http://www.generalaviationnews.com/2010/01/11/carb-ice-suspected-in-piper-crash/
http://aircrashed.com/cause/cCHI87FA187.shtml
http://www.check-six.com/Crash_Sites/PlaneInATree-N6487J.htm
http://www.asa2fly.com/files/docs/900108NtsbRecCarbHeat.pdf
"One of the prime reasons for the persistence of accidents caused by
carburetor ice is the unpredictable nature of the phenomenon, and the
difficulty or inability of the pilot to detect it. Further, there are
documented cases of pilots who did detect carburetor ice, but too late to
avoid loss of engine power.
A typical accident of this type occurred on May 5, 1980, when a
Piper
Cherokee PA-28-151, N43954, lost engine power while on final approach to the
Front Royal, Virginia Airport.4J The pilot was unable to obtain sufficient
power from the engine, and the airplane collided with power lines 1/2 mile
short of the runway. The pilot suffered a broken back, and the airplane was
destroyed. Meteorological conditions at the time of the accident were, in
part: sky clear, visibility 15 miles, temperature 80 F.
...
"Related factors included weather conditions "conducive to carburetor/induction
system icing." According to the Piper Cherokee Owners Handbook, "Carburetor
heat should not be applied unless there is an indication of carburetor icing,
since the use of carburetor heat causes a reduction of power which may be
critical in case of a go-around. Full throttle operation with heat on is likely to
cause detonation." The pilot stated that she had no indication of carburetor ice
until she attempted to increase power.
...
Accordingly, the Safety Board believes that pilots need more definitive
guidance from airplane manufacturers concerning the use of carburetor heat on
the descent and/or before-landing checklists. Descents in most carburetorequipped
general aviation airplanes can be conducted without adverse
consequences to the powerplant with full carburetor heat on when power is
reduced below the normal cruise flight engine power setting (that is, below
the green arc on the tachometer or the manifold pressure gauge).5J The use
of this procedure would preclude the formation of carburetor ice when
detection of such formation could be difficult, in lieu of more specific
guidance or procedures from manufacturers concerning designated airplane
models .
...
Therefore, the National Transportation Safety Board recommends that the
Federal Aviation Administration:
Amend, as necessary, in conjunction with the General
Aviation Manufacturers Association and the airframe
manufacturers, the descent and before-landing checklists
in the pilot’s operating handbooks and airplane flight
manuals of carburetor-equipped airplanes to require the
use of full carburetor heat when engine power is reduced
below the normal cruise power range (the green arc on
the tachometer or the manifold pressure gauge), or below
an alternate engine power setting as determined by the
manufacturer. (Class 11, Priority Action) (A-89-140)"