P/N 13772-150 21 of 50
Cirrus Design Section 9
SR22 Supplements
8. Left Wing Tip
• WARNING •
Pitot Probe may be HOT.
a. Pitot Probe (underside) .............................. UNOBSTRUCTED
b. Pitot Probe..............................................................VERY HOT
9. Cabin
a. Fluid Quantity .......................... VERIFY 5 GALLON MINIMUM
b. ICE PROTECT System Switch..........................................OFF
c. Flaps....................................................................................0%
d. Battery 1 Master Switch ....................................................OFF
e. Avionics Master Switch......................................................OFF
f. Cabin Speaker...................................................................OFF
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.
Original Issue: 02-01-13
To Next Page
Loading...
