曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
12.5 % MAC
FS 139.1
2700 lb
17.4 % MAC
FS 141.4
3210 lb
22.4 % MAC
FS 143.8
3400 lb
Center of Gravity Limits
June 2007
Information Manual 6-15
Cirrus Design Section 6
SR22 Weight & Balance
Weight & Balance Loading Form
Serial Num: ________________ Date: ________________________
Reg. Num: _________________ Initials: ______________________
• 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 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
81 Gallon @ 6.0 lb/gal. Maximum
7.
Ramp Condition Weight
Sub total item 5 and 6
8.
Fuel for start, taxi, and runup
Normally 9 lb at average moment of 1394.
– –
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-7
Weight and Balance Loading Form
June 2007
6-16 Information Manual
Section 6 Cirrus Design
Weight & Balance SR22
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 **81 U.S. Gallons Usable
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 2.87 3.60 4.16 3.10 260 37.31 46.80 40.27
40 5.74 7.20 8.32 6.20 280 40.18 50.40 43.37
60 8.61 10.80 12.48 9.29 300 43.05 54.00 46.47
80 11.48 14.40 16.64 12.39 320 45.92 57.60 49.57
100 14.35 18.00 20.80 15.49 340 48.79 61.20 52.67
120 17.22 21.60 24.96 18.59 360 51.66 64.80 55.76
140 20.09 25.20 (27.04)* 21.69 380 54.53 68.40 58.86
160 22.96 28.80 24.78 400 57.40 72.00 61.96
180 25.83 32.40 27.88 420 60.27 75.60 65.06
200 28.70 36.00 30.98 440 63.14 79.20 68.16
220 31.57 39.60 34.08 460 71.25
240 34.44 43.20 37.18 486** 75.28
0.00 20.0 40.0 60.0 80.0
SR22_FM06_1946
0
100
200
300
400
500
Moment/1000
Weight - Pounds
Loading Chart Fwd Pass
Fuel
Aft Pass
Baggage
100
Loading Data
June 2007
Information Manual 6-17
Cirrus Design Section 6
SR22 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
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 461 481
2650 369 392 3300 471 489
2700 375 400 3350 480 496
2750 383 407 3400 489 504
2800 390 415
3200
3400
SR22_FM06_1947
300 350
3000
Moment/1000
Weight - Pounds
450 500
2800
2600
2400
2200
2000
400
Figure 6-9
Moment Limits
June 2007
6-18 Information Manual
Section 6 Cirrus Design
Weight & Balance SR22
Equipment List
This list will be determined after the final equipment has been installed
in the aircraft.
June 2007
Information Manual 7-1
Cirrus Design Section 7
SR22 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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(50)
