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(30.0% MAC) at 2570 lb., to FS 148.1 (31.5% MAC) at 2900 lb., and to FS 148.0 (31.3% MAC) at
3000 lb.
Center of Gravity Limits
March 2010
Information Manual 6-15
Cirrus Design Section 6
SR20 Weight & Balance
Weight & Balance Loading Form
Serial Num: ________________ Date: ________________________
Reg. Num: _________________ Initials: ______________________
• Note •
The Takeoff Condition Weight must not exceed 3000 lb. All weights above 2900 lb
must consist of fuel.
The Takeoff Condition Moment must be within the Minimum Moment to Maximum
Moment range at the Takeoff Condition Weight. (Refer to Figure 6-9, Moment
Limits).
Item Description
Weight
LB
Moment/
1000
1.
Basic Empty Weight
Includes unusable fuel & full oil
2.
Front Seat Occupants
Pilot & Passenger (total)
3. Rear Seat Occupants
4.
Baggage Area
130 lb maximum
5.
Zero Fuel Condition Weight
Sub total item 1 thru 4
6.
Fuel Loading
56 Gallon @ 6.0 lb/gal. Maximum
7.
Ramp Condition Weight
Sub total item 5 and 6
8.
Fuel for start, taxi, and runup
Normally 6 lb at average moment of 922.8
– –
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-7
Weight and Balance Loading Form
March 2010
6-16 Information Manual
Section 6 Cirrus Design
Weight & Balance SR20
Figure 6-8
Loading Data
Use the following chart or table to determine the moment/1000 for fuel
and payload items to complete the Loading Form (Figure 6-7).
*130 lb Maximum
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Baggage
FS 208.0
Fuel
FS 153.8
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Fuel
FS 153.8
20 2.87 3.60 4.16 3.08 220 31.57 39.60 33.83
40 5.74 7.20 8.32 6.15 240 34.44 43.20 36.90
60 8.61 10.80 12.48 9.23 260 37.31 46.80 39.98
80 11.48 14.40 16.64 12.30 280 40.18 50.40 43.05
100 14.35 18.00 20.80 15.38 300 43.05 54.00 46.13
120 17.22 21.60 24.96 18.45 320 45.92 57.60 49.20
140 20.09 25.20 (27.04)* 21.53 340 48.79 61.20 52.28
160 22.96 28.80 24.60 360 51.66 64.80 55.35
180 25.83 32.40 27.68 380 54.53 68.40
200 28.70 36.00 30.75 400 57.40 72.00
SR20_FM06_1942
50
0
100
200
300
400
500
Moment/1000
Weight - Pounds
10
Fwd Pass
Fuel
Aft Pass
Baggage
Loading Chart
0 20 30 40 60 70 80 90
Loading Data
March 2010
Information Manual 6-17
Cirrus Design Section 6
SR20 Weight & Balance
Moment Limits
Use the following chart or table to determine if the weight and moment
from the completed Weight and Balance Loading Form (Figure 6-7)
are within limits.
Weight
LB
Moment/1000 Weight
LB
Moment/1000
Minimum Maximum Minimum Maximum
2110 293 305 2600 366 383
2150 299 311 2650 374 391
2200 306 320 2700 381 399
2250 314 328 2750 390 406
2300 321 336 2800 398 414
2350 329 344 2850 407 422
2400 336 352 2900 415 429
2450 344 360 2950 424 437
2500 351 368 3000 432 444
2550 359 376
SR20_FM06_1943A
280 300 320
3000
Moment/1000
Weight - Pounds
420 440
2800
2600
2400
2200
2000
340 360 380 400
Figure 6-9
Moment Limits
March 2010
6-18 Information Manual
Section 6 Cirrus Design
Weight & Balance SR20
Equipment List
This list will be determined after the final equipment has been installed
in the aircraft.
March 2010
Information Manual 7-1
Cirrus Design Section 7
SR20 Airplane Description
Section 7
Airplane and Systems Description
Table of Contents
Introduction .....................................................................................7-5
Airframe ..........................................................................................7-6
Fuselage ......................................................................................7-6
Wings...........................................................................................7-6
Empennage .................................................................................7-7
Flight Controls .................................................................................7-8
Elevator System...........................................................................7-8
Aileron System...........................................................................7-10
　
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