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Flaps 0% (UP)
Wind Zero Glide Distance 13.9 NM
SR22_FM09_2438
GROUND DISTANCE - NAUTICAL MILES
HEIGHT ABOVE GROUND - FEET
0 2 4 6 8 10 12 14 16 18 20
0
2000
4000
6000
8000
10000
12000
14000
Figure - 1
Maximum Glide
Revision 02: 08-26-09
4 of 8 P/N 13772-129
Section 9 Cirrus Design
Supplements SR22
Section 4 - Normal Procedures
Climb
Aircraft with subject propeller must use higher climb speeds to
facilitate engine cooling. For climb, follow basic AFM procedure but
use performance data in Section 5 of this supplement.
Noise Characteristics/Abatement
The certificated noise levels for the Cirrus Design SR22 established in
accordance with FAR 36 Appendix G are:
Section 5 - Performance
Installation of the subject propeller changes the climb airspeeds
required to meet engine cooling requirements on hot days. Refer to the
basic AFM for all performance information except for the following
tables.
Configuration Actual Maximum Allowable
Hartzel 3-blade Propeller
PHC-J3YF-1N/N7605(B)
83.50 dB(A) 88.00 dB(A)
Hartzel 3-blade Propeller
PHC-J3Y1F-1N/N7605(B)
83.50 dB(A) 88.00 dB(A)
Revision 02: 08-26-09
P/N 13772-129 5 of 8
Cirrus Design Section 9
SR22 Supplements
Enroute Climb Gradient
• Note •
• Climb Gradients shown are the gain in altitude for the horizontal distance traversed
expressed as Feet per Nautical Mile.
• For operation in air colder than this table provides, use coldest data shown.
• For operation in air warmer than this table provides, use extreme caution.
Conditions: Example:
• Power .............................. Full Throttle Outside Air Temp........................20°C
• Mixture ...................... Set Per Placard Weight .................................. 3400 LB
• Flaps .....................................0% (UP) Pressure Altitude .................. 4000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed ...................109 Knots
Gradient............................529 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 ISA
3400
SL 112 769 731 694 657 703
2000 110 682 645 610 574 689
4000 109 598 563 529 495 607
6000 108 518 484 451 419 528
8000 107 440 408 376 346 452
10000 105 366 335 305 276 379
12000 104 295 266 237 209 308
14000 103 228 199 171 145 240
16000 102 163 135 109 84 175
2900
SL 112 951 907 862 819 873
2000 110 849 806 763 722 867
4000 109 751 709 669 629 771
6000 108 657 617 578 540 679
8000 107 567 529 491 455 591
10000 105 481 444 408 374 506
12000 104 398 363 329 296 425
14000 103 320 286 253 222 346
16000 102 244 212 181 152 271
Revision 02: 08-26-09
6 of 8 P/N 13772-129
Section 9 Cirrus Design
Supplements SR22
Enroute Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• For operation in air colder than this table provides, use coldest data shown.
• For operation in air warmer than this table provides, use extreme caution.
Conditions: Example:
• Power...............................Full Throttle Outside Air Temp ....................... 20°C
• Mixture.......................Set Per Placard Weight...................................3400 LB
• Flaps.....................................0% (UP) Pressure Altitude...................6000 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed................... 108 Knots
Rate of Climb .......................913 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~°C
-20 0 20 40 ISA
3400
SL 112 1328 1314 1292 1266 1298
2000 110 1211 1192 1167 1138 1179
4000 109 1093 1070 1041 1008 1060
6000 108 974 946 913 877 941
8000 107 853 821 784 745 822
10000 105 730 694 654 612 703
12000 104 606 566 523 477 584
14000 103 481 437 390 341 465
16000 102 354 306 255 203 346
2900
SL 112 1636 1622 1600 1572 1606
2000 110 1503 1484 1458 1426 1479
4000 109 1368 1345 1314 1278 1344
6000 108 1233 1204 1169 1130 1208
8000 107 1095 1062 1023 980 1073
10000 105 957 918 875 829 939
12000 104 816 773 726 676 804
14000 103 675 627 576 523 670
16000 102 532 480 425 368 536
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(95)
