曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Takeoff Distance
Factors:
The following factors are to be applied to the computed takeoff
distance for the noted condition:
• Headwind - Subtract 10% from computed distance for each 12
knots headwind.
• Tailwind - Add 10% for each 2 knots tailwind up to 10 knots.
• Grass Runway, Dry - Add 20% to ground roll distance.
• Grass Runway, Wet - Add 30% to ground roll distance.
• Sloped Runway - Increase table distances by 22% of the
ground roll distance at Sea Level, 30% of the ground roll
distance at 5000 ft, 43% of the ground roll distance at 10,000 ft
for each 1% of upslope. Decrease table distances by 7% of the
ground roll distance at Sea Level, 10% of the ground roll
distance at 5000 ft, and 14% of the ground roll distance at
10,000 ft for each 1% of downslope.
• Caution •
The above corrections for runway slope are required to be
included herein. These corrections should be used with
caution since published runway slope data is usually the net
slope from one end of the runway to the other. Many runways
will have portions of their length at greater or lesser slopes
than the published slope, lengthening (or shortening) takeoff
ground roll estimated from the table.
• If brakes are not held while applying power, distances apply
from point where full throttle and mixture setting is complete.
• For operation in outside air temperatures colder than this table
provides, use coldest data shown.
• For operation in outside air temperatures warmer than this table
provides, use extreme caution.
Conditions: Example:
• Winds.......................................... Zero Outside Air Temp ....................... 20°C
• Runway................... Dry, Level, Paved Weight...................................3400 LB
• Flaps........................................... 50% Pressure Altitude...................2000 FT
• Power...............................Full Throttle Headwind ....................................Zero
• Mixture.......................Set per Placard Runway ............................. Dry, Paved
Liftoff Speed.......................... 72 KIAS
Obstacle Speed .................... 78 KIAS
Takeoff Ground Roll ..............1299 FT
Dist. over 50' Obstacle ..........1995 FT
Original: 03-27-07
13772-130 25 of 58
Cirrus Design Section 9
SR22 Supplements
Takeoff Distance
WEIGHT = 3400 LB
Speed at Liftoff = 73 KIAS
Speed over 50 Ft. Obstacle = 78 KIAS
Flaps - 50% · Takeoff Pwr · Dry Paved
Headwind: Subtract 10% for each 12
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 917 990 1067 1146 1229 1028
50 ft 1432 1539 1650 1764 1883 1594
1000 Grnd Roll 1011 1092 1176 1264 1355 1117
50 ft 1574 1691 1813 1939 2069 1728
2000 Grnd Roll 1116 1206 1299 1395 1496 1215
50 ft 1732 1861 1995 2133 2276 1874
3000 Grnd Roll 1234 1332 1435 1542 1653 1323
50 ft 1907 2049 2196 2349 2507 2035
4000 Grnd Roll 1365 1474 1588 1706 1829 1441
50 ft 2102 2259 2422 2590 2764 2212
5000 Grnd Roll 1512 1633 1758 1889 2025 1572
50 ft 2320 2493 2673 2858 3051 2407
6000 Grnd Roll 1676 1810 1950 2095 2245 1717
50 ft 2564 2755 2953 3159 3371 2622
7000 Grnd Roll 1861 2009 2164 2325 2492 1877
50 ft 2837 3048 3267 3494 3729 2859
8000 Grnd Roll 2068 2233 2405 2584 2770 2054
50 ft 3142 3376 3619 3871 4131 3122
9000 Grnd Roll 2302 2485 2677 2875 3082 2250
50 ft 3485 3744 4014 4293 4581 3412
10000 Grnd Roll 2564 2769 2982 3204 3434 2468
50 ft 3870 4158 4457 4767 5088 3733
Original: 03-27-07
26 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Takeoff Distance
WEIGHT = 2900 LB
Speed at Liftoff = 70 KIAS
Speed over 50 Ft Obstacle = 74 KIAS
Flaps - 50% · Takeoff Pwr · Dry Paved
Headwind: Subtract 10% for each 12
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 610 659 710 763 818 684
50 ft 971 1043 1118 1195 1275 1080
1000 Grnd Roll 673 727 783 841 902 743
50 ft 1066 1146 1228 1313 1401 1170
2000 Grnd Roll 743 802 864 929 995 809
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(143)