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

Page: 927 / 1956

PAGE 1
Feb 28/07 5C9
34-00-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
GENERAL
1. 1995 thru 2005 ( S/N’s 4636001 thru 4636374. )
A. Standard
Traditional 3.25 inch flight instruments are installed as standard equipment . These instruments are
face mounted, see 39-10-00 for removal and installation.
B. Optional ( S/N’s 4636333 thru 4636374; and 4636299 only .)
The Meggitt Avionics next Generation Integrated Cockpit (MAGIC) Electronic Flight Instrument
System (EFIS) is available as an option on the pilot’s side only. When installed, it’s the primary flight
and navigation instrumentation. The MAGIC EFIS consists of three primary components:
(1) Primary Flight Display (PFD) [i.e. - Electronic Attitude Director Indicator (EADI)],
(2) Navigation Display (NAV) [i.e. - Electronic Horizontal Situation Indicator (EHSI)], and
(3) Air Data & Attitude Heading Reference System (ADAHRS) [i.e. - Attitude Heading Reference
System (AHRS)].
WARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN
SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER
AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION
- SUPPLEMENTARY PUBLICATIONS.)
Line maintenance of this system is limited to basic troubleshooting and that is addressed in 34-20-00.
2. 2006 and up ( S/N’s 4636375 and up. )
The Avidyne FlightMax Entegra Electronic Flight Instrument System (EFIS) is installed as standard
equipment.
This system uses three large 10.4-inch diagonal, high-resolution, sunlight-readable full color displays
(PFD and MFD), to provide standard flight instrumentation including attitude direction indicator (EADI),
horizontal situation indicator (EHSI), altitude, airspeed, vertical speed, moving map, weather, terrain and
traffic data, as well as all engine instrumentation. Two-inch standby flight instruments (i.e. - airspeed,
electric attitude indicator, and altimeter) provide redundancy. (See 34-20-00, Figure 2.)
The EFIS installation consists of the following components: pilot and co-pilot Primary Flight Displays
(PFD’s); a single Multifunction Display (MFD); Data Acquisition Unit (DAU), and associated sensors; and
two Magnetometer/OAT Sensor Assemblies.
WARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING
OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY
RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY
PUBLICATIONS.)
Line maintenance of this system is limited to basic troubleshooting and that is addressed in 34-20-00.
See 77-40-00 for additional info on the Data Acquisition Unit (DAU).