AIRPLANE
FLIGHT
MANUAL
LIMITATIONS
EMBRAER 190 ECJ
ANAC APPROVED 2-06
REVISION 11 code 12 Page 1
AFM-1912
CENTER OF GRAVITY ENVELOPE
(ALTERNATE 1 – CENTER OF GRAVITY – 17%)
EMBRAER 195 STANDARD, LR AND AR MODELS
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.
CG POSITION − % MAC
24000
−5
WEIGHT − kg
5152535
26000
28000
30000
32000
34000
36000
38000
40000
42000
44000
46000
48000
50000
52000
54000
56000
58000
27%
31%
0 10203040
29500 kg
32.5%
7%
31800 kg
31195 kg
30100 kg
52290 kg
9.3%
11.3%
51230 kg
50415 kg
22%
18.4%
28.5%
30600 kg
43400 kg
38000 kg
INFLIGHT LIMITS (FLAPS AND GEAR UP)
1REGION
LANDING LIMITS
17%
10%
29726 kg
TAKEOFF LIMITS − CG ALTERNATE 1
1
EM170AOM020096B.DGN
NOTE: The CAFM CG Envelope option must be set to alternate 1 for
takeoff.
To Next Page
Loading...
