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
Total 2788 2861 2934 2972
1000 Grnd Roll 1396 1451 1506 1533
Total 2856 2932 3010 3049
2000 Grnd Roll 1448 1505 1562 1590
Total 2928 3008 3090 3131
3000 Grnd Roll 1502 1561 1620 1650
Total 3004 3089 3174 3217
4000 Grnd Roll 1558 1620 1682 1712
Total 3085 3174 3263 3309
5000 Grnd Roll 1618 1682 1745 1777
Total 3170 3263 3358 3406
6000 Grnd Roll 1680 1746 1812 1845
Total 3261 3359 3458 3508
7000 Grnd Roll 1744 1813 1882
Total 3356 3459 3564
8000 Grnd Roll 1812 1884 1955
Total 3458 3566 3675
9000 Grnd Roll 1883 1957 2032
Total 3565 3679 3794
10000 Grnd Roll 1957 2034
Total 3678 3798
Revision 02: 11-17-09
36 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Section 6 - Weight & Balance
Refer to Section 6 - Weight and Balance of the basic POH for current weight
and balance data. Use the following table to determine the Moment/1000 for
anti-ice fluid to complete the Loading Form in the Weight and Balance Section
of the basic POH.
• Total Fluid Reservoir capacity is 8.5 gallon (32L).
• Anti-Ice fluid weight is 9.2 pounds per gallon.
Weight
LB Gallons
Mom/
1000@
Fluid
Reservoir
(FS148.0)
Weight
LB Gallons
Mom/
1000@
Fluid
Reservoir
(FS148.0)
Weight
LB Gallons
Mom/
1000@
Fluid
Reservoir
(FS148.0)
1 0.1 0.148 28 3.0 4.14 55 6.0 8.14
2 0.2 0.296 29 3.2 4.29 56 6.1 8.29
3 0.3 0.444 30 3.3 4.44 57 6.2 8.44
4 0.4 0.592 31 3.4 4.59 58 6.3 8.58
5 0.5 0.740 32 3.5 4.74 59 6.4 8.73
6 0.7 0.888 33 3.6 4.88 60 6.5 8.88
7 0.8 1.036 34 3.7 5.03 61 6.6 9.03
8 0.9 1.184 35 3.8 5.18 62 6.7 9.18
9 1.0 1.332 36 3.9 5.33 63 6.8 9.32
10 1.1 1.480 37 4.0 5.48 64 7.0 9.47
11 1.2 1.628 38 4.1 5.62 65 7.1 9.62
12 1.3 1.776 39 4.2 5.77 66 7.2 9.77
13 1.4 1.924 40 4.3 5.92 67 7.3 9.92
14 1.5 2.072 41 4.5 6.07 68 7.4 10.06
15 1.6 2.220 42 4.6 6.22 69 7.5 10.21
16 1.7 2.368 43 4.7 6.36 70 7.6 10.36
17 1.8 2.516 44 4.8 6.51 71 7.7 10.51
18 2.0 2.664 45 4.9 6.66 72 7.8 10.66
19 2.1 2.812 46* 5.0 6.81 73 7.9 10.80
20 2.2 2.960 47 5.1 6.96 73.6* 8.0 10.89
21 2.3 3.108 48 5.2 7.10 *Minimum Dispatch Fluid Level
22 2.4 3.256 49 5.3 7.25 **Usable Reservoir Capacity
23 2.5 3.404 50 5.4 7.40
24 2.6 3.552 51 5.5 7.55
25 2.7 3.700 52 5.7 7.70
26 2.8 3.848 53 5.8 7.84
27 2.9 3.996 54 5.9 7.99
Revision 02: 11-17-09
P/N 13772-134 37 of 44
Cirrus Design Section 9
SR22 Supplements
Section 7 - System Description
The Anti-Ice System consists of porous panels on the wing, horizontal
stabilizer, and vertical stabilizer leading edges, a propeller slinger ring,
windshield spray nozzles, heated stall warning system, wing-ice
inspection lights, pumps, sensors, solenoid, filters, pump control unit,
proportioning units, fluid reservoirs, electrical switching, and
associated system plumbing.
28 VDC is supplied through the 5-amp ICE PROTECT B circuit
breaker on ESS BUS 2 and provides power directly to the #2 metering
pump which is operated by a redundant combination of the pump
controller unit and the PUMP BKUP switch. The remainder of the
system, with the exception of the stall warning, operates on 28 VDC
supplied through the 5-amp ICE PROTECT A circuit breaker on MAIN
BUS 1.
Wing and Stabilizer Porous Panels
The porous panels, mounted to the leading edge of the wing,
horizontal stabilizer, elevator horns, and vertical stabilizer, are
designed to prevent and remove ice accumulation by distributing a thin
film of glycol-based fluid over the flight surface. The presence of this
fluid lowers the freezing temperature on the flight surface below that of
the ambient precipitation preventing the formation and adhesion of ice.
Propeller Slinger Ring
Protection for the propeller is provided by a tube which directs anti-ice
fluid into a slinger ring located on the spinner back plate. Centrifugal
action throws the fluid from the slinger ring onto grooved rubber boots
fitted to the root end of each propeller blade.
Windshield Spray Nozzles and Pump
The Anti-Ice System incorporates windshield protection through the
installation of individual spray nozzles located at the base of the pilot
side windshield. Anti-ice fluid is supplied to the nozzles by an ondemand
gear pump located adjacent to the main metering pumps
beneath the cabin floor. In addition, the pump also acts as a priming
pump for the main metering pumps; In the event of a loss of system
prime, the windshield pump may be activated to purge the system of
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(110)
