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SECTION 9
SUPPLEMENT 3
SECTION 1 - GENERAL
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.
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 and SURF DEICE an-
nunciation.
(2) Wing ice detection light.
(3) Electrothermal propeller deice pads on the propeller blades.
(4) Electrically heated windshield and WSHLD HEAT annunciation.
(5) Heated lift detector.
(6) Heated pitot head.
(7) Dual alternators.
(8) Dual vacuum pumps.
(9) Alternate static source.
(10) All equipment required for night IFR flight.
(c) If all the equipment listed is not installed and operative, the fol-
lowing placard must be installed in full view of the pilot.
THIS AIRCRAFT IS NOT APPROVED FOR
FLIGHT IN ICING CONDITIONS.
REPORT:-1710
9-16, 2 of 16
WARNING
ISSUED: FEBRUARY 23, 1999
PA-46-350P, MALIBU
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