Embraer EMB145 Operation Manual page 728

PERFORMANCE
EMB-145/135 FAA
QUICK TURN AROUND WEIGHT TABLE
ALL ENGINE TYPES - FAA - FLAPS 22
ER BRAKES
Temp.
O
( C)
-2% -1%
-20 28077 28463 28929 29394 29785 31120 31567 32066 32575 33012
-15 27809 28191 28654 29114 29502 30803 31244 31740 32244 32676
-10 27547 27924 28384 28840 29225 30493 30928 31420 31920 32347
-5 27295 27666 28123 28576 28957 30194 30622 31112 31607 32029
0 27049 27415 27870 28319 28696 29903 30325 30812 31303 31721
4 26857 27220 27673 28119 28493 29676 30094 30578 31066 31481
8 26669 27028 27479 27922 28294 29454 29867 30349 30833 31245
12 26484 26840 27289 27729 28098 29236 29645 30124 30605 31014
16 26302 26653 27101 27538 27904 29020 29425 29901 30379 30785
20 26121 26469 26915 27349 27713 28806 29207 29681 30156 30558
24 25945 26290 26734 27166 27527 28598 28995 29467 29939 30338
28 25774 26115 26557 26986 27345 28395 28788 29258 29727 30123
32 - -
Temp.
O
( C)
-2% -1%
-20 32190 32660 33170 33694 34147 33284 33775 34296 34837 35306
-15 31855 32318 32825 33344 33792 32928 33412 33930 34466 34930
-10 31527 31983 32486 33001 33444 32580 33057 33571 34101 34560
-5 31211 31660 32160 32670 33108 32244 32714 33225 33750 34204
0 30903 31346 31843 32348 32782 31917 32381 32889 33409 33858
4 30663 31101 31595 32097 32527 31663 32121 32626 33143 33588
8 30427 30860 31352 31851 32277 31413 31866 32369 32881 33323
12 30196 30625 31114 31609 32032 31168 31616 32116 32625 33063
16 29968 30391 30878 31370 31789 30926 31369 31866 32372 32806
20 29741 30160 30645 31134 31549 30685 31124 31619 32121 32551
24 29521 29936 30418 30904 31317 30453 30886 31378 31877 32304
28 29306 29717 30197 30679 31089 30224 30653 31143 31639 32062
32 29096 29502 29980 30459 30865 30001 30425 30913 31405 31825
NOTE: Quick Turn Around Weight in lb.
Page
28
1-04-30
AIRPLANE
OPERATIONS
MANUAL
-10 kt
0 1% 2%
- -
10 kt
0 1% 2%
Code
02
Copyright © by Embraer. Refer to cover page for details.
o
- 8000 FT
WIND
SLOPE
-2% -1%
- 28196 28585 29053 29519 29912
WIND
SLOPE
-2% -1%
0 kt
0 1% 2%
20 kt
0 1% 2%
REVISION 41