ATR 42 Model : 400
WEIGHT AND LOADING
LIMITATIONS
P 1
NOV 98
400
2.01
.
02
DESIGN WEIGHT LIMITATIONS
MAXIMUM WEIGHT
KG
LB
RAMP
18070
39837
TAKE-OFF
17900
39462
LANDING
17600
38801
ZERO FUEL
16300
35935
CENTER OF GRAVITY ENVELOPE
The limits of the center of gravity are given in percentage of the mean aerodynamic
chord (MAC), landing gear extended.
The MAC is 2.285 meters long (89.961 in).
Station 0 is located 2.362 meters (92.992 in) forward of the fuselage nose.
The distance from station 0 to reference chord leading edge is 11.425 meters (449.803 in).
CARGO COMPARTMENT LOADING LIMITATIONS
See W.B.M. : 1.10.04 p 1
AA
R
R
R
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01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only
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