Stalls - Cessna TR182 1979 Pilot Operating Handbook

CESSNA
MODEL TR182
SECTION 4
NORMAL PROCEDURES
MIXTURE
EXHAUST GAS
DESCRIPTION
TEMPERATURE
RECOMMENDED LEAN
(Pilot's Operating Handbook 50
0
F Rich of Peak EGT
and Power Computer)
BEST ECONOMY Peak EGT
Figure 4-4. EGT Table
peak EGT is established, then enrichen to any desired mixture setting that
allows smooth engine operation.
The mixture may be leaned during descent to provide smooth engine
operation and improved fuel economy. Any change in altitude, power or
carburetor heat will require a change in the mixture setting and a recheck
of the EGT.
Carburetor ice, as evidenced by an unexplained drop in manifold
pressure, can be removed by application of full carburetor heat. Upon
regaining the original manifold pressure indication (with heat off),use the
minimum amount of heat (by trial and error) to prevent ice from forming.
When operating above approximately
5000
feet at maximum recommended
cruise power, the heat available from turbocharging increases with
altitude and carburetor icing becomes less likely.
Carburetor heat may be used an an alternate air source in the event the
induction air filter becomes blocked. However, since application of full
carburetor heat at high altitudes may result in the loss of as much as 10
inches of manifold pressure, carburetor heat should be used only as
necessary. With carburetor heat on, throttle and mixture should be
readjusted as necessary.
STALLS
The stall characteristics are conventional and aural warning is
provided by a stall warning horn which sounds between
5
and 10knots
above the stall in all configurations. Altitude loss during stall recovery
may be as much as
300
feet.
Power-off stall speeds at maximum weight for both forward and aft
C.G. positions are presented in Section
5.
1 October 1978
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