Piper Malibu PA-46-310P Pilot Operating Handbook page 450

PIPER AIRCRAFT CORPORATION
PA-46-310P, MALIBU
NOTE
SECTION9
SUPPLEMENT 10
When icing conditions are encountered, loss of
cruise airspeed and increased fuel now resulting
from higher than normal power settings to
maintain altitude will reduce the aircraft range
significantly. The use of an alternate airport
should be considered if fuel quantity appears
marginal.
CAUTION
If cruise airspeed drops below 130 knots in icing
conditions increase power to maintain 130
knots. If maximum continuous power is re-
quired to maintain 130 knots immediate action
should be taken to exit icing conditions.
NOTE
For additional general information on inflight
icing refer to FAA Advisory Circular 91-51,
Airplane Deice and Anti-ice Systems.
SECTION 6 - WEIGHT AND BALANCE
Factory installed optional equipment is included in the licensed weight
and balance data in Section 6 of the Airplane Flight Manual.
ISSUED: JULY 30, 1984
REPORT: VB-1200
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