Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 935 / 1956

PAGE 7
Feb 28/07 5C17
34-10-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
(c) Increase the simulator airspeed indication to 210 knots.
(d) Decrease the simulator airspeed indication until the overspeed aural alarm first stops.
Verify that the simulator indicates an airspeed of less than 198 knots.
(e) Turn OFF the PFD (i.e. - EADI).
(12) When equipped with the Avidyne Entegra EFIS:
(a) Turn OFF the copilot’s PFD.
(b) Operate the simulator to indicate 140 knots on the pilot’s PFD. Verify that the pilot’s PFD
indicates within three (3) knots of the simulator indication.
(c) Turn OFF the pilot’s PFD and turn ON the copilot’s PFD.
(d) Repeat step (b) for the copilot’s PFD and for the standby airspeed indicator.
(e) Turn ON the pilot’s PFD and turn OFF the copilot’s PFD.
(f) Operate the simulator until the overspeed aural alarm first sounds. Verify that the
simulator indicates an airspeed of 198 to 204 knots.
(g) Increase the simulator airspeed indication to 210 knots.
(h) Decrease the simulator airspeed indication until the overspeed aural alarm first stops.
Verify that the simulator indicates an airspeed of less than 198 knots.
(i) Turn OFF the pilot’s PFD and turn ON the copilot’s PFD.
(i) Repeat steps (f) - (h).
(13) Remove the test fixture from the pitot head.
(14) Attach static test fixture to the static port and pitot test port of the aircraft. Tape over the other
static button.
(15) When equipped with the optional Meggitt EFIS, turn ON the PFD (i.e. - EADI).
(16) When equipped with the Avidyne Entegra, turn ON the Pilot’s PFD.
(17) Set the aircraft altimeter needles to read zero altitude. Operate the static simulator to cause the
aircraft altimeter needles to read 1,000 feet altitude. Momentarily open the alternate static port.
There should be a decrease in altimeter indication. If no change occurs the system is blocked
and must be repaired prior to further testing.
(18) Increase altitude to 1,050 feet.
(19) Check that the aircraft altimeter shows an increase.
(20) Observe the aircraft altimeter. Loss of indicated altitude shall not exceed 100 feet in one
minute.
(21) Increase altitude to 12,700 feet.
(22) Check that the aircraft altimeter shows an increase.
(23) Observe the aircraft altimeter. Loss of indicated altitude shall not exceed 254 feet in one
minute.
(24) If a leak exceeds the tolerances in step (18) or (21), check the fixture installation, plumbing and
fittings. Repair the leak when found and repeat the static system checks above.
(25) When equipped with the optional Meggitt EFIS, turn OFF the PFD (i.e. - EADI).
(26) When equipped with the Avidyne Entegra, turn OFF the Pilot’s PFD and turn ON the copilot’s
PFD. Repeat steps (17) thru (24) for copilot’s PFD.
(27) Remove the test fixture and tape from the static button.