SR22 AMM - Cirrus Aircraft

SR22 AMM - Cirrus Aircraft
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
CENTRAL DISPLAY SYSTEMS
1. DESCRIPTION
This section covers those systems and components which give visual display of conditions in unrelated
systems. This includes the multi-function display and primary flight display.
A. Multi-Function Display (MFD)
(1)
ARNAV MFD
The multi-function display, located on the instrument panel, provides 10.4-inch diagonal, color
depiction of navigational data from its own database and position and flight-plan data from the
GPS receiver. 28 VDC is supplied through the 5-amp MFD circuit breaker on the Avionics NonEssential Bus. For additional information on the ARNAV MFD, refer to the ICDS 2000 Operations Handbook. (Refer to 05-10)
(2)
Avidyne MFD
The multi-function display, located on the instrument panel, provides 10.4-inch diagonal, color
depiction of navigational data from its own database and position and flight-plan data from the
GPS receiver. 28 VDC is supplied through the 5-amp MFD circuit breaker on the Avionics NonEssential Bus.
Serials 22-0002 thru 22-1601, 22-1603 thru 22-1643, 22-1645 thru 22-1662 w/ EMax Engine
Monitoring, 22-1602, 22-1644, 22-1663 & subs: The MFD displays fuel flow, nautical miles per
gallon, fuel remaining, fuel-to-waypoint, fuel-to-destination, cylinder head temperatures (CHT),
exhaust gas temperatures (EGT), engine crankshaft speed, manifold pressure, oil temperature,
oil pressure, outside air temperature (OAT), and electrical bus voltages. For additional information on the Avidyne MFD, refer to the FlightMax EX-Series MFD Pilot’s Guide. (Refer to 05-10)
(3)
Perspective MFD
Airplanes are equipped with either a Garmin GDU 1040 10-inch or Garmin GDU 1240 12-inch
multi-function display. The MFD, located above the center console, depicts navigation, terrain,
lightning, traffic data, NAV/COM frequencies, and annunciation information. All engine data is
displayed on a dedicated ENGINE page. When the ENGINE page is not shown, all essential
engine information is shown on an engine strip at the edge of the display.
Redundant power sources provide 28 VDC for MFD operation. Power is supplied through the 5amp MFD PWR 1 circuit breaker on the MAIN BUS 3 and the 5-amp MFD PWR 2 circuit breaker
on MAIN BUS 1. Either circuit is capable of powering the MFD. System start-up is automatic
once power is applied. Power-on default brightness is determined by ambient lighting and is
user adjustable. For additional information on the Perspective MFD, refer to the Cirrus Perspective Integrated Avionics System Pilot’s Guide. (Refer to 05-10)
B. Primary Flight Display (PFD)
(1)
Avidyne PFD
Airplanes are equipped with the Avidyne FlightMax Entegra-Series Primary Flight Display (PFD).
The PFD is a 10.4-inch landscape-oriented display located in the LH instrument panel. The PFD
is intended to be the primary display for attitude, airspeed, heading, and altitude.
The PFD acts as the primary attitude indicator, heading indicator, airspeed indicator, altimeter,
vertical speed indicator, directional gyro, course deviation indicator, and altitude pre-select controller within a single electronic display. The PFD replaces the Horizontal Situation Indicator
(HSI), Vertical Speed Indicator (VSI), VOR/LOC Indicator, altitude alerter, and the OAT gage/
clock.
Serials 22-1602, 22-1644, 22-1663 & subs: The PFD provides for the primary display of engine
speed, manifold pressure, fuel flow, and oil pressure. Percent power is provided on the upper LH
portion of the display in vertical tape format and as text. This vertical tape representation of percent power is the primary indicator to set engine power. Engine RPM, manifold pressure (MAP),
EFFECTIVITY:
All
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
fuel flow, and oil pressure are displayed full time as text in the engine parameters field located in
the lower right corner of the PFD.
The PFD communicates with GPS 1, GPS 2, NAV 1, NAV 2 and accepts data from GPS sensors
and System 55X Autopilot. The airplane's Pitot-Static system is connected to the PFD to provide
airspeed, altitude, and vertical speed.
A magnetometer assembly is mounted in the RH wing to provide three axis magnetic field vector
measurements and outside air temperature (OAT) data. (Refer to 34-20)
To provide roll data to the autopilot system, a turn coordinator is mounted inside the console.
(Refer to 34-20)
An integral air data/attitude and heading reference system (ADAHRS) uses a 3-axis solid state
gyro and accelerometer system combined with a flux-gate compass to replace the vertical and
directional gyros. ADAHRS also provides roll, pitch, heading data and continually updates the
winds aloft and true airspeed (TAS) indications on the PFD.
In case of total or partial PFD failure, backup instruments for airspeed, attitude, and altitude are
mounted on the LH bolster panel.
Battery power is supplied directly to the PFD from either one of the two airplane batteries.
Because the PFD does not have an on/off switch, the PFD will become energized as soon as
either battery switch is turned on. The pilot can control intensity of the PFD display by using the
brightness control on the upper RH side of the PFD bezel. The brightness of the buttons is controlled by the dimmer control switch on the bolster panel. For additional information on the Avidyne PFD, refer to the FlightMax Entegra PFD Pilot's Guide. (Refer to 05-10)
(2)
Perspective PFD
Airplanes are equipped with either a Garmin GDU 1040 10-inch or Garmin GDU 1240 12-inch
primary flight display. The PFD, located directly in front of the pilot, is intended to be the primary
display of flight parameter information (attitude, airspeed, heading, and altitude) during normal
operations. The PFD accepts data from a variety of sources, including the MFD and the Integrated Avionics Units through a high-speed data bus connection. In conjunction with Flight Management System Keyboard, the PFD also controls and displays all communication and
navigation frequencies as well as displaying warning/status annunciations on aircraft systems.
During engine start, reversionary operation (MFD failure), or when the reversionary switch is
selected, engine system information is displayed on the PFD. Redundant power sources provide
28 VDC for PFD operation. Power is supplied through the 5-amp PFD PWR 1 circuit breaker on
the ESS BUS 1 and the 5-amp PFD PWR 2 circuit breaker on MAIN BUS 2. Either circuit is
capable of powering the PFD. System start-up is automatic once power is applied. Power-on
default brightness is determined by ambient lighting and is user adjustable. Typical alignment
time is 60 seconds from battery turn on.
In the event of a detected display failure, the Perspective Avionics System automatically
switches to reversionary mode. In reversionary mode, all essential flight information from the
PFD is presented on the remaining display in the same format as in normal operating mode with
the addition of the engine indicating system. The reversionary switch, located on the center
instrument panel between the PFD and MFD, may be used to manually activate the reversionary
mode. For additional information on the Perspective PFD, refer to the Cirrus Perspective Integrated Avionics System Pilot’s Guide. (Refer to 05-10)
31-60
Page 2
15 Jun 2010
EFFECTIVITY:
All
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
C. Troubleshooting - Serials w/ Avidyne PFD
Trouble - PFD Attitude Display
Probable Cause
Remedy
Pitch ladder and horizon removed PFD Air Data Attitude Heading
Replace PFD. (Refer to 31-60)
and replaced with red X.
Reference System (ADAHRS) failure.
Trouble - PFD Altitude,
Airspeed, Vertical Velocity
Display
Instruments removed and
replaced with red X.
Trouble - PFD Heading
Heading indication removed and
replaced with red X.
Excessive heading error.
Trouble - PFD OAT
Probable Cause
Remedy
PFD Air Data Computer failure.
Replace PFD. (Refer to 31-60)
Pitot-Static failure.
Repair pitot-static system.
Probable Cause
Remedy
Open or shorted wire between
PFD and Magnetometer.
Test and repair wiring.
Magnetometer failed.
Replace Magnetometer/OAT
assembly. (Refer to 34-20)
PFD RS-422 or Magnetometer
output power failure.
Replace PFD. (Refer to 31-60)
Magnetometer not properly calibrated.
Calibrate Magnetometer. (Refer to
34-20)
Probable Cause
Remedy
Display indicates red dashes.
OAT probe failed.
Replace Magnetometer/OAT
assembly. (Refer to 34-20)
Excessive temperature error.
OAT probe failed.
Replace Magnetometer/OAT
assembly. (Refer to 34-20)
Trouble - PFD True Airspeed
Display indicates red dashes.
EFFECTIVITY:
Serials w/ Avidyne PFD
Probable Cause
OAT probe failed.
Remedy
Replace Magnetometer/OAT
assembly. (Refer to 34-20)
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
Trouble - PFD VHF/GPS NAV 1
PFD Primary Nav, Bearing, or
Auxiliary indication displays
dashes when GPS 1 or VLOC 1
selected.
Probable Cause
MODELS SR22 AND SR22T
Remedy
VHF/GPS NAV 1 not configured
properly.
Configure Garmin 430.
Open or shorted wire between
PFD and VHF/GPS NAV 1.
Test and repair wiring.
VHF/GPS NAV 1 ARINC 429 out- Replace VHF/GPS NAV 1.
put failed.
PFD ARINC 429 input failed.
GPS1 does not slave to PFD
course pointer in OBS mode.
Replace PFD. (Refer to 31-60)
Open or shorted ARINC 429 wire Test and repair wire.
between PFD and GPS NAV 1.
ARINC 429 receive input failed.
Replace VHF/GPS NAV 1.
ARINC 429 transmit output failed. Replace PFD. (Refer to 31-60)
Trouble - PFD VHF/GPS NAV 2
PFD Primary Nav, Bearing, or
Auxiliary indication displays
dashes when GPS 2 or VLOC 2
selected.
Probable Cause
Remedy
VHF/GPS NAV 2 not configured
properly.
Configure Garmin 430.
Open or shorted wire between
PFD and VHF/GPS NAV 2.
Test and repair wiring.
VHF/GPS NAV 2 ARINC 429 out- Replace VHF/GPS NAV 2.
put failed.
PFD ARINC 429 input failed.
Trouble - PFD Autopilot
Integration
Airspeed, Heading, or Altitude
bugs do not "fill" but autopilot
modes still engage.
Probable Cause
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15 Jun 2010
Remedy
Open or shorted annunciator wires Test and repair wiring.
between PFD and autopilot computer.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
Autopilot VS mode does not track Open or shorted VS command
PFD Vertical Speed setting, but
wires between PFD and autopilot
autopilot mode engages.
computer.
31-60
Replace PFD. (Refer to 31-60)
Test and repair wiring.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
EFFECTIVITY:
All
CIRRUS
AIRPLANE MAINTENANCE MANUAL
Trouble - PFD Autopilot
Integration
Autopilot HDG mode does not
track PFD Heading setting, but
autopilot mode engages.
Probable Cause
Test and repair wiring.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
PFD heading bug out of alignment.
Perform PFD heading bug calibration.
EFFECTIVITY:
All
Test and repair wiring.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
Autopilot out of alignment.
Perform autopilot alignment in
NAV mode.
Autopilot NAV annunciator flashes Open or shorted CDI flag wire
and FAIL indication appears.
between PFD and autopilot computer.
Autopilot APR mode fails to
engage.
Remedy
Open or shorted heading datum
wire between PFD and autopilot
computer.
Autopilot NAV mode does not
Open or shorted course datum
track PFD Nav Course Pointer set- and cross track wires between
ting or CDI.
PFD and autopilot computer.
Autopilot APR mode does not
track PFD CDI or VDI.
MODELS SR22 AND SR22T
Test and repair wiring.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
VHF/GPS NAV 1 or 2 Nav data
invalid.
Refer to VHF/GPS NAV 1 & 2
Troubleshooting procedure.
PFD interface failure.
Replace PFD. (Refer to 31-60)
Open or shorted CDI and VDI
Test and repair wiring.
wires between PFD and autopilot
computer.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
Open or shorted glideslope flag or Test and repair wiring.
LOC switch wires between PFD
and autopilot computer.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
Trouble - PFD Autopilot
Integration
Autopilot computer display indicates vertical speed value.
Autopilot GPSS mode fails to
engage.
Probable Cause
Page 6
15 Jun 2010
Remedy
Open or shorted ALT select wire
between PFD and autopilot.
Test and repair wiring.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
Open or shorted PFD ARINC 429 Test and repair wiring.
transmit or autopilot relay control
wire.
Autopilot relay failure.
Replace autopilot relay.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
Autopilot GPSS only follows GPS Break in autopilot relay control
1 source.
wire.
31-60
MODELS SR22 AND SR22T
Test and repair wire.
Autopilot relay failure.
Replace autopilot relay.
Autopilot computer interface failure.
Replace autopilot unit. (Refer to
22-11)
PFD interface failure.
Replace PFD. (Refer to 31-60)
EFFECTIVITY:
All
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
D. Troubleshooting - Serials w/ Perspective Avionics
Trouble - PFD
PFD display does not power up.
Probable Cause
PFD failure.
Remedy
Ensure power is present at display backshell connector.
Replace PFD. (Refer to 31-60)
GIA1 and/or GIA2 to LRU data
path not working.
GIA1 and/or GIA2 configuration
failure.
Ensure GIA1 and GIA2 are configured correctly.
Check wiring, connectors & pins
as needed.
EFFECTIVITY:
Serials w/ Perspective Avionics
31-60
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CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
#1 GNS-430
GPS
#2 GNS-430
GPS
or
GNC-420
GPS
SkyWatch
WX-500 Stormscope
Avidyne MFD
MFD
10
AVIONICS NON-ESSENTIAL
BUS
Serials 22-0002 thru 22-0434, 22-0435 thru 22-0820 w/o PFD.
SR22_MM31_2526
Figure 31-601
Flight Display System Schematic - Serials 22-0002 thru 22-0820 w/o PFD (Sheet 1 of 3)
31-60
Page 8
15 Jun 2010
EFFECTIVITY:
Serials 22-0002 thru 22-0820 w/o PFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
PFD 2
MAIN BUS 2
10
PFD 1
ESSENTIAL BUS
10
#1 GNS-430
GPS
Pitot
Static
Avidyne PFD
Data Aquisition Unit
#2 GNS-430
GPS
or
GNC-420
GPS
OAT Sensor /
Magnetometer
F
OF
AP ON
FD
ON
AP
Flight Director System
Avidyne MFD
STEC System 55x
Autopilot
WX-500 Stormscope
SkyWatch
MFD
TAWS
10
AVIONICS NON-ESSENTIAL
BUS
Serials 22-0435 thru 22-0820 w/ PFD, 22-0821 & subs.
NOTE
Serials w/ Flight Director.
Serials 22-1602, 22-1644, 22-1663 & subs.
SR22_MM31_1604C
Figure 31-601
Flight Display System Schematic - Serials 22-0435 & subs w/ Avidyne MFD & PFD (Sheet 2 of 3)
EFFECTIVITY:
Serials 22-0435 & subs w/ Avidyne MFD & PFD
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
MFD PWR 1
PFD PWR 1
ESS BUS 1
5
MFD PWR 2
PFD PWR 2
MAIN BUS 2
5
5
MAIN BUS 3
5
MAIN BUS 1
PFD
MFD
Satellite Data
Link Receiver
(optional)
FMS Keyboard
Magnetometer 2
Magnetometer 1
AHRS 1
Autopilot
Mode Controller
(optional)
AHRS 2
Air Data
Computer
Integrated
Avionics Unit 2
Integrated
Avionics Unit 1
SR22_MM31_2938
Figure 31-601
Flight Display System Schematic - Serials w/ Perspective Avionics (Sheet 3 of 3)
31-60
Page 10
15 Jun 2010
EFFECTIVITY:
Serials w/ Perspective Avionics
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
BRIGHTNESS
CONTROL
L1
R1
L2
R2
L3
R3
L4
R4
L5
R5
LEFT KNOB
RIGHT KNOB
Multi-Function Display (MFD).
Serials 22-0002 & subs.
BRIGHTNESS
CONTROL
L1
R1
L2
R2
L3
R3
L4
R4
LEFT KNOB
RIGHT KNOB
Primary Flight Display (PFD).
Serials 22-0435 thru 22-0820 w/ PFD, 22-0821 & subs.
NOTE
Line select keys.
SR22_MM31_2556
Figure 31-602
Display Controls - Serials 22-0435 & subs w/ Avidyne MFD & PFD (Sheet 1 of 2)
EFFECTIVITY:
Serials 22-0435 & subs w/ Avidyne MFD & PFD
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
VOLUME KNOB
FREQUENCY CONTROL
NAV KNOB
Multi-Function Display (MFD).
Serials w/ Perspective Avionics.
VOLUME KNOB
FREQUENCY CONTROL
COM KNOB
BARO KNOB
RANGE / PAN KNOB
KEYPAD
FMS KNOB
Primary Flight Display (PFD).
Serials w/ Perspective Avionics.
FMS / XPDR / COM / NAV
KNOB
MODE
KEYPAD
KEYS
HDG KNOB
RANGE KNOB
FREQUENCY CONTROL
CRS KNOB
ALT SEL KNOB
NOTE
Soft keys.
Alphanumeric keys.
Flight Management System Keyboard
Serials w/ Perspective Avionics.
Figure 31-602
Display Controls - Serials w/ Perspective Avionics (Sheet 2 of 2)
31-60
Page 12
15 Jun 2010
EFFECTIVITY:
Serials w/ Perspective Avionics
SR22_MM31_2940
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
2. MAINTENANCE PRACTICES
A. Multi-Function Display (MFD) - Serials 22-0002 thru 22-0141 w/ ARNAV MFD (See Figure 31-603)
(1)
Removal - ARNAV MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Pull MFD circuit breaker.
(c)
Remove center bolster trim. (Refer to 25-10)
(d) Rotate captive screws counter-clockwise to loosen MFD from instrument panel.
CAUTION:
(2)
(3)
When removing MFD, do not strain wire harness by pulling cable too far
from instrument panel.
(e) Pull MFD from instrument panel just sufficiently to expose cable connector.
(f)
Rotate cable plug counter-clockwise, then remove from receptacle.
(g) Remove MFD from airplane.
Installation - ARNAV MFD
(a) Position MFD close enough to instrument panel cutout to connect cable plug to receptacle
without straining wire harness.
(b) Slide MFD forward into instrument panel cutout until captive screws align with instrument
panel mounting holes.
(c)
Rotate captive screws clockwise until detent position is felt, indicating screw is aligned
with receptacle. Continue clockwise rotation approximately 1/4 rotation until screw is
secure.
(d) Reset MFD circuit breaker.
(e) If MFD is a different unit from the originally installed MFD:
1
Perform Functional Test - ARNAV MFD Setup. (Refer to 31-60)
2
Perform Operational Test - ARNAV MFD. (Refer to 31-60)
(f)
If MFD is the same unit as the originally installed MFD:
1
Perform Operational Test - ARNAV MFD. (Refer to 31-60)
(g) Install center bolster trim. (Refer to 25-10)
Operational Test - ARNAV MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
(b) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(c)
Set GNS power in GPS 1 position to ON position.
(d) On MFD, before approving the Database page, press [MAPPING] to display Map page.
(e) Verify values match the following:
(f)
(g)
(h)
GROUNDSPEED
150 knots
BEARING TO WAYPOINT
135°
ACTIVE WAYPOINT
“GARMIN”
DISTANCE TO GO
10.0 nautical miles
TIME TO GO
4 minutes
PRESENT POSITION
N39°04.05’, W94°53.86
Set GNS power in GPS 1 position to OFF position.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
EFFECTIVITY:
Serials 22-0002 thru 22-0141 w/ ARNAV MFD
31-60
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CIRRUS
(4)
AIRPLANE MAINTENANCE MANUAL
Functional Test - ARNAV MFD Setup
Note:
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
(k)
(l)
(m)
(n)
(o)
(p)
(q)
(r)
(s)
(t)
(u)
MFD configuration values provided in this test are typical, but may not correlate
with all airplanes. Use the appropriate RS232 designation for avionics equipment
as it is configured on the airplane.
Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
On MFD, press RH top button to enter Software Main page.
Press [Checklist].
Press [End Program].
At [LEFT] and [RIGHT] arrows, press [LEFT] arrow to highlight “End”, then press [Sel].
Press [Setup/User Graphics].
With “no Demo” highlighted, press [Sel].
At [LEFT] and [RIGHT] arrows, press [LEFT] arrow to highlight "Yes", then press [Sel].
Press [System Configuration].
Press [Ack] repeatedly to move cursor to “Stormscope” selection.
Press [Next] to highlight “1 for Stormscope ON”, then press [Sel].
At [LEFT] and [RIGHT] arrows, press [LEFT] arrow to highlight "Yes", then press [Sel].
Press [End].
Press [Diagnostics].
Press [Stormscope].
Press [Heading Stabilization].
At [LEFT] and [RIGHT] arrows, press [LEFT] arrow to highlight “Enable”, then press [Sel].
Press [Reset Antenna Configuration].
At [LEFT] and [RIGHT] arrows, press [LEFT] arrow to highlight “Top”, then press [Sel].
Press [Configuration/Heading].
CAUTION:
(v)
(w)
(x)
(y)
31-60
Page 14
15 Jun 2010
MODELS SR22 AND SR22T
If values do not match those below, call Cirrus Design Customer Service.
Verify values and jumper setting match the following:
HDG: XYZ: J3 - 1
Jumper
J2 - 2
Open
HDG VALID FLAG
No Fla
FLAG SENSE
+ vld
J3 - 4
Jumper
HDG VALUE
###
INHIBIT LINE
Off
ANTENNA MOUNT
Top
J3 - 3
Jumper
(Value should match HSI reading)
Press RH top button.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
EFFECTIVITY:
Serials 22-0002 thru 22-0141 w/ ARNAV MFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
INSTRUMENT PANEL
(REF)
3
1
2
LEGEND
1. MFD
2. Captive Screw
3. Connector
Serials 22-0002 thru 22-0141.
SR22_MM31_2929
Figure 31-603
MFD Installation - Serials 22-0002 thru 22-0141 w/ ARNAV MFD
EFFECTIVITY:
Serials 22-0002 thru 22-0141 w/ ARNAV MFD
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
B. Multi-Function Display (MFD) - Serials 22-0142 & subs w/ Avidyne MFD (See Figure 31-604)
(1)
Removal - Avidyne MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Pull MFD circuit breaker.
(c)
Remove center bolster trim. (Refer to 25-10)
(d) Rotate captive screws counter-clockwise to loosen MFD from instrument panel.
CAUTION:
(2)
(3)
(e) Pull MFD from instrument panel just sufficiently to expose cable connector.
(f)
Loosen cable plug retaining screws, then remove from receptacle.
(g) Remove MFD from airplane.
Installation - Avidyne MFD
(a) Position MFD close enough to instrument panel cutout to connect cable plug to receptacle
without straining wire harness.
(b) Slide MFD forward into instrument panel cutout until captive screws align with instrument
panel mounting holes.
(c)
Rotate captive screws clockwise until detent position is felt, indicating screw is aligned
with receptacle. Continue clockwise rotation approximately 1/4 rotation until screw is
secure.
(d) Reset MFD circuit breaker.
(e) If MFD is a different unit from the originally installed MFD:
1
Perform Functional Test - Avidyne MFD Setup. (Refer to 31-60)
2
Perform Operational Test - Avidyne MFD. (Refer to 31-60)
(f)
If MFD is the same unit as the originally installed MFD:
1
Perform Operational Test - Avidyne MFD. (Refer to 31-60)
(g) Install center bolster trim. (Refer to 25-10)
Operational Test - Avidyne MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
(b) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(c)
Set GNS power in GPS 1 position to ON position.
(d) On MFD, before approving the Database page, press [MAPPING] to display Map page.
(e) Verify values match the following:
(f)
(g)
(h)
31-60
Page 16
15 Jun 2010
When removing MFD, do not strain wire harness by pulling cable too far
from instrument panel.
GROUNDSPEED
150 knots
BEARING TO WAYPOINT
135°
ACTIVE WAYPOINT
“GARMIN”
DISTANCE TO GO
10.0 nautical miles
TIME TO GO
4 minutes
PRESENT POSITION
N39°04.05’, W94°53.86
Set GNS power in GPS 1 position to OFF position.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
CIRRUS
(4)
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
Functional Test - Avidyne MFD Setup - Serials w/ MFD Software P/Ns 530-00162-000 Rev 03 or
lower
Note:
(a)
(b)
(c)
(d)
(e)
MFD configuration values provided in this test are typical, but may not correlate
with all airplanes. Use the appropriate RS232 designation for avionics equipment
as it is configured on the airplane.
Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
On MFD, when PRESS ANY BEZEL KEY TO CONTINUE is displayed, press any key.
If Engine Monitoring is selected, press [Fuel Done] to enter Map page.
Rotate left knob to select Setup page.
Note:
(f)
(g)
(h)
(i)
(j)
(k)
The five line select keys on the LH side of the MFD are L1 through L5, with
L1 in the uppermost position. The five line select keys on the RH side of the
MFD are R1 through R5, with R1 in the uppermost position.
Press and hold [L1] and [L3] until Maintenance page is displayed.
Press [GPS Setup].
For EX3000C:
1
Set RECEIVER to "King/Aviation Format".
2
Set PORT to "RS232 1".
3
Set BAUD to "9600".
4
Press [Save].
For EX5000C:
1
Set RECEIVER A to "GAMA 429 Format".
2
Set PORT to "ARINC429 1-GPS A Default".
3
Set SPEED to "Low".
4
Set RECEIVER B to "GAMA 429 Format".
5
Set PORT to "ARINC429 2-GPS".
6
Set SPEED to "Low".
7
Press [Save].
Press [Traffic Setup].
1
Serials w/o SkyWatch: Set SENSOR to "Not Installed".
2
Serials w/ SkyWatch: Set SENSOR to "TAS".
3
Serials w/ SkyWatch: Set PORT to "ARINC429 3-Traffic Default".
4
Serials w/ SkyWatch: Set TAS TYPE to "SkyWatch".
5
Serials w/ SkyWatch: Deselect check box for EXTERNAL CONTROLLER.
6
Press [Save].
Press [Lightning Setup].
1
Serials w/o Stormscope: Set SENSOR to "Not Installed".
2
Serials w/ Stormscope: Set SENSOR to "WX-500".
3
Serials w/ Stormscope: Set OPERATING MODE to "Weather".
4
Serials 22-0002 thru 22-1086 w/ Stormscope: Set PORT to "RS232 1-Lightning
Default".
5
Serials 22-1087 thru 22-1601, 22-1603 thru 22-1643, 22-1645 thru 22-1662 w/
Stormscope: Set PORT to "RS232 3-Lightning Default".
6
Serials w/ Stormscope & w/o PFD: Set STAB TYPE to "Synchro".
7
Serials w/ Stormscope & w/ PFD: Set STAB TYPE to "Use Map Heading/Track".
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
31-60
Page 17
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
8
(l)
Serials w/ Stormscope: Select check box for ENABLE LIGHTNING AHEAD WARNING?.
9
Serials w/ Stormscope: Select check box for ANTENNA ON TOP?.
10
Press [Save].
Press [Engine Setup].
1
Serials w/o EMax Engine Monitoring: Set SENSOR TYPE to "Not Installed".
2
Serials w/ EMax Engine Monitoring: Set SENSOR TYPE to "Avidyne SIU".
3
Serials w/ EMax Engine Monitoring: Set PORT to "RS232 2".
4
Serials w/ EMax Engine Monitoring: Set AIRCRAFT MODEL to "SR22".
Note:
(m)
(n)
(o)
(p)
(q)
(r)
31-60
Page 18
15 Jun 2010
The data box at the bottom of the Engine Setup page shows you the
configuration of the SIU. If page settings do not match with the DIP
switch settings of the SIU, a yellow annunciator indicates to recheck
configuration of this page and/or the DIP switches on the SIU.
5
Serials w/ EMax Engine Monitoring: Set ELECTRICAL to appropriate setting.
6
Press [Save].
Press [TAWS Setup].
1
Serials w/o TAWS: Set SENSOR to "Not Installed".
2
Serials w/ TAWS: Set SENSOR to "Honeywell EGPWS".
3
Serials w/ TAWS: Set ARINC 429 PORT to "ARINC 429 4-TAWS Default".
4
Serials w/ TAWS: Set ARINC 453 PORT to "ARINC 453 2-TAWS Default".
5
Serials w/ TAWS: Select check box for ALTITUDE ANNUNCIATION ON.
6
Press [Save].
For EX3000C, press [Map Heading].
1
Set MAP HEADING to "None (Use GPS Track)".
2
Press [Save].
For EX5000C, press [Map Heading].
1
Serials w/ PFD or Sandel: Set MAP HEADING to "FMS/GPS".
2
Serials w/ Stormscope & w/o PFD or Sandel: Set MAP HEADING to "Stormscope".
3
Serials w/ SkyWatch & w/o PFD, Sandel, or Stormscope: Set MAP HEADING to
"Skywatch".
4
Serials w/o PFD, Sandel, Stormscope, or SkyWatch: Set MAP HEADING to "None".
5
Press [Save].
Press [Aircraft Setup].
1
Set CHECKLIST to appropriate configuration.
2
Set BRIGHTEST DIMMING VOLTAGE to "24.0" volts.
3
Set DARKEST DIMMING VOLTAGE to "5.0" volts.
4
Serials w/o XM Weather: Set BROADCAST to "Not Installed".
5
Serials w/ XM Weather: Set BROADCAST to "XM Radio".
6
Serials w/ XM Weather: Set PORT to "RS232 4-Broadcast Default".
7
Press [Save].
Press [Restart System].
1
When PRESS ANY BEZEL KEY TO CONTINUE is displayed, press any key.
2
If Engine Monitoring is selected, press [Fuel Done] to enter Map page.
3
Rotate left knob to select Setup page.
Press [System Time].
1
Set Time Source to "GPS".
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
CIRRUS
(s)
(t)
AIRPLANE MAINTENANCE MANUAL
2
Set Time Zone to present time zone offset for UTC.
3
Set Menu Timeout to "Never".
4
Press [Save].
Press [Back To Setup].
For EX3000C, rotate left knob to select Map page.
Note:
(u)
If no GPS signal is acquired, TRK will not be displayed on MFD.
1
Verify MFD TRK value matches GPS 1 TRK value displayed on 4th Nav page.
2
Verify that no error messages display.
For EX5000C, rotate left knob to select Map page.
Note:
(v)
MODELS SR22 AND SR22T
If no GPS signal is acquired, HDG will not be displayed on MFD.
1
Verify HDG value matches PFD heading.
2
Verify that no error messages display.
Serials w/ EMax Engine Monitoring: Perform test for OAT sensor and MFD accuracy.
1
Acquire necessary tools, equipment, and supplies.
Description
Calibrated Thermometer
P/N or Spec.
-
Supplier
Any Source
Purpose
Measure temperature
at OAT sensor.
2
(w)
Use thermometer to measure temperature approximately 4 inches from OAT sensor
located on fuselage forward of RH door.
3
Verify OAT reading on MFD matches thermometer reading ±2°C.
Serials w/ SkyWatch: Perform test for SkyWatch installation.
1
Confirm selected ranges:
2
3
MFD
5NM
GNC 420
or
GNS 430
10NM
On MFD, rotate left knob to select Setup page.
Press [Traffic Self Test].
During test, "Traffic 9 o'clock/2.0NM/-200FT" should be displayed at bottom of MFD.
When test is complete, "Traffic advisory system test-passed" should be heard over
the headset and speaker.
(x)
Serials w/ Stormscope: Perform test for Stormscope installation.
1
Confirm selected ranges:
MFD
30NM
SANDEL
30NM
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
31-60
Page 19
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
GNC 420
or
GNS 430
2
3
MODELS SR22 AND SR22T
35NM
On MFD, rotate left knob to select Setup page.
Press [Lightning Self Test].
For Avidyne MFD, a strike should be displayed every 2-3 seconds, in the 2 o'clock
position-relative to aircraft heading.
For PFD, heading must be available with ADAHRS operational.
For Sandel, STST should flash on the display indicating Stormscope is in test mode.
For GNS 430 on 2nd Nav page, strikes should be displayed in the 2 o'clock positionrelative to aircraft heading.
4
(5)
When test is complete, verify LIGHTNING SENSOR IS OPERATING NORMALLY is
displayed at bottom of MFD display.
(y)
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(z)
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
Functional Test - Avidyne MFD Setup - Serials w/ MFD Software P/Ns 530-00180-000 Rev 00 &
subs
Note:
(a)
(b)
(c)
(d)
(e)
MFD configuration values provided in this test are typical, but may not correlate
with all airplanes. Use the appropriate RS232 designation for avionics equipment
as it is configured on the airplane.
Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
On MFD, when PRESS ANY BEZEL KEY TO CONTINUE is displayed, press any key.
If Engine Monitoring is selected, press [Fuel Done] to enter Map page.
Rotate left knob to select AUX page.
Note:
(f)
(g)
(h)
31-60
Page 20
15 Jun 2010
The five line select keys on the LH side of the MFD are L1 through L5, with
L1 in the uppermost position. The five line select keys on the RH side of the
MFD are R1 through R5, with R1 in the uppermost position.
Press and hold [L1] and [L3] until Maintenance page is displayed.
Press [GPS Setup].
1
Set RECEIVER 1 to "GAMA 429 Format".
2
Set PORT to "ARINC429 1".
3
Set SPEED to "Low".
4
Set RECEIVER 2 to "GAMA 429 Format".
5
Set PORT to "ARINC429 2".
6
Set SPEED to "Low".
7
Press [Save].
Press [Traffic Setup].
1
Serials w/o SkyWatch: Set SENSOR to “Not Installed”.
2
Serials w/ SkyWatch: Set SENSOR to “TAS”.
3
Serials w/ SkyWatch: Set PORT to “ARINC429 3".
4
Serials w/ SkyWatch: Set TAS TYPE to “Skywatch”.
5
Serials w/ SkyWatch: Deselect check box for EXTERNAL CONTROLLER.
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
CIRRUS
(i)
(j)
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
6
Press [Save].
Press [Lightning Setup].
1
Serials w/o Stormscope: Set SENSOR to "Not Installed".
2
Serials w/ Stormscope: Set SENSOR to "WX-500".
3
Serials w/ Stormscope: Set OPERATING MODE to "Weather".
4
Serials w/ Stormscope: Set PORT to "RS232 3".
5
Serials w/ Stormscope: Set STAB TYPE to "Use Map Heading/Track".
6
Serials w/ Stormscope: Select check box for ENABLE LIGHTNING AHEAD WARNING?.
7
Serials w/ Stormscope: Select check box for ANTENNA ON TOP?.
8
Press [Save].
Press [Engine Setup].
1
Set SENSOR TYPE to "Avidyne DAU".
2
Set PORT to "RS232 2".
3
Set AIRCRAFT MODEL to "SR22".
Note:
The data box at the bottom of the Engine Setup page shows the configuration of the DAU. If page settings do not match with the configuration jumper setting of the DAU, a yellow annunciator indicates to
recheck configuration of this page and/or the configuration jumper
setting of the DAU.
4
5
6
(k)
(l)
(m)
Serials 22-0002 thru 22-2437: Select FUEL TANK SIZE to "SR22 (81 gal fuel)”.
Serials 22-2438 & subs: Select FUEL TANK SIZE to "SR22 (92 gal fuel)”.
Serials 22-0002 thru 22-2437 w/ MFD Software P/Ns 530-00195-100 Rev 00 &
subs: Set FUEL TO TABS to "47".
7
Serials 22-2438 & subs w/ MFD Software P/Ns 530-00195-100 Rev 00 & subs: Set
FUEL TO TABS to "60".
8
Press [Save].
Press [TAWS Setup].
1
Serials w/o TAWS: Set SENSOR to "Not Installed".
2
Serials w/ TAWS: Set SENSOR to "Honeywell EGPWS".
3
Serials w/ TAWS: Set ARINC 429 PORT to "ARINC 429 4".
4
Serials w/ TAWS: Set ARINC 453 PORT to "ARINC 453 2".
5
Serials w/ TAWS: Select check box for ALTITUDE ANNUNCIATION ON.
6
Press [Save].
Press [Map Heading].
1
Set MAP HEADING to "FMS/GPS".
2
Press [Save].
Press [Aircraft Setup].
1
Set CHECKLIST to appropriate configuration.
2
Serials w/o XM Weather: Set BROADCAST to "Not Installed".
3
Serials w/ XM Weather: Set BROADCAST to "XM Radio".
4
Serials w/ XM Weather: Set PORT to "RS232 4".
5
Set AUX DATA to "Entegra PFD".
6
Set PORT to "RS232 1".
7
Set BRIGHTEST DIMMING VOLTAGE to "24.0" volts.
8
Set DARKEST DIMMING VOLTAGE to "5.0" volts.
9
Press [Save].
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
31-60
Page 21
01 Jan 2012
CIRRUS
(n)
31-60
Page 22
15 Jun 2010
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
Press [Restart System].
1
When PRESS ANY BEZEL KEY TO CONTINUE is displayed, press any key.
2
If Engine Monitoring is selected, press [Fuel Done] to enter Map page.
3
Rotate left knob to select AUX page.
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
CIRRUS
(o)
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
Press [Data Blocks].
1
Set parameters for the Data Blocks Setup page.
TO WPT
DEST WPT
GND SPD
NRST ARPT
FUEL
NRST ARPT
FUEL RMNG
UTC
LEAN
LOCAL TIME
%PWR/EGT/CHT
(p)
(q)
(r)
2
Press [Save].
Press [System Time].
1
Airplanes w/ MFD software 530-00180-() Rev 02 or lower: Set Time Source to
"GPS".
2
Airplanes w/ MFD software 530-00180-() Rev 03 or higher: Set Time Source to
"Auto".
3
Set Time Zone to present time zone offset for UTC.
4
Set Menu Time-out to "Never".
5
Press [Save].
Press [Back To Setup].
Rotate left knob to select Map page.
Note:
(s)
If no GPS signal is acquired, HDG will not be displayed on MFD.
1
Verify HDG value matches PFD heading.
2
Verify that no error messages display.
Serials w/ SkyWatch: Perform test for SkyWatch installation.
1
Confirm selected ranges:
2
3
MFD
5NM
GNC 420
or
GNS 430
10NM
On MFD, rotate left knob to select AUX page.
Press [Traffic Self Test].
During test, "Traffic 9 o'clock/2.0NM/-200FT" should be displayed at bottom of MFD.
When test is complete, "Traffic advisory system test-passed" should be heard over
the headset and speaker.
(t)
Serials w/ Stormscope: Perform test for Stormscope installation.
1
Confirm selected ranges:
MFD
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
30NM
31-60
Page 23
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
GNC 420
or
GNS 430
2
3
MODELS SR22 AND SR22T
35NM
On MFD, rotate left knob to select AUX page.
Press [Lightning Strk Test].
For Avidyne MFD, a strike should be displayed every 2-3 seconds, in the 2 o'clock
position-relative to aircraft heading.
For PFD, heading must be available with ADAHRS operational.
For GNS 430 on 2nd Nav page, strikes should be displayed in the 2 o'clock positionrelative to aircraft heading.
4
(u)
(v)
31-60
Page 24
15 Jun 2010
When test is complete, verify LIGHTNING SENSOR IS OPERATING NORMALLY is
displayed at bottom of MFD display.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
INSTRUMENT PANEL
(REF)
2
3
1
LEGEND
1. MFD
2. Captive Screw
3. Connector
SR22_MM31_1995A
Figure 31-604
MFD Installation - Serials 22-0142 & subs w/ Avidyne MFD
EFFECTIVITY:
Serials 22-0142 & subs w/ Avidyne MFD
31-60
Page 25
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
C. Multi-Function Display (MFD) - Serials w/ Perspective MFD (See Figure 31-605)
(1)
Removal - Perspective MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Pull MFD #1 and MFD #2 circuit breakers.
(c)
Rotate captive screws counter-clockwise to loosen MFD from instrument panel.
CAUTION:
(2)
(3)
(d) Pull MFD from instrument panel just sufficiently to expose cable connector.
(e) Disconnect connector from MFD.
(f)
Remove MFD from airplane.
Installation - Perspective MFD
(a) Position MFD close enough to instrument panel to connect connector without straining
wire harness.
(b) Slide MFD forward into instrument panel until captive screws align with instrument panel
mounting holes.
(c)
Rotate captive screws clockwise until detent position is felt, indicating screw is aligned
with receptacle. Continue clockwise rotation approximately 1/4 rotation until screw is
secure.
(d) Reset MFD #1 and MFD #2 circuit breakers.
(e) If MFD has been repaired or is a new or different unit from originally installed unit:
1
Perform Functional Test - Perspective MFD Software Loading. (Refer to 31-60)
2
Perform Functional Test - Perspective MFD Configuration Loading. (Refer to 31-60)
(f)
Perform Operational Test - Perspective MFD. (Refer to 31-60)
Operational Test - Perspective MFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
(b) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(c)
Allow PFD and MFD to initialize for approximately one minute.
Note:
(d)
(e)
(f)
In normal operating mode, a large red X through a data field indicates the
data field is invalid. Valid data fields will not display a red X.
At top corners of PFD and MFD, verify all NAV and COM fields are valid.
On PFD, verify altitude, airspeed, vertical speed, TAS, and OAT fields are valid.
Verify engine instrument fields are valid and read as follows:
1
Percent Power should read zero.
2
RPM should read zero.
3
Manifold Pressure should read the current barometric pressure ±0.5 inHg.
4
Fuel Used should read zero.
5
Fuel Flow should read zero.
6
Oil Temperature should read ambient.
7
Oil Pressure should read 0±2 PSI.
8
BAT1 Current should read between 0 and 10 amps.
Note:
9
31-60
Page 26
01 Jan 2016
When removing MFD, do not strain wire harness by pulling cable too far
from instrument panel.
Turn on large electrical loads (landing light, navigation lights, pitot
heat, etc.) to ensure more amps are drawn when larger electrical
loads are introduced.
Essential Bus Voltage should read 26±2 VDC.
EFFECTIVITY:
Serials w/ Perspective MFD
CIRRUS
(4)
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
10
Main Bus 1 Voltage should read 26±2 VDC.
11
Main Bus 2 Voltage should read 26±2 VDC.
12
CHT should read bottom of scale (All six CHTs).
13
EGT should read bottom of scale (All six EGTs).
14
ALT1 should read 0 amps.
15
ALT2 should read 0 amps.
(g) Press reversionary switch and verify both the PFD and MFD enter reversion mode. Both
displays should have valid altitude, airspeed, vertical speed, and engine instrument fields.
(h) Press reversionary switch again and verify both the PFD and MFD switch back to normal
display mode.
(i)
Verify that no MANIFEST or CONFIGURATION alert messages appear in the lower right
corner of the PFD (press the flashing ALERTS softkey to view alert messages). If any
MANIFEST errors appear, the correct software to the related LRU must be loaded before
proceeding. (Refer to 31-60)
(j)
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(k)
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
Functional Test - Perspective MFD Software Loading
Note:
If displays are reinstalled in original positions, no software or configuration loading
is required. This does not include units returned for repair as the software and
configuration files are deleted during the repair testing process.
If PFD and MFD are installed in opposite locations, no software or configuration
loading is required. Some button/knob functions may not work correctly until displays are reinstalled in original locations. Return displays to original locations after
troubleshooting.
If a new, repaired, or exchanged MFD is installed, load software and configuration
files from the Cirrus Perspective software loader card. Retain Supplemental Database and other SD cards from original display to reinstall in new display after loading software.
(a)
(b)
Connect 28 ±1 VDC external power to external power receptacle.
Pull STARTER and FUEL PUMP circuit breakers.
CAUTION:
Failure to remove database cards may result in cards becoming corrupted.
(c)
(d)
(e)
(5)
Remove SD cards from top and bottom slots of MFD and PFD.
Insert Cirrus Perspective software loader card into top slot of MFD.
Power on PFD and MFD in Configuration mode.
1
While holding far right softkey on PFD and MFD, set BAT 1 and AVIONICS switches
to ON positions.
2
When “INITIALIZING SYSTEM” appears in upper left corner of displays, release
softkeys.
(f)
Press [YES] softkey at “DO YOU WANT TO UPDATE SYSTEM FILES?” prompt.
(g) After software has finished loading, press any key to confirm update completion.
(h) Press [YES] softkey at “DO YOU WANT TO UPDATE SPLASH SCREEN?” prompt.
(i)
After splash screen has finished loading, press any key to confirm update completion.
(j)
Perform Adjustment/Test - Perspective MFD Configuration Loading. (Refer to 31-60)
Functional Test - Perspective MFD Configuration Loading
(a) Connect 28 ±1 VDC external power to external power receptacle.
EFFECTIVITY:
Serials w/ Perspective MFD
31-60
Page 27
15 Jun 2010
CIRRUS
(b)
AIRPLANE MAINTENANCE MANUAL
Pull STARTER and FUEL PUMP circuit breakers.
CAUTION:
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(k)
(l)
(m)
(n)
(p)
(q)
31-60
Page 28
15 Jun 2010
Pressing [ENT] key will check and uncheck highlighted software and
configuration boxes.
Load the following configuration files:
1
Press [CLR ALL] softkey at bottom of display.
2
Using [FMS] knob and [ENT] key, select MFD Configuration box.
3
Press [LOAD] softkey.
4
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE
window.
Once files are selected, press [LOAD] softkey.
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE window.
Move curser to AIRFRAME window, rotate inner [FMS] knob to display list of AIRFRAME
choices, highlight “Options” in pop-up window, and press [ENT] key.
In FILE box, rotate inner [FMS] knob to display list of FILE choices. Load appropriate files
based on aircraft optional equipment.
• GFC700 w/YD - MFD Configuration file
•
(o)
Failure to remove database cards may result in cards becoming corrupted.
Remove SD cards from top and bottom slots of MFD and PFD.
Insert Cirrus Perspective software loader card into top slot of PFD.
Power on PFD and MFD in Configuration mode.
1
While holding far right softkey on PFD and MFD, set BAT 1 and AVIONICS switches
to ON positions.
2
When “INITIALIZING SYSTEM” appears in upper left corner of displays, release
softkeys.
3
On PFD, press [NO] softkey at “DO YOU WANT TO UPDATE SYSTEM FILES?”
prompt.
4
On PFD, press [NO] softkey at “DO YOU WANT TO UPDATE SYSTEM SPLASH
SCREEN?”
After System Status page appears on PFD, use inner [FMS] knob to select System Upload
page.
Press inner [FMS] knob to activate cursor.
Rotate inner [FMS] knob to display list of AIRFRAME choices, highlight appropriate airframe model in pop-up window, then press [ENT] key.
In FILE box, rotate inner [FMS] knob to display list of FILE choices, highlight appropriate
airframe configuration file in the pop-up window, and press [ENT] key.
Note:
(j)
MODELS SR22 AND SR22T
GFC700 w/o YD - MFD Configuration file
Move curser to AIRFRAME window, rotate inner [FMS] knob to display list of AIRFRAME
choices, highlight “AHRS ADC Options” in pop-up window, and press [ENT] key.
In FILE box, rotate inner [FMS] knob to display list of FILE choices, highlight File that
matches number of AHRS and ADC units installed on aircraft, and press [ENT] key.
1
Press [CLR ALL] softkey.
2
Using [FMS] knob and [ENT] key, select MFD Configuration box.
3
Press [LOAD] softkey.
4
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE
window.
Pull PFD#1, PFD#2, MFD#1, MFD#2 circuit breakers.
EFFECTIVITY:
Serials w/ Perspective MFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
Note:
(r)
Restarting in normal mode sets the System ID and is required before inserting the supplemental database cards.
Power on PFD and MFD in normal mode and allow to initialize.
Set BAT 1 and AVIONICS switches to OFF positions.
CAUTION:
(u)
(v)
(w)
(x)
Whenever AIRFRAME file is loaded from main aircraft configuration file,
additional features such as TAWS, Synthetic Vision, and Jeppesen ChartView must be unlocked.
If TAWS, Synthetic Vision, and/or ChartView option is installed, unlock system option.
1
Insert unlock card in top slot of PFD.
2
While holding far right softkey on PFD and MFD, reset PFD and MFD circuit breakers.
3
When “INITIALIZING SYSTEM” appears in upper left corner of displays, release
softkeys.
4
After System Status page appears on PFD, rotate inner [FMS] knob to select System Upload page.
5
Activate the cursor, rotate inner [FMS] knob to display list of AIRFRAME choices,
highlight “Unlock File” in pop-up window, and press [ENT] key.
6
In FILE box, rotate inner [FMS] knob to display list of FILE choices, highlight “Unlock
File” in pop-up window, and press [ENT] key.
7
Press [LOAD] softkey.
8
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE
window.
9
Pull PFD#1, PFD#2, MFD#1, MFD#2 circuit breakers.
10
Repeat for additional unlock cards.
Note:
(s)
(t)
MODELS SR22 AND SR22T
Wait for “flash” of display screens or 5 seconds to ensure backup capacitors
have discharged before removing software loader card.
Remove Cirrus Perspective software loader card from PFD.
Insert SD cards into top and bottom slots of MFD and PFD.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Disconnect 28 ±1 VDC external power from external power receptacle.
EFFECTIVITY:
Serials w/ Perspective MFD
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
INSTRUMENT PANEL
(REF)
INSTRUMENT PANEL
(REF)
3
2
1
LEGEND
1. MFD
2. Captive Screw
3. Connector
SR22_MM31_2816
Figure 31-605
MFD Installation - Serials w/ Perspective Avionics 12-Inch MFD (Sheet 1 of 2)
31-60
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15 Jun 2010
EFFECTIVITY:
Serials w/ Perspective Avionics 12-Inch MFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
INSTRUMENT PANEL
(REF)
3
2
1
LEGEND
1. MFD
2. Captive Screw
3. Connector
SR22_MM31_3024
Figure 31-605
MFD Installation - Serials w/ Perspective Avionics 10-Inch MFD (Sheet 2 of 2)
EFFECTIVITY:
Serials w/ Perspective Avionics 10-Inch MFD
31-60
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15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
D. Primary Flight Display (PFD) - Serials w/ Avidyne PFD (See Figure 31-606)
CAUTION:
(1)
Pitot and Static System Leak Tests must be performed every time a static or pitot line is
disconnected from the Primary Flight Display (PFD). If the PFD unit is replaced, the new
PFD must be recalibrated. The Pitot and Static connections are marked by using color
coding. The Pitot connector on the PFD is color coded red.
Removal - Avidyne PFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
Note:
(b)
(c)
To assist in PFD removal, remove MFD or glareshield.
Remove MFD. (Refer to 31-60)
Remove screws securing PFD to instrument panel.
CAUTION:
When removing PFD, do not strain wire harnesses, pitot lines, or static lines
by pulling them too far from instrument panel. Note color of static and pitot
lines for reassembly. The Pitot connector on the PFD is color coded red.
(d)
(2)
Partially slide PFD out of instrument panel, then disconnect static line, pitot line, and electrical connectors.
(e) Cap off static and pitot lines, then remove PFD.
(f)
Cap off static and pitot fittings on PFD.
Installation - Avidyne PFD
CAUTION:
(a)
The Pitot connector on the PFD is color coded red. If pitot line and static lines are
not properly connected, instrument damage may occur.
Remove caps from static line, pitot line, static fitting on PFD, and pitot fitting on PFD.
CAUTION:
Do not angle PFD downward when installing PFD into instrument panel to
avoid impacting the GPSS Interconnect Relay. The GPSS Interconnect
Relay is mounted below PFD and could become disconnected from its
socket.
(b)
(3)
31-60
Page 32
15 Jun 2010
Partially slide PFD into instrument panel, then connect static line, pitot line, and electrical
connectors to corresponding fittings.
(c)
Install screws securing PFD to instrument panel. Torque screws to 30.0 ± 3.0 in-lb (3.4 ±
0.34 Nm).
(d) Perform Functional Test - Pitot System Plumbing. (Refer to 34-10)
(e) Perform Functional Test - Static System Plumbing. (Refer to 34-10)
(f)
Install MFD. (Refer to 31-60)
(g) If PFD is a different unit from the originally installed PFD:
1
Perform Functional Test - Avidyne PFD Setup. (Refer to 31-60)
2
Perform Functional Test - Magnetometer Calibration. (Refer to 34-20)
3
Airplanes w/ PFD software 530-00159-000 Rev 01 or lower: Perform Functional Test
- IRU Calibration. (Refer to 31-60)
(h) Perform Functional Test - Altitude Encoder Calibration. (Refer to 34-10)
(i)
Perform Functional Test - Flight Guidance Programmer/Computer. (Refer to 22-11)
Functional Test - Avidyne PFD Setup
(a) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(b) Connect 28 ±1 VDC external power to external power receptacle.
EFFECTIVITY:
Serials w/ Avidyne PFD
CIRRUS
(c)
(d)
(e)
(f)
(g)
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
Pull HSI/PFD#1 circuit breaker, verify PFD remains on, then reset HSI/PFD#1 circuit
breaker.
Pull HSI/PFD#2 circuit breaker, then verify PFD remains on.
Pull HSI/PFD#1 circuit breaker, then verify PFD shuts off.
Reset HSI/PFD#1 and HSI/PFD#2 circuit breakers.
Serials w/ PFD Software P/N 530-00159-000 Rev 02 or lower: The system will begin its
normal start up procedure and INITIAL AHRS ALIGNMENT-REMAIN STATIONARY-OK
TO TAXI will be displayed.
Serials w/ PFD Software P/N 530-00177-000 Rev 00 or higher: The system will begin its
normal start up procedure. A series of "AHRS ALIGNMENT" messages followed by
"AHRS WARMING UP - OK TO TAXI" will be displayed.
(h)
Simultaneously, press and hold [L1] and [L3] keys until countdown timer in lower left corner of display indicates zero.
Note:
(i)
Serials w/ PFD Software P/N 530-00159-000 Rev 02 or lower: At end of displayed countdown, the System Setup page will appear.
Note:
(j)
(k)
(m)
(n)
Verify no faults are indicated on System Setup page at top portion of display.
Serials w/ PFD Software P/N 530-00177-000 Rev 00 or higher: At end of displayed countdown, the System page will appear.
Verify that AIRCRAFT MAKE indicates "Cirrus".
Note:
(l)
The four line select keys on the LH side of the PFD are L1 through L4, with
L1 in the uppermost position. The four line select keys on the RH side of the
PFD are R1 through R4, with R1 in the uppermost position.
If AIRCRAFT MAKE is incorrect, the wrong configuration may be installed.
Serials w/ PFD Software P/N 530-00183-000 Rev 02 or lower: Press [A/C Model].
1
Serials 22-0002 thru 22-1662 w/ SIU: Select "SR22+".
2
Serials 22-0002 thru 22-1662 w/o SIU, 22-1663 & subs: Select "SR22".
Serials w/ PFD Software P/N 530-00194-000 Rev 00 or higher: Press [A/C Model].
1
Serials 22-0002 thru 22-2437: Select "SR22".
2
Serials 22-2438 & subs: Select "SR22 (W2)".
Serials 22-2438 & subs w/ PFD Software P/N 530-00183-000 Rev 01 or Rev 02: Press
[Configure ASI].
Note:
1
2
3
4
5
6
7
8
EFFECTIVITY:
Serials w/ Avidyne PFD
Press [NEXT SELECTION] to navigate through ASI configuration settings.
Rotate RH knob to change value.
For ASI TYPE, select "Fixed Vne".
For VSO, set value to "62 Knots".
For VS1, set value to "73 Knots".
For VFE, verify value is "104 Knots".
For VNO, verify value is "177 Knots".
For VNE, verify value is "200 Knots".
For VX AT SEA LEVEL, verify value is "78 Knots".
For VY AT SEA LEVEL, verify value is "101 Knots".
31-60
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CIRRUS
(o)
AIRPLANE MAINTENANCE MANUAL
Serials 22-2438 & subs w/ PFD Software P/N 530-00194-000 Rev 00 or higher: Press
[Configure ASI].
Note:
(p)
(q)
(r)
(s)
(t)
(u)
(v)
(w)
(x)
MODELS SR22 AND SR22T
Press [NEXT SELECTION] to navigate through ASI configuration settings.
Rotate RH knob to change value.
1
For VG MIN WEIGHT, select "87 Knots".
2
For VG MAX WEIGHT, set value to "88 Knots".
3
For VX ALTITUDE GRADIENT, set value to "0.4 Knots per 1000 Feet".
4
For VY ALTITUDE GRADIENT, verify value is "-0.5 Knots per 1000 Feet".
Rotate left knob to select Avionics page.
For ENGINE DAU, verify value is "Installed".
Press [Nav1] to select "430/530".
Press [Nav2].
1
In a dual GNS 430(W)/GNC 420(W) setup, select "420".
2
In a dual GNS 430(W) setup, select "430/530".
Press [Perform A/P Cal].
Press [A/P Type].
1
Serials w/ S-TEC FIFTY FIVE SR Autopilot: Select "STEC55SR".
2
Serials w/ S-TEC FIFTY FIVE X Autopilot: Select "STEC55X".
Serials w/ PFD Software P/N 530-00177-000 Rev 00 or higher: For ADF, select "None".
Serials w/ PFD Software P/N 530-00177-000 Rev 00 or higher: Rotate left knob to select
Display page.
1
For A/P ANN., select "HIDE".
2
For V-SPEEDS, select "SHOW".
3
For HORIZ MARKS, select "SHOW".
Serials w/ Flight Director: For TRIM ANN, select “HIDE”.
Note:
For metric countries, select "hPa" for hectopascals or "Mb" for millibars.
(y)
(z)
Press [Baro Unit] to select "inHg" for inches of mercury.
Serials w/ PFD Software P/N 530-00177-000 Rev 00 or higher: Press [ARS].
1
Serials w/o Flight Director: Select "W".
2
Serials w/ Flight Director: Select "DELTA".
(aa) Rotate left knob to advance past Logging page, then select SystemInfo page.
(ab) Verify no faults are listed on the SystemInfo page.
Note:
If any changes have been made to Setup Configuration, you must select
"Back To PFD" for changes to be saved.
(ac) Select "Back To PFD".
CAUTION:
PFD unit must be powered down and then powered up again to effect previous settings.
The new settings may not be displayed if you do not allow a 30 second wait
prior to cycling power.
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15 Jun 2010
(ad) To effect settings, toggle BAT 1 switch to OFF position, then to ON position.
(ae) Serials w/o EMax Engine Monitoring: Perform test for OAT sensor and PFD accuracy.
EFFECTIVITY:
Serials w/ Avidyne PFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
1
MODELS SR22 AND SR22T
Acquire necessary tools, equipment, and supplies.
Description
P/N or Spec.
Calibrated Thermometer
-
Supplier
Any Source
Purpose
Measure temperature
at OAT sensor.
2
(4)
Use thermometer to measure temperature approximately 4 inches from OAT sensor
located on fuselage forward of RH door.
3
Verify OAT reading on PFD matches thermometer reading ±2°C.
(af) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(ag) Disconnect 28 ±1 VDC external power from external power receptacle.
(ah) Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Functional Test - Avidyne IRU Calibration - Airplanes w/ PFD software 530-00159-000 Rev 01 or
lower
Note:
(a)
The following Functional Test must be performed whenever the PFD is replaced
with a different unit.
Acquire necessary tools, equipment, and supplies.
Description
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
P/N or Spec.
Supplier
Purpose
Digital Level, 0.25° Resolution
±0.25° Accuracy Any Source PFD calibration.
Straight Edge
minimum 5.0 ft (1.5 m)
-
Any Source Level platform.
Spacer Blocks
1.0 × 2.0 inches (2.54 × 5.08
cm)
-
Any Source Level platform.
Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
Allow PFD to align for approximately 3 minutes, until Air Data Attitude Heading Reference
System (ADAHRS) countdown timer expires and gyro warm-up box disappears.
Once aligned, allow PFD to remain in aligned state for 10 additional minutes.
Enter the setup mode on the PFD by simultaneously pressing and holding top left, and 3rd
down from top left keys until the countdown timer in the lower left corner of the display indicates zero.
After System Setup page appears, press [Perform IRU Cal] and the IRU Calibration page
will appear.
Open both doors on airplane.
At LH door opening, position digital level on lower composite ledge located below door
seal, pointing fore and aft, to represent pitch axis for pitch attitude. Measure at three positions along ledge and determine the average measurement. (See Figure 31-607)
Follow directions on IRU Calibration page to increase or decrease pitch attitude as
required.
1
To increase pitch, press [Increase Pitch].
2
To decrease pitch, press [Decrease Pitch].
Place spacer blocks on LH and RH door sills so that height of blocks is higher than door
seals.
EFFECTIVITY:
Serials w/ Avidyne PFD
31-60
Page 35
15 Dec 2014
CIRRUS
(k)
(l)
(m)
(n)
(o)
AIRPLANE MAINTENANCE MANUAL
Place a straight edge on top and perpendicular to spacer blocks positioned on door sills,
centered.
Place digital level on top and parallel to straight edge, centered, so it points outboard to
represent roll axis.
Follow directions on IRU Calibration page to increase or decrease roll attitude as required.
1
To increase roll, press [Increase Roll].
2
To decrease roll, press [Decrease Roll].
Press [Calibrate IRU].
Press [Back to PFD].
Note:
(p)
MODELS SR22 AND SR22T
If you are going to perform the Functional Test - Magnetometer Calibration
immediately after this procedure, time can be saved by powering down the
PFD one time, after the Functional Test - Magnetometer Calibration has
been performed.
Perform Functional Test - Magnetometer Calibration. (Refer to 34-20)
CAUTION:
PFD unit must be powered down and then powered up again to retain previous calibration settings.
The calibration may be adversely affected if you do not allow a 10 second
wait prior to cycling power.
(q)
(r)
(s)
(t)
31-60
Page 36
15 Jun 2010
To retain calibration settings, toggle BAT 1 switch to OFF position, then to ON position.
Verify initial countdown timer goes to zero and calibrated PFD screen is displayed.
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
Perform Functional Test - Flight Guidance Programmer/Computer. (Refer to 22-11)
EFFECTIVITY:
Serials w/ Avidyne PFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
P
S
1
2
PFD (REF)
CONSOLE ASSEMBLY
(REF)
FORWARD PFD SUPPORT
(REF)
NOTE
Connect color-coded pitot and static lines to
corresponding color-coded connection on PFD.
LH, INBOARD VIEW
Ensure lower clip on PFD engages forward
PFD support.
LEGEND
1. PFD
2. Captive Screw
SR22_MM31_1627A
Figure 31-606
PFD Installation - Serials w/ Avidyne PFD
EFFECTIVITY:
Serials w/ Avidyne PFD
31-60
Page 37
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
WL 100
DOOR SILL
NOTE
DIGITAL LEVEL
At LH door opening, position digital level along
lower composite ledge located below door seal,
to represent pitch axis for pitch attitude.
Measure at three positions along ledge and
determine the average measurement to be used
as the "Pitch" value on the IRU calibration page.
Position digital level on straight edge so it points
outboard, to represent roll axis for roll attitude and
take measurement to be used as the "Roll" value
on the IRU calibration page.
STRAIGHT EDGE
LEVEL
STRAIGHT EDGE
STRAIGHT EDGE
SPACER BLOCK
SPACER BLOCK
DOOR SEAL
(REF)
DOOR SILL
DOOR SEAL
(REF)
DOOR SILL
SR22_MM31_2026
Figure 31-607
Roll and Pitch Measurements for PFD Calibration - Serials w/ Avidyne PFD
31-60
Page 38
15 Jun 2010
EFFECTIVITY:
Serials w/ Avidyne PFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
E. Primary Flight Display (PFD) - Serials w/ Perspective PFD (See Figure 31-608)
(1)
Removal - Perspective PFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Remove screws securing PFD to instrument panel.
CAUTION:
(2)
When removing PFD, do not strain wire harness by pulling them too far from
instrument panel.
(c)
Partially slide PFD out of instrument panel, then disconnect electrical connector.
(d) Remove PFD from airplane.
Installation - Perspective PFD
Note:
If replacing the PFD with a new, repaired, or exchanged PFD, the new PFD must
be temporarily installed in the MFD location while loading software and configuration files. Failure to do so may cause the system ID residing in the config module
to be deleted. After system files have been installed, the PFD may be installed in
the correct location.
(a)
(3)
If installing a new, repaired, or exchanged PFD, perform the following:
1
Remove MFD. (Refer to 31-60)
2
Partially slide PFD into MFD location of instrument panel, then connect electrical
connector to corresponding fitting.
3
Install screws securing PFD to instrument panel.
4
Perform Functional Test - Perspective PFD Software Loading. (Refer to 31-60)
5
Perform Functional Test - Perspective PFD Configuration Loading. (Refer to 31-60)
6
Remove PFD from MFD location. (Refer to 31-60)
7
Partially slide PFD into PFD location of instrument panel, then connect electrical
connector to corresponding fitting.
8
Install screws securing PFD to instrument panel.
9
Install MFD. (Refer to 31-60)
10
Perform Operational Test - Perspective PFD. (Refer to 31-60)
(b) If installing existing PFD, perform the following:
1
Partially slide PFD into instrument panel, then connect electrical connector to corresponding fitting.
2
Install screws securing PFD to instrument panel.
3
Perform Operational Test - Perspective PFD. (Refer to 31-60)
Operational Test - Perspective PFD
(a) Set BAT 1, BAT 2, and AVIONICS switches to ON positions.
(b) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(c)
Allow PFD and MFD to initialize for approximately one minute.
Note:
(d)
(e)
(f)
(g)
In normal operating mode, a large red X through a data field indicates the
data field is invalid. Valid data fields will not display a red X.
At top corners of PFD and MFD, verify all NAV and COM fields are valid.
On PFD, verify altitude, airspeed, vertical speed, TAS, and OAT fields are valid.
Press reversionary switch and verify both the PFD and MFD enter reversion mode. Both
displays should have valid altitude, airspeed, vertical speed, and engine instrument fields.
Press reversionary switch again and verify both the PFD and MFD switch back to normal
display mode.
EFFECTIVITY:
Serials w/ Perspective PFD
31-60
Page 39
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
(h)
(4)
Verify that no MANIFEST or CONFIGURATION alert messages appear in the lower right
corner of the PFD (press the flashing ALERTS softkey to view alert messages). If any
MANIFEST errors appear, the correct software to the related LRU must be loaded before
proceeding. (Refer to 31-60)
(i)
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
(j)
Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
Adjustment/Test - Perspective PFD Software Loading
Note:
If displays are reinstalled in original positions, no software or configuration loading
is required. This does not include units returned for repair as software and configuration files are deleted during the repair testing process.
If PFD and MFD are installed in opposite locations, no software or configuration
loading is required. Some button/knob functions may not work correctly until displays are reinstalled in original locations. Return displays to original locations after
troubleshooting.
If a new, repaired, or exchanged PFD is installed, load software and configuration
files from the Cirrus Perspective software loader card. Retain Supplemental Database and other SD cards from original display to reinstall in new display after loading software.
(a)
(b)
Connect 28 ±1 VDC external power to external power receptacle.
Pull STARTER and FUEL PUMP circuit breakers.
CAUTION:
Failure to remove database cards may result in cards becoming corrupted.
(c)
(d)
(e)
(5)
Remove SD cards from top and bottom slots of MFD and PFD.
Insert Cirrus Perspective software loader card into top slot of PFD.
Power on PFD and MFD in Configuration mode.
1
While holding far right softkey on PFD and MFD, set BAT 1 and AVIONICS switches
to ON positions.
2
When “INITIALIZING SYSTEM” appears in upper left corner of displays, release
softkeys.
(f)
Press [YES] softkey at “DO YOU WANT TO UPDATE SYSTEM FILES?” prompt.
(g) Press any key to confirm update completion after software has finished loading.
(h) Press [YES] softkey at “DO YOU WANT TO UPDATE SPLASH SCREEN?” prompt.
(i)
Press any key to confirm update completion after splash screen has finished loading.
(j)
Perform Adjustment/Test - Perspective PFD Configuration Loading. (Refer to 31-60)
Adjustment/Test - Perspective PFD Configuration Loading
Note:
(a)
(b)
This Adjustment/Test is a standalone procedure to load the Perspective PFD configuration files. Individuals directed here from the Adjustment/Test - Perspective
PFD software loading procedure will already have the displays in configuration
mode and may skip ahead to the step, “After System Status page appears on
PFD, use inner [FMS] knob to select System Upload page.”
Connect 28 ±1 VDC external power to external power receptacle.
Pull STARTER and FUEL PUMP circuit breakers.
CAUTION:
31-60
Page 40
15 Jun 2010
Failure to remove database cards may result in cards becoming corrupted.
EFFECTIVITY:
Serials w/ Perspective PFD
CIRRUS
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
AIRPLANE MAINTENANCE MANUAL
Remove SD cards from top and bottom slots of MFD and PFD.
Insert Cirrus Perspective software loader card into top slot of PFD.
Power on PFD and MFD in Configuration mode.
1
While holding far right softkey on PFD and MFD, set BAT 1 and AVIONICS switches
to ON positions.
2
When “INITIALIZING SYSTEM” appears in upper left corner of displays, release
softkeys.
3
On PFD, press [NO] softkey at “DO YOU WANT TO UPDATE SYSTEM FILES?”
prompt.
4
On PFD, press [NO] softkey at “DO YOU WANT TO UPDATE SYSTEM SPLASH
SCREEN?”
After System Status page appears on PFD, use inner [FMS] knob to select System Upload
page.
Press inner [FMS] knob to activate cursor.
Rotate inner [FMS] knob to display list of AIRFRAME choices, highlight appropriate airframe model in pop-up window, and press [ENT] key.
In FILE window, rotate inner [FMS] knob to display list of FILE choices, highlight appropriate airframe configuration file in pop-up window, and press [ENT] key.
Load the following configuration files:
1
Press [CLR ALL] softkey.
2
Using [FMS] knob and [ENT] key, select AIRFRAME, SYSTEM, MANIFEST and
PFD Configuration box.
3
Press [LOAD] softkey.
4
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE
window.
Note:
(k)
(l)
(m)
(n)
(o)
(p)
MODELS SR22 AND SR22T
Pressing [ENT] key will check and uncheck highlighted software and
configuration boxes.
Once files are selected, press [LOAD] softkey.
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE window.
Move curser to AIRFRAME window, rotate inner [FMS] knob to display list of AIRFRAME
choices, highlight “Options” in pop-up window, and press [ENT] key.
In FILE box, rotate inner [FMS] knob to display list of FILE choices. Load appropriate Files
based on aircraft optional equipment.
• Skywatch 497 - ALERTS Configuration file
•
Oxygen - AIRFRAME and ALERTS Configuration files
•
De-ice Protection - AIRFRAME and ALERTS Configuration files
•
GFC700 w/YD or GFC700 w/o YD - PFD, ALERTS and MANIFEST Configuration files
•
GDL69/A – AIRFRAME, SYSTEM and MANIFEST Configuration files
•
CO Guardian – ALERTS Configuration file
•
GTX 32/33 - MANIFEST Configuration file
Move curser to AIRFRAME window, rotate inner [FMS] knob to display list of AIRFRAME
choices, highlight “AHRS ADC Options” in pop-up window, and press [ENT] key.
In FILE box, rotate inner [FMS] knob to display list of FILE choices, highlight File that
matches number of AHRS and ADC units installed on aircraft, and press [ENT] key.
1
Press [CLR ALL] softkey at bottom of PFD.
2
Using [FMS] knob and [ENT] key, select PFD Configuration box.
EFFECTIVITY:
Serials w/ Perspective PFD
31-60
Page 41
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
3
4
(q)
Press [LOAD] softkey.
When upload is complete, press [ENT] key to select OK in UPLOAD COMPLETE
window.
Power off MFD and PFD.
Note:
(r)
Whenever AIRFRAME file is loaded from main aircraft configuration file,
additional features such as TAWS, Synthetic Vision, and Jeppesen ChartView must be unlocked.
If TAWS, Synthetic Vision, and/or ChartView option is installed, unlock system option.
1
Insert unlock card in top slot of PFD.
2
Power on MFD and PFD in Config mode.
3
After System Status page appears on PFD, rotate inner [FMS] knob to select System Upload page.
4
Activate the cursor, rotate inner [FMS] knob to display list of Airframe choices, highlight CONFIGURATION FILES in pop-up box, and press [ENT] key.
5
In FILE box, rotate inner [FMS] knob to display list of File choices, highlight ENABLE
in pop-up box, and press [ENT] key.
6
Press [LOAD] softkey.
7
When upload is complete, press [ENT] key to select OK in Upload Complete window.
8
Power off MFD and PFD.
9
Repeat for additional unlock cards.
Note:
(s)
(t)
(u)
Power on MFD and PFD in normal mode and allow to initialize.
Perform Adjustment/Test - Aviation Database Loading. (Refer to 42-20)
Set BAT 1 and AVIONICS switches to OFF positions.
CAUTION:
(v)
(w)
(x)
(y)
31-60
Page 42
15 Jun 2010
Restarting in normal mode sets the System ID and is required before
inserting the Supplemental Database cards.
Wait for “flash” of display screens or 5 seconds to ensure backup capacitors
have discharged before removing software loader card.
Remove Cirrus Perspective software loader card from PFD.
Insert SD cards into top and bottom slots of MFD and PFD.
Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers.
Disconnect 28 ±1 VDC external power from external power receptacle.
EFFECTIVITY:
Serials w/ Perspective PFD
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
INSTRUMENT PANEL
(REF)
3
INSTRUMENT PANEL
(REF)
1
2
LEGEND
1. PFD
2. Captive Screw
3. Connector
SR22_MM31_2818A
Figure 31-608
PFD Installation - Serials w/ Perspective Avionics 12-Inch PFD (Sheet 1 of 2)
EFFECTIVITY:
Serials w/ Perspective Avionics 12-Inch PFD
31-60
Page 43
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
3
INSTRUMENT PANEL
(REF)
2
1
LEGEND
1. PFD
2. Captive Screw
3. Connector
SR22_MM31_3026
Figure 31-608
PFD Installation - Serials w/ Perspective Avionics 10-Inch PFD (Sheet 2 of 2)
31-60
Page 44
15 Jun 2010
EFFECTIVITY:
Serials w/ Perspective Avionics 10-Inch PFD
CIRRUS
F.
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
Reversionary Switch - Serials w/ Perspective Avionics 12-Inch Displays (See Figure 31-609)
(1)
(2)
Removal - Reversionary Switch
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Remove glareshield. (Refer to 25-10)
(c)
Disconnect switch wiring from wire harness.
(d) Remove cable tie securing switch wiring to instrument panel support.
(e) Remove switch from instrument panel.
Installation - Reversionary Switch
(a) Install switch to instrument panel.
(b) Connect switch wiring to wire harness.
(c)
Position switch wiring to instrument panel support and secure with cable tie.
(d) Install glareshield. (Refer to 25-10)
EFFECTIVITY:
Serials w/ Perspective Avionics 12-Inch Displays
31-60
Page 45
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
G. Reversionary Switch - Serials w/ Perspective Avionics 10-Inch Displays (See Figure 31-609)
(1)
(2)
31-60
Page 46
15 Jun 2010
Removal - Reversionary Switch
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Remove glareshield. (Refer to 25-10)
(c)
Disconnect wiring from switch terminals.
(d) Remove nut, washer, and gasket securing switch to instrument panel. Remove switch
from airplane.
Installation - Reversionary Switch
(a) Position switch to instrument panel and secure with gasket, washer, and nut.
(b) Connect wiring to switch terminals.
(c)
Install glareshield. (Refer to 25-10)
EFFECTIVITY:
Serials w/ Perspective Avionics 10-Inch Displays
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
1
5
4
2
3
6
INSTRUMENT PANEL
(REF)
LEGEND
1. Reversionary Switch
2. Cable Tie Anchor
3. Cable Tie
4. Connector
5. Flexible Grommet
6. Screw
SR22_MM31_2709A
Figure 31-609
Reversionary Switch Installation - Serials w/ Perspective Avionics 12-Inch Displays (Sheet 1 of 2)
EFFECTIVITY:
Serials w/ Perspective Avionics 12-Inch Displays
31-60
Page 47
15 Jun 2010
CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODELS SR22 AND SR22T
9
7 8
5
Intentionally Left Blank
4
2
1
3
6
INSTRUMENT PANEL
(REF)
LEGEND
1. Reversionary Switch
2. Cable Tie Anchor
3. Cable Tie
4. Connector
5. Flexible Grommet
6. Screw
7. Gasket
8. Washer
9. Nut
SR22_MM31_3028
Figure 31-609
Reversionary Switch Installation - Serials w/ Perspective Avionics 10-Inch Displays (Sheet 2 of 2)
31-60
Page 48
15 Jun 2010
EFFECTIVITY:
Serials w/ Perspective Avionics 10-Inch Displays
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