Embraer 170 - Page 72

LIMITATIONS
AIRPLANE
FLIGHT
MANUAL
2-06 ANAC APPROVED
Page 2 code 05 REVISION 13
AFM-1385
EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD
SB 170-00-0003 OR EQUIPPED WITH AN EQUIVALENT
MODIFICATION FACTORY INCORPORATED AND PRE-MOD SB
170-00-0016
NOTE: The data below must be used in conjunction with the maximum
weight values (ramp, takeoff, landing and zero fuel) associated
to each model and found in the Maximum Weight table.
90000
85000
80000
75000
70000
65000
60000
55000
50000
45000
40000
0−10 −5 5 10 15 20 25 30 35 40 45
27%
82011 lb
65256 lb
50706 lb
48060 lb
4%
50706 lb
75728 lb
18.8%
WEIGHT − lb
CG POSITION − % MAC
4%
7%
14.2%11.2% 25.5%
85097 lb
INFLIGHT LIMITS (FLAPS AND GEAR UP)
1REGION
LANDING LIMITS
16%
8%
73413 lb
72310 lb
TAKEOFF LIMITS − CG ALTERNATE 1
1
MLW
EM170AOM020146B.DGN
NOTE: The CAFM CG Envelope option must be set to Alternate 1 for
takeoff.