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

allowed.
2. For departure from or approach to an airport, avoid prolonged
flight at low altitude near noise-sensitive areas.
Configuration Actual Maximum Allowable
Hartzel 3-blade Propeller
PHC-J3YF-1RF/F7694
83.65 dB(A) 88.00 dB(A)
Hartzel 3-blade Propeller
PHC-J3YF-1RF/F7693DF
84.81 dB(A) 88.00 dB(A)
McCauley 3-blade Propeller
D3A34C443/78CYA-0
83.15 dB(A) 88.00 dB(A)
MT 3-blade Propeller
MTV-9-D/198-52
84.80 dB(A) 88.00 dB(A)
Revision A8
P/N 13772-001 4-29
Cirrus Design Section 4
SR22 Normal Procedures
Fuel Conservation
Minimum fuel use at cruise will be achieved using the best economy
power setting described under cruise.
Revision A5
4-30 P/N 13772-001
Section 4 Cirrus Design
Normal Procedures SR22
Revision A5
Intentionally Left Blank
P/N 13772-001 5-1
Cirrus Design Section 5
SR22 Performance Data
Section 5
Performance Data
Table of Contents
Introduction .....................................................................................5-3
Associated Conditions Affecting Performance.............................5-3
Flight Planning ................................................................................5-4
Sample Problem .............................................................................5-4
Takeoff.........................................................................................5-5
Climb............................................................................................5-6
Cruise ..........................................................................................5-7
Fuel Required ..............................................................................5-8
Landing ........................................................................................5-9
Demonstrated Operating Temperature........................................5-9
Airspeed Calibration......................................................................5-10
Normal Static Source.................................................................5-10
Airspeed Calibration......................................................................5-11
Alternate Static Source ..............................................................5-11
Altitude Correction ........................................................................5-12
Normal Static Source.................................................................5-12
Altitude Correction ........................................................................5-13
Alternate Static Source ..............................................................5-13
Temperature Conversion ..............................................................5-14
Outside Air Temperature for ISA Condition ..................................5-15
Stall Speeds..................................................................................5-16
Wind Components ........................................................................5-17
Takeoff Distance ...........................................................................5-18
Takeoff Distance ...........................................................................5-19
Takeoff Distance ...........................................................................5-20
Takeoff Climb Gradient .................................................................5-21
Takeoff Rate of Climb ...................................................................5-22
Enroute Climb Gradient ................................................................5-23
Enroute Rate of Climb...................................................................5-24
Enroute Rate of Climb Vs Density Altitude ...................................5-25
Time, Fuel and Distance to Climb.................................................5-26
Cruise Performance ......................................................................5-27
Cruise Performance ......................................................................5-28
Revision A7
5-2 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Cruise Performance ......................................................................5-29
Range / Endurance Profile ............................................................5-30
Range / Endurance Profile ............................................................5-31
Range / Endurance Profile ............................................................5-32
Balked Landing Climb Gradient ....................................................5-33
Balked Landing Rate of Climb.......................................................5-34
Landing Distance ..........................................................................5-35
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：CIRRUS DESIGN SR22西銳22飛行員操作手冊和飛機飛行手冊(39)