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

(1) Verify evidence of anti-ice fluid from spray nozzles.
h. ICE PROTECT System Switch ........................................... ON
i. ICE PROTECT Mode Switch .........................................NORM
(1) Metering Pump Duty Cycle ..........Verify 30s ON, 90s OFF
(2) Anti-Ice Fluid and Endurance Indications.............. CHECK
j. ICE PROTECT System Switch ..........................................OFF
k. PUMP BKUP Switch........................................................... ON
(1) Metering Pump Duty Cycle ...........Verify Continuously ON
Revision 02: 11-17-09
P/N 13772-134 19 of 44
Cirrus Design Section 9
SR22 Supplements
(2) Anti-Ice Fluid and Endurance Indications ............. CHECK
l. PUMP BKUP Switch..........................................................OFF
m. ICE Inspection Lights Switch...............................................ON
(1) Verify LH and RH Operation.
n. PITOT HEAT Switch .......................ON 45 seconds, then OFF
• WARNING •
Pitot Mast may be HOT.
(1) Exit airplane and verify Pitot Mast is hot.
o. ICE PROTECT System Switch............................................ON
p. ICE PROTECT Mode Switch...........................................HIGH
(1) Metering Pump Duty Cycle ...........Verify Continuously ON
(2) Anti-Ice Fluid and Endurance Indications ............. CHECK
2. Empennage
a. Stabilizers Porous Panels................CONDITION / SECURITY
(1) Verify Evidence of Anti-Ice Fluid Along Length of Panels
and Elevator Horns.
3. Right Wing Forward and Main Gear
a. Fluid Reservoir ........................VERIFY DESIRED QUANTITY
(1) Check Cap Condition and Security.
b. Porous Panels ..........................CONDITION AND SECURITY
(1) Check Evidence of Anti-Ice Fluid Along Length of Panels.
• WARNING •
Stall Warning Faceplate and Vane may be HOT.
c. Stall Warning Transducer Faceplate........ PERCEPTIBLY HOT
d. Stall Warning Vane.................................................VERY HOT
(1) Verify Stall Warning System audio annunciation within 4
seconds after lifting stall vane with wooden tooth pick or
tongue depressor.
(Continued on following page)
Revision 02: 11-17-09
20 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
e. Fluid Vent (underside wing) ........................UNOBSTRUCTED
4. Nose, Right Side
a. Ice-Inspection Light .........................CONDITION / SECURITY
5. Nose Gear, Propeller, Spinner
a. Slinger Ring ..........................EVIDENCE OF ANTI-ICE FLUID
6. Nose, Left Side
a. Ice-Inspection Light .........................CONDITION / SECURITY
b. Windshield Spray Nozzles ...............CONDITION / SECURITY
7. Left Wing Forward and Main Gear
a. Fluid Reservoir ........................VERIFY DESIRED QUANTITY
(1) Check Cap Condition and Security.
b. Porous Panels..................................CONDITION / SECURITY
(1) Check Evidence of Anti-Ice Fluid Along Length of Panels.
c. Fluid Vent (underside wing) ........................UNOBSTRUCTED
8. Left Wing Tip
a. Pitot Mast (underside) ................................UNOBSTRUCTED
9. Cabin
a. Fluid Quantity .......................... VERIFY 5 GALLON MINIMUM
b. ICE PROTECT System Switch ..........................................OFF
c. Battery 1 Master Switch ....................................................OFF
d. Avionics Master Switch......................................................OFF
e. Cabin Speaker ...................................................................OFF
f. Flaps....................................................................................0%
Ice Formation Determination
Typically, a leading edge with a small radius will collect ice more
quickly than a leading edges with a large radius. To help monitor
possible ice accumulation, a thin metal tab is attached to the outboard
end of the RH and LH stall strips. In some icing conditions this tab may
be the first place that airframe ice accretion is noticeable. Additionally,
refer to other areas of the aircraft, such as the horizontal tail and lower
windscreen, to aid in determining if ice is accreting to the aircraft.
Revision 02: 11-17-09
P/N 13772-134 21 of 44
Cirrus Design Section 9
SR22 Supplements
Before Takeoff
If icing conditions are anticipated immediately after take-off:
1. ICE PROTECT System Switch ..................................................ON
2. ICE PROTECT Mode Switch ...................................NORM / HIGH
3. PITOT HEAT Switch...................................................................ON
4. Cabin Heat ...............................................................................HOT
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 2979(104)