1 25.9
0 7.5 8.2 8.9 12.3 13.2 14.3 17.7 19.3 20.8 23.9 26.0 27.9
15 8.0 8.7 9.4 13.1 14.0 15.1 18.8 20.4 22.0 25.4 27.7 29.5
20 8.1 8.8 9.6 13.3 14.3 15.4 19.2 20.8 22.4 25.9 28.3 30.0
40 8.7 9.5 10.2 14.3 15.3 16.6 20.7 22.4 24.1 27.9 30.0 32.1
60
-20 6.6 7.2 7.7 10.6 11.5 12.4 15.3 16.6 18.0 20.5 22.2 24.0 26.5
0 7.1 7.8 8.4 11.5 12.5 13.5 16.7 18.1 19.6 22.4 24.3 26.1 28.9
15 7.6 8.3 8.9 12.3 13.3 14.3 17.8 19.3 20.8 23.8 25.8 27.8 30.7
20 7.7 8.4 9.1 12.5 13.5 14.5 18.1 19.7 21.2 24.3 26.3 28.3 31.3
40 8.2 9.1 9.7 13.4 14.5 15.6 19.5 21.2 22.8 26.2 28.3 30.4 28.9
55
-20 6.1 6.6 7.1 9.8 10.6 11.5 14.1 15.3 16.5 19.1 20.5 22.1 24.5 26.4
0 6.6 7.2 7.7 10.7 11.6 12.5 15.4 16.7 18.0 20.7 22.4 24.1 26.7 28.8
15 7.1 7.6 8.2 11.4 12.3 13.3 16.3 17.8 19.1 22.0 23.8 25.6 28.4 30.6
20 7.2 7.7 8.3 11.6 12.5 13.5 16.6 18.1 19.5 22.4 24.3 26.1 28.9 31.2
40 7.7 8.3 8.9 12.5 13.5 14.5 17.9 19.5 21.0 24.1 26.2 28.2 31.1 33.6
50
-20 5.7 6.2 6.7 9.1 9.8 10.6 13.2 14.3 15.3 17.6 19.0 20.4 22.6 24.5 26.4
0 6.2 6.7 7.3 9.9 10.7 11.6 14.4 15.6 16.7 19.2 20.7 22.2 24.7 26.7 28.8
15 6.6 7.2 7.8 10.4 11.4 12.3 15.2 16.5 17.8 20.3 22.0 23.6 26.2 28.4 30.6
20 6.7 7.3 7.9 10.6 11.6 12.5 15.5 16.8 18.2 20.7 22.4 24.1 26.7 28.9 31.2
40 7.2 7.8 8.4 11.5 12.5 13.5 16.7 18.1 19.6 22.3 24.1 26.0 28.8 31.1 33.5
45
-20 5.5 6.0 6.3 8.5 9.2 9.9 12.2 13.1 14.1 16.0 17.4 18.8 20.5 22.2 24.0
0 5.9 6.4 6.9 9.3 10.0 10.8 13.2 14.3 15.3 17.4 18.9 20.4 22.4 24.3 26.2
15 6.3 6.8 7.3 9.9 10.7 11.5 14.0 15.1 16.3 18.5 20.1 21.7 23.8 25.8 27.8
20 6.4 6.9 7.4 10.1 10.9 11.7 14.3 15.4 16.6 18.9 20.5 22.1 24.3 26.3 28.3
40 6.8 7.4 7.9 10.8 11.7 12.6 15.3 16.5 17.8 20.4 22.0 23.8 26.2 28.3 30.5
40
-20 5.1 5.5 5.9 7.9 8.5 9.1 11.0 12.0 12.9 14.6 15.8 17.2 18.8 20.2 21.7
0 5.5 5.9 6.4 8.6 9.3 10.0 12.0 13.0 14.0 15.9 17.3 18.7 20.5 22.1 23.8
15 5.8 6.3 6.8 9.1 9.8 10.6 12.8 13.8 14.9 17.0 18.4 19.8 21.7 23.5 25.3
20 5.9 6.4 6.9 9.2 10.0 10.8 13.0 14.1 15.2 17.3 18.8 20.2 22.1 24.0 25.8
40 6.3 6.8 7.4 9.9 10.8 11.6 14.0 15.1 16.3 18.6 20.2 21.7 23.8 25.8 27.8
* To correct for wind, enter table with the brakes on speed minus one half the headwind or plus 1.5 times
the tailwind.
If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C.
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.12.9
ADVISORY INFORMATION
Advisory Information Recommended Brake Cooling Schedule
Adjusted Brake Energy Per Brake (Millions of Foot Pounds)
No Reverse Thrust
Two Engine Detent Reverse Thrust
Cooling Time (Minutes) - Category A Brakes
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
EVENT 5 10 15 20 25 30 35
RTO MAX MAN 5 10 15 20 25 30 35
LANDING
MAX MAN 3.4 7.4 11.9 16.5 21.1 25.8 30.5
MAX AUTO 3.2 7.0 11.4 15.5 19.7 24.2 28.5
AUTOBRAKE 3 3.1 6.7 10.8 14.6 18.2 22.2 25.9
AUTOBRAKE 2 2.9 6.3 10.3 13.8 17.0 20.1 23.2
AUTOBRAKE 1 2.9 6.2 10.0 13.4 16.5 19.7 22.6
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
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
　
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