Piper Malibu PA-46-310P Pilot Operating Handbook page 113

PIPER AIRCRAFf CORPORATION
PA-46-310P, MALIBU
SECTION4
NORMAL PROCEDURES
CRUISE CLIMB
Mixture .................................................................................................. full RICH
Prop speed ........................................................................................... 2500 RPM
\.,,_,I
Manifold pressure ................................................................................. 35
in. Hg.
Climb speed ................................................................ 125 KIAS below 22,()()() ft
115 KIAS above 22,000 ft
Aux. fuel pump ....................................................................... LOW - if required
Pressurization controls ...................................................................................... set
CRUISING
WARNING
Operation above 25,000 ft is not approved.
NOTE
The cruise mixture must be set in strict
accordance with the procedure outlined in the
amplified procedures of this section. Failure to
do so
will
result in excess fuel burn and reduced
engine life.
NOTE
Maximum continuous T.I.T. is l 750°F.
Temporary operation up to 1800°F is
permitted in order to define peak T.I.T. In no
case should the aircraft be operated more than
30 seconds with a T.I.T. in excess of 1750°F.
Reference Section 5 power setting table and performance charts.
Maximum cruise power ................................................................................. 75%
Power ...................................................................................... set per power table
Mixture ................................................................................ 50 lean of peak T.I.T.
Aux. fuel pump .............................................................................................. OFF
Pressurization controls ................................................................................. check
ISSUED: JANUARY
11, 1984
REVISED: OCTOBER
14, 1991
REPORT: VB-1200
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