Service manual

4.33 GO-AROUND (4.5n)
To initiate a go-around from a landing approach, the mixture should be
set to full RICH, the propeller control should be at full INCREASE, and the
throttle should be advanced to full power while the pitch attitude is increased
to obtain the balked landing climb speed of 80 KIAS. Retract the landing
gear and slowly retract the flaps when a positive climb is established. Allow
the airplane to accelerate to the best angle of climb speed (81 KIAS) for
obstacle clearance or to the best rate of climb speed (110 KIAS) if obstacles
are not a factor. Reset the longitudinal trim as required.
4.35 AFTER LANDING (4.5o)
When clear of the active runway, move the induction air control to
PRIMARY, retract the flaps, and turn the air conditioner on as desired.
Turn OFF the radar, emergency (EMERG) fuel pump, and strobe lights.
Turn OFF the landing and taxi lights as required.
4.37 STOPPING ENGINE (4.5p)
Prior to shutdown, all radio and electrical equipment and external lights
should be turned OFF.
The air conditioner should be turned OFF, the propeller control set in
the full INCREASE position, and the throttle should be CLOSED until there
is a decided decrease in CHT. Increase throttle to 1000 rpm. Maintain speed
for approximately 30 seconds to ensure adequate scavenging of turbocharger
oil system. Stop the engine by pulling the mixture control back to idle cut-
off. After the engine stops, both magneto switches, alternator switches, and
battery master switches must be turned OFF.
4.33 GO-AROUND (4.5n)
To initiate a go-around from a landing approach, the mixture should be
set to full RICH, the propeller control should be at full INCREASE, and the
throttle should be advanced to full power while the pitch attitude is increased
to obtain the balked landing climb speed of 80 KIAS. Retract the landing
gear and slowly retract the flaps when a positive climb is established. Allow
the airplane to accelerate to the best angle of climb speed (81 KIAS) for
obstacle clearance or to the best rate of climb speed (110 KIAS) if obstacles
are not a factor. Reset the longitudinal trim as required.
4.35 AFTER LANDING (4.5o)
When clear of the active runway, move the induction air control to
PRIMARY, retract the flaps, and turn the air conditioner on as desired.
Turn OFF the radar, emergency (EMERG) fuel pump, and strobe lights.
Turn OFF the landing and taxi lights as required.
4.37 STOPPING ENGINE (4.5p)
Prior to shutdown, all radio and electrical equipment and external lights
should be turned OFF.
The air conditioner should be turned OFF, the propeller control set in
the full INCREASE position, and the throttle should be CLOSED until there
is a decided decrease in CHT. Increase throttle to 1000 rpm. Maintain speed
for approximately 30 seconds to ensure adequate scavenging of
turbocharger oil system. Stop the engine by pulling the mixture control back
to idle cut-off. After the engine stops, both magneto switches, alternator
switches, and battery master switches must be turned OFF.
SECTION 4
PA-46-350P, MALIBU NORMAL PROCEDURES
SECTION 4
PA-46-350P, MALIBU NORMAL PROCEDURES
ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710
4-35
ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710
4-35
FOR REFERENCE ONLY
NOT FOR FLIGHT