Airplane Flight Manual
Page 11
FAA Approved
Revision A3: Apr 26, 2007
Section - 6
WEIGHT & BALANCE
M9411_0.AI
REFERENCE POINT
(RIGHT SIDE)
485.04
-25
-20
-15
-10
-5
5
10
15
20
25
-0
FEET FROM C. G. DATUM
NOTE: REFER TO CONVERSION FACTORS FOR METRIC EQUIVALENT.
C. G. DATUM
353.04
214.75 (F
R.9B
)
190.50
(FR.9)
171.00 (FR.7)
180.25 (FR.8)
204.50 (F
R.9A
)
224.40 (F
R.10)
241.60 (FR.10A)
283.10 (FR.12)
303.85 (F
R.13)
329.85 (FR.14)
352.00 (FR.15)
374.55 (FR.16)
395.30 (FR.1
7)
408.80 (FR.18)
423.53 (F
R.19)
449.40 (F
R.20)
473.27 (FR.21)
509.28 (FR.2
3)
542.77 (F
R.25)
526.02 (F
R.24)
492.55 (FR.2
2)
436.00 (FR.20A)
262.35 (F
R.11)
135.82 (FR.4) CANTED
120.
50 (
F
R.
3)
CA
NT
ED
109.
00 (
F
R.
1)
CA
NT
ED
87.00
151.18
(FR.5) CANTED
161.00
(FR.6) CANTED
FRAME SPACING
IN INCHES
FUSELAGE STATION LOCATING DIAGRAM
Percent Standard Mean Chord
Figure 6.3
For Training Purposes Only