AIRPLANE
FLIGHT
MANUAL
LIMITATIONS
ANAC APPROVED 2-06
REVISION 13 code 11 Page 1
AFM-1385
CENTER OF GRAVITY ENVELOPE
EMBRAER 175 STANDARD, LR AND SU MODELS -
CF34-8E5 ENGINES - POST-MOD SB 170-57-0058 (ENHANCED
WING TIP) OR WITH AN EQUIVALENT FACTORY MODIFICATION
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.
51525
35
CG POSITION − % MAC
010203040
INFLIGHT LIMITS (FLAPS AND GEAR UP)
NOT ALLOWED FOR TAKEOFF
1REGION
TAKEOFF AND LANDING LIMITS
WEIGHT − lb
40000
44000
48000
52000
56000
60000
64000
68000
72000
76000
80000
84000
88000
92000
96000
74957 lb
49604 lb
45
89000 lb
54674 lb
9%
12%
26%
33%
22.4%
EM170AOM020169A.DGN
57650 lb
14.6%
17.6%
27.5%
30.5%
1
27%
69445 lb
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