AIRPLANE
FLIGHT
MANUAL
LIMITATIONS
ANAC APPROVED 2-06
REVISION 13 code 05 Page 3
AFM-1385
EMBRAER 170 STANDARD, LR, SE AND SU MODELS POST-MOD
SB 170-00-0016 OR EQUIPPED WITH AN EQUIVALENT
MODIFICATION FACTORY INCORPORATED
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%
TAKEOFF LIMITS − CG ALTERNATE 1
1
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%
TAKEOFF LIMITS − CG ALTERNATE 1
1
EM170AOM020149A.DGN
NOTE: The CAFM CG Envelope option must be set to Alternate 1 for
takeoff.
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