Piper Malibu PA-46-310P Pilot Operating Handbook page 443

SECTION9
SUPPLEMENT 10
SECTION 1 - GENERAL
PIPER AIRCRAFf CORPORATION
PA-46-310P, MALIBU
This supplement supplies information necessary for the operation of the
airplane when the optional Ice Protection System is installed in accordance
with .. FAA Approved" Piper data.
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SECTION 2 - LIMITATIONS
(a) The ice protection system was designed and tested for operation
in the meteorological conditions of FAR 25, Appendix C, for
continuous maximum and intermittent maximum icing conditions.
The ice protection system was not designed or tested for flight
in freezing rain and/or mixed conditions or for icing
conditions more severe than those of FAR 25, Appendix C.
Therefore, flight in those conditions may exceed the capabilities
of the ice protection system.
(b) Equipment required for flight into known or forecast icing:
( 1) Pneumatic wing and empennage boots.
(2) Wing ice detection light.
(3) Electrothermal propeller deice pads on the propeller blades.
( 4) Electrothermal windshield panel.
(5) Heated lift detector.
( 6) Heated pilot head.
(7) Dual alternators.
(8) Dual vacuum pumps.
(9) Alternate static source.
( I 0) All equipment required for night IFR flight.
(c) If all the equipment listed is not installed and operative, the following
placard must be installed in full view of the pilot.
WARNING
This aircraft is not approved for flight in icing
conditions.
REPORT: VB-1200
9-88, 2
of
16
ISSUED: JULY 30, 1984
REVISED: OCTOBER 15, 1997