Embraer EMB145 Operation Manual page 761

QUICK TURN AROUND WEIGHT TABLE
ALL ENGINE TYPES - FAA - FLAPS 45
LR BRAKES
Temp.
o
( C)
-2% -1%
-20 36902 37399 37856 38416 38896 40480 41016 41515 42124 42622
-15 36547 37040 37493 38048 38527 40066 40598 41091 41695 42191
-10 36201 36691 37139 37690 38166 39663 40190 40679 41278 41771
-5 35864 36351 36795 37341 37816 39271 39794 40278 40871 41363
0 35537 36020 36461 37002 37476 38890 39409 39888 40476 40966
2 35409 35891 36330 36870 37342 38741 39258 39736 40322 40811
4 35282 35763 36200 36739 37210 38593 39109 39585 40169 40657
8 35033 35511 35945 36480 36951 38302 38815 39288 39867 40354
12 34789 35264 35696 36227 36696 38018 38527 38997 39573 40058
16 34551 35023 35453 35981 36449 37740 38247 38713 39285 39770
20 34316 34786 35213 35738 36205 37467 37971 38434 39002 39485
24 34088 34556 34980 35501 35967 37201 37702 38162 38727 39208
28 33864 34329 34750 35269 35734 36940 37438 37895 38456 38936
Temp.
o
( C)
-2% -1%
-20 41827 42378 42892 43520 44024 43130 43694 44223 44869 45380
-15 41393 41939 42448 43070 43573 42673 43232 43756 44396 44905
-10 40971 41512 42016 42633 43133 42229 42783 43302 43936 44442
-5 40560 41096 41596 42206 42705 41796 42346 42860 43487 43992
0 40160 40693 41187 41793 42289 41376 41921 42430 43052 43554
2 40004 40535 41027 41631 42126 41211 41755 42262 42882 43383
4 39849 40378 40869 41470 41965 41048 41590 42095 42713 43213
8 39544 40070 40558 41154 41648 40728 41266 41768 42381 42880
12 39246 39769 40253 40845 41337 40414 40949 41447 42056 42553
16 38956 39475 39956 40544 41035 40108 40640 41134 41739 42235
20 38669 39186 39663 40248 40736 39807 40336 40826 41427 41921
24 38390 38904 39378 39959 40446 39514 40040 40527 41123 41616
28 38117 38627 39098 39675 40161 39226 39748 40232 40824 41316
NOTE: Quick Turn Around Weight in lb.
REVISION 41
AIRPLANE
OPERATIONS
MANUAL
-10 Kt
SLOPE
0 1% 2%
10 Kt
SLOPE
0 1% 2%
Copyright © by Embraer. Refer to cover page for details.
o
- 10000 FT
WIND
-2% -1%
WIND
-2% -1%
1-04-30
PERFORMANCE
EMB-145/135 FAA
0 Kt
0 1% 2%
20 Kt
0 1% 2%
Page Code
61 02