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2. Front Seat Occupants – Enter the total weight and moment/1000
for the front seat occupants from the Loading Data (Figure 6-4).
3. Rear Seat Occupants – Enter the total weight and moment/1000
for the rear seat occupants from the Loading Data (Figure 6-4).
4. Baggage – Enter weight and moment for the baggage from the
Loading Data (Figure 6-4).
• If desired, subtotal the weights and moment/1000 from steps 1
through 4. This is the Zero Fuel Condition. It includes all useful
load items excluding fuel.
5. Fuel Loading – Enter the weight and moment of usable fuel
loaded on the airplane from the Loading Data (Figure 6-4).
• Subtotal the weight and moment/1000. This is the Ramp
Condition or the weight and moment of the aircraft before taxi.
6. Fuel for start, taxi, and run-up – This value is pre-entered on the
form. Normally, fuel used for start, taxi, and run-up is
approximately 9 pounds at an average moment/1000 of 1.394.
7. Takeoff Condition – Subtract the weight and moment/1000 for
step 8 (start, taxi, and run-up) from the Ramp Condition values
(step 7) to determine the Takeoff Condition weight and moment/
1000.
• The total weight at takeoff must not exceed the maximum weight
limit of 3400 pounds. The total moment/1000 must not be above
the maximum or below the minimum moment/1000 for the
Takeoff Condition Weight as determined from the Moment Limits
chart or table (Figure 6-5).
March 2010
Cirrus Design Section 6
SR22 Weight and Balance Data
Information Manual 6-9
Weight and Balance Loading Form
• Note •
The Takeoff Condition Weight must not exceed 3400 lb.
The Takeoff Condition Moment must be within the Minimum
Moment to Maximum Moment range at the Takeoff Condition
Weight. (Refer to Moment Limits).
Serial Num: __________________________ Date: ______________
Reg. Num: ___________________________ Initials:_____________
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
92 Gallon @ 6.0 lb/gal. Maximum
7. Ramp Condition Weight
Sub total item 5 and 6
8. Fuel for start, taxi, and run-up
Normally 9 lb at average moment of 1394.
– –
9. Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-3
March 2010
6-10 Information Manual
Section 6 Cirrus Design
Weight and Balance Data SR22
Loading Data
Use the following chart or table to determine the moment/1000 for fuel
and payload items to complete the Loading Form.
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Baggage
FS 208.0
Fuel
FS 154.9
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Fuel
FS 154.9
20 2.9 3.6 4.2 3.1 300 43.1 54.0 46.5
40 5.7 7.2 8.3 6.2 320 45.9 57.6 49.6
60 8.6 10.8 12.5 9.3 340 48.8 61.2 52.7
80 11.5 14.4 16.6 12.4 360 51.7 64.8 55.8
100 14.4 18.0 20.8 15.5 380 54.5 68.4 58.9
120 17.2 21.6 25.0 18.6 400 57.4 72.0 62.0
140 20.1 25.2 27.04* 21.7 420 60.3 75.6 65.1
160 23.0 28.8 24.8 440 63.1 79.2 68.2
180 25.8 32.4 27.9 460 71.3
200 28.7 36.0 31.0 480 74.4
220 31.6 39.6 34.1 500 77.5
240 34.4 43.2 37.2 520 80.5
260 37.3 46.8 40.3 552** 85.5
280 40.2 50.4 43.4
*130 lb Maximum **92 U.S. Gallons Usable
Figure 6-4
SR22_FM06_2686
Fwd Pass
Fuel
Aft Pass
Baggage
0
100
200
300
400
500
600
0.0 20.0 40.0 60.0 80.0 100.0
Moment/1000
Weight - Pounds
Loading Chart
March 2010
Cirrus Design Section 6
SR22 Weight and Balance Data
Information Manual 6-11
Moment Limits
Use the following chart or table to determine if the weight and moment
from the completed Weight and Balance Loading Form (Figure 6-3)
are within limits.
Weight
LB
Moment/1000 Weight
LB
Moment/1000
Minimum Maximum Minimum Maximum
2200 304 326 2850 398 422
2250 311 333 2900 406 430
2300 318 341 2950 414 437
2350 326 348 3000 421 444
2400 333 355 3050 429 452
2450 340 363 3100 437 459
2500 347 370 3150 444 467
2550 354 378 3200 452 474
2600 362 385 3250 460 481
2650 369 392 3300 467 489
2700 375 400 3350 475 496
2750 383 407 3400 483 504
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(50)
