UPS Aviation Technologies i-linc MFD Owner's manual

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Road SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA APPROVED
AIRPLANE FLIGHT MANUAL SUPPLEMENT
or
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
for
i-linc™ MFD SYSTEM INSTALLATION
as installed in
_____________________________________
Make and Model Airplane
Registration Number ____________
Serial Number _____________
This document serves as a Airplane Flight Manual Supplement or as a Supplemental
Airplane Flight Manual when the aircraft is equipped with the i-linc MFD. This document
must be carried in the airplane at all times when the i-linc MFD is installed in accordance
with Supplemental Type Certificate No. SA02154AK. The information contained in this
document supplements or supersedes the information made available to the operator by the
manufacturer in the form of clearly stated placards, markings, or manuals as required by
CAR 3.777(b) or in the form of an FAA approved Airplane Flight Manual, only in those
areas listed herein. For limitations, procedures, and performance information not contained
in this document, consult the basic placards, markings, or manuals or the basic FAA
approved Airplane Flight Manual.

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Rd. SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA Approved
Page 2 of 11 Date: February 26, 2003
Revision Log
Rev Date Description EN By
00 - 04/25/02 Initial release, Word 97 SR71 7301 CWH
00 A 06/20/02 Updated for V3.2 software 7340 CWH
01 08/08/02 Updated for V3.3 software 7391 CWH
02 10/21/02 Updated for V4.0 software 7475 JDB
02 A 02/10/03 Updated for V4.1 software 7571 RDG
TABLE OF CONTENTS
1. GENERAL ......................................................................................................................... 3
1.1 I-LINC MULTI-FUNCTIONAL DISPLAY................................................................................... 3
2. LIMITATIONS ................................................................................................................. 4
2.1 OPERATIONAL ...................................................................................................................... 4
2.2 USER MANUAL..................................................................................................................... 5
2.3 SYSTEM SOFTWARE .............................................................................................................. 5
2.4 MAGNETIC VARIATION......................................................................................................... 5
2.5 POWER ON SELF TEST (POST)............................................................................................. 5
2.6 PLACARD.............................................................................................................................. 5
3. EMERGENCY / ABNORMAL PROCEDURES ........................................................... 5
3.1 EMERGENCY PROCEDURES ................................................................................................... 5
3.2 ABNORMAL PROCEDURES .................................................................................................... 5
4. NORMAL PROCEDURES .............................................................................................. 6
4.1 DETAILED OPERATING PROCEDURES ................................................................................... 6
4.2 SYSTEM SWITCHES / CONTROLS ........................................................................................... 6
4.3 DISPLAY ANNUNCIATORS..................................................................................................... 7
4.4 ADVISORY INDICATIONS ....................................................................................................... 8
4.5 I-LINK TERRAIN AWARENESS................................................................................................ 8
4.6 LANDMARK TAWS BASED TERRAIN ................................................................................... 9
4.7 LIGHTNING STRIKE DATA...................................................................................................... 9
4.8 RADAR DISPLAY:.................................................................................................................. 9
4.8.1 False Return Displays.......................................................................................................................... 10
4.9 DISPLAY OF SKYWATCH TRAFFIC ....................................................................................... 10
5. PERFORMANCE............................................................................................................ 11
6. WEIGHT AND BALANCE............................................................................................ 11
7. AIRPLANE & SYSTEM DESCRIPTIONS ................................................................. 11

Airplane Flight Manual Supplement
UPS Aviation Technologies i-linc MFD
2345 Turner Rd. SE February 10, 2003
Salem, OR 97302 Part #:560-1045-02 Rev A
FAA Approved
Date: February 26, 2003 Page 3 of 11
1. GENERAL
1.1 I-LINC MULTI-FUNCTIONAL DISPLAY
The i-linc Multi-Function Display (MFD) is a General Aviation in-cockpit display designed to
provide the pilot with a wide variety of situational awareness related information. The display is
capable of displaying Moving Map, Terrain Awareness information and VFR/IFR charting
functions. Basic information displayed includes airports, navigational aids, terrain, current flight
plan and more.
Figure 1 i-linc MFD
The i-linc MFD can provide display and control for the Goodrich SKYWATCH® and
SKYWATCH HP systems. Traffic will appear on the traffic page, thumbnail and can be overlaid
on the custom moving map.

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Rd. SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA Approved
Page 4 of 11 Date: February 26, 2003
The i-linc MFD can display relative terrain proximity as supplied by the internal database, or by
the Goodrich LANDMARK® external TSO-C151a certified TAWS sensor. When the terrain is
depicted from the external TAWS sensor, this depiction is specifically referred to as TAWS based
terrain.
Airborne weather radar systems can also be interfaced, allowing weather display functions similar
to that of the original equipment indicator. The I-linc does not support the accessory functions of
some indicators, such as flight plan overlay, checklist presentations etc.
The i-linc MFD Obstruction database includes man made obstacles greater than 250’ AGL as
provided by NOAA. This database is updated on a 56 day cycle on the front loading datacard with
other nav databases. Symbology similar to sectional charts show towers and poles. Catenary
support structures that support overhead transmission lines located across rivers, chasms gorges etc
are depicted with a crossed symbol.
The i-linc MFD has a built in pre-heat mode (30 seconds to 60 seconds) on each startup below
30C. During the pre-heat mode, the display will remain dark. The pre-heat mode is designed to
extend the life of the LCD backlight.
WARNING
The radar system generates microwave radiation and improper use,
or exposure, may cause serious bodily injury.
DO NOT OPERATE THIS EQUIPMENT UNTIL YOU HAVE
READ AND CAREFULLY FOLLOWED THE SAFETY
PRECAUTIONS AND INSTRUCTIONS in the
RADAR USER MANUAL
2. LIMITATIONS
2.1 OPERATIONAL
The i-linc MFD is limited to supplemental VFR Navigation only. The i-linc multifunction
display is provided to enhance situation awareness under VFR & IFR conditions. Precise lateral
navigation guidance must be predicated on the associated remote CDI/HSI instrument. The i-linc
MFD integrates with separately approved sensor installations.
When heading information is not available, traffic presentation will be offset by any wind
correction angle.
Adherence to limitations in appropriate installation AFM supplements is mandatory.

Airplane Flight Manual Supplement
UPS Aviation Technologies i-linc MFD
2345 Turner Rd. SE February 10, 2003
Salem, OR 97302 Part #:560-1045-02 Rev A
FAA Approved
Date: February 26, 2003 Page 5 of 11
2.2 USER MANUAL
The manual or the information contained in the manual listed below(or later appropriate revisions),
must be immediately available to the flight crew.
·i-linc MFD Multi-Function Display Pilot’s Guide……P/N 0040-19001-01 Rev D
2.3 SYSTEM SOFTWARE
The system software resides on the front loading datacard. The front loading datacard must be
inserted into the unit for operational use and not removed during flight. The system must utilize
the software version listed below (or later FAA approved versions). The software version can be
displayed in the system mode on the i-linc display under the INFO smart key.
·i-linc Software ........................................... Ver 4.1 (138-0448-041)
·i-linc Software (with ChartView ®).......... Ver 4.1 (138-0456-041)
2.4 MAGNETIC VARIATION
The automatic magnetic variation (MagVar) correction is not available in the i-linc MFD above
73°North or below 73°South latitude. All bearing and track information is computed and
displayed relative to true north in these polar regions.
2.5 POWER ON SELF TEST (POST)
The i-linc MFD performs a self test when power is applied. The pilot is responsible for verifying
all tests pass. If any of the i-linc MFD tests fail, power off the i-linc MFD.
2.6 PLACARD
Aircraft will have a placard identifying the MFD circuit breaker. The placard will be placed
directly adjacent to the respective breaker.
3. EMERGENCY / ABNORMAL PROCEDURES
3.1 EMERGENCY PROCEDURES
No change. Refer to approved Airplane Flight Manual.
3.2 ABNORMAL PROCEDURES
No change. Refer to approved Airplane Flight Manual.

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Rd. SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA Approved
Page 6 of 11 Date: February 26, 2003
4. NORMAL PROCEDURES
4.1 DETAILED OPERATING PROCEDURES
The normal operating procedures for the i-linc MFD are described in the Pilot’s Guide listed in the
Section 2.2 on page 5. The pilot shall review and clear all messages after power up.
CAUTION
Caution must be exercised when viewing the map function page in
the North-Up mode to avoid disorientation when transferring to a
function page presented in the Track-UP mode.
4.2 SYSTEM SWITCHES / CONTROLS
a) Power/Brightness
The power/brightness control is on the upper right corner of the i-linc MFD. Pulling out this
knob will allow for the brightness to be controlled manually.
b) Function Key FN
The function key is located on the lower left corner of the i-linc MFD. The function key
allows the user to scroll through the available functions.
c) Smart Function Option Keys
The soft keys along the bottom allow for selection of the function as identified directly above
it or perform commonly used actions within a function.
d) Menu/Enter Key
The Menu /Enter key is located on the bottom right hand corner of the i-linc MFD. Press the
Menu/Enter key to show a menu of options to modify the display of the current function.
Press the Menu/Enter key again to hide the menu. The Menu/Enter key is also used to
confirm entry when user input is required.
e) Line Select Keys
The line select keys are on the right hand side of the i-linc MFD. These keys are activated by
the Menu/Enter Key. The keys control the various options available to the user.

Airplane Flight Manual Supplement
UPS Aviation Technologies i-linc MFD
2345 Turner Rd. SE February 10, 2003
Salem, OR 97302 Part #:560-1045-02 Rev A
FAA Approved
Date: February 26, 2003 Page 7 of 11
4.3 DISPLAY ANNUNCIATORS
These annunciators are displayed on the left-hand side of the i-linc MFD display screen:
a) “POS” (Amber) No valid position information is available from the source. Do not
expect a valid position, valid terrain and valid traffic representation on the maps. The
Ownship symbol will have a red “X” through it.
b) “RTE” (Amber) No valid route (flight plan) is available from the external navigation
source. Route (Flight plan) information will not be shown on the maps. The Ownship
symbol will have a red “X” through it.
c) “ALT” (Amber) No valid altitude information is available from the external source.
Altitude related functions will not operate, such as terrain awareness.
d) “LT” (Amber) No valid lightning detection information is being received from the
external source. Strike and cell information will not be displayed.
e) “TER” (Amber) Terrain coverage is not available for some part of the terrain advisory
coverage area. Terrain advisories may not be provided.
f) “MSG” (Amber) Indicates a message is available on the message page.
g) “SKYW” (Amber) No valid traffic information is being received from the Skywatch
sensor. Traffic information will not be displayed.
h) “RDR” (Amber) Indicates that radar status information is not available from the
external radar transmitter head. Radar related functionality may not be available.
i) “RDR” (Green) Indicates that the radar is ON and transmitting RF energy. Appropriate
precautions should be taken.
j) “RDR” (Green - Flashing) Indicates that the radar is in Hold and freezes the display
image. Depending on the last state, the radar may be transmitting RF energy. Appropriate
precautions should be taken.
k) “TAWS” (Amber) Indicates that no terrain information is being received from the
Goodrich Landmark TAWS system. Terrain depiction may not be provided.

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Rd. SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA Approved
Page 8 of 11 Date: February 26, 2003
4.4 ADVISORY INDICATIONS
These are displayed on the upper left hand side of the i-linc MFD.
a) Lightning Advisory The lightning advisory flag will show on the left side of the display
when the WX500 sends an indication that lightning has been detected near your location.
See the WX500 manual for details about range and other detection parameters.
b) Terrain Advisory The terrain advisory flag will appear on the left side of the display when
the terrain surface altitude or an obstruction is within approximately 500 feet of your
altitude and within approximately two minutes of flight in any direction. This only applies
to the i-linc MFD internal terrain functionality. When an external TAWS system is
connected, supplemental terrain alerting annunciation is provided directly on the TER
(Terrain) Function.
c) Traffic Advisory The traffic advisory (TA) flag will appear on the left side of the display
when the Skywatch sensor detects traffic. See the Skywatch Pilot’s manual for details
about range and other detection parameters.
4.5 I-LINK TERRAIN AWARENESS
When an external TAWS sensor is not installed, internal terrain presentation capabilities are
available. Terrain that is closer than 2000 feet below the aircraft, or any terrain that is above the
aircraft, and is within the horizontal range of the i-link, will be displayed. Color variations are
used to show terrain heights relative to the aircraft, as follows:
·RED Terrain is at or above your current altitude.
·YELLOW Terrain that is within 500 feet below your current altitude.
·GREEN Terrain that is within 2000 feet below your current altitude.
·BLACK Terrain is greater than 2000 feet below your current altitude.
·LT BLUE NO terrain data is available
Red Terrain is also displayed on a small “Thumbnail” view provided in the upper right corner of
the display. See the i-link Users Guide for additional information.
Navigation, terrain and obstacle separation must NOT be predicated upon the use of the terrain
function. The i-linc is not authorized to provide terrain separation. Terrain data is advisory only.
For all terrain functions, it is necessary that the aircraft altitude encoder be calibrated on a bi-
annual basis. The i-linc internal terrain function is not TSO approved and does not provide TAWS
equivalent functionality.

Airplane Flight Manual Supplement
UPS Aviation Technologies i-linc MFD
2345 Turner Rd. SE February 10, 2003
Salem, OR 97302 Part #:560-1045-02 Rev A
FAA Approved
Date: February 26, 2003 Page 9 of 11
4.6 LANDMARK TAWS BASED TERRAIN
When the system is interfaced to the Goodrich Landmark® TAWS system, terrain data is provided
by that external sensor. The color coding utilized follows the users guide for the Landmark®
system. The “Alt” and “Baro” fields normally present on the Navigational Bar will not be
displayed.
The i-linc will automatically “Pop-Up” to the terrain page when a terrain alert is generated by the
Landmark® TAWS system. Terrain “Pop-Up” takes priority over Traffic based “Pop-Ups”.
Primary means for alerting to a TAWS based Caution or Warning Alert is provided by the aural
messages generated by the Landmark® system, and visual annunciation provided by external
cockpit lamps.
For detailed operating instructions regarding the Landmark® system, refer to the Landmark®
User’s Guide.
4.7 LIGHTNING STRIKE DATA
For installations that interface to the Goodrich WX-500 Stormscope®, lightning strike data
detected by the WX-500 will appear on the i-linc MFD. For detailed operating instructions
regarding the interface of the i-linc MFD with the WX-500, refer to the WX-500 User’s Guide and
the i-linc MFD Pilot’s Guide for the WX-500 Stormscope interface.
4.8 RADAR DISPLAY:
For installations that interface to an airborne weather radar system, the radar returns will be painted
on the i-linc MFD. For detailed operating instructions regarding the interface of the i-linc MFD
with an airborne weather radar system, refer to the Radar System’s Pilots Operating Handbook
Supplement and the i-linc MFD Pilot’s Guide. The main modes of radar operation are as follows:
a) On/Off Mode: Turns the power on/off to the radar transmitter.
b) Standby Mode: Turns DC power on to the radar transmitter. The radar antenna will perform
initialization and start scanning, however, no RF energy is transmitted and the unit will not
return reflections.
c) Test Mode: Test mode is used to ensure proper functionality of the display and radar
transmitter unit. A rainbow test pattern will be displayed when the unit is in the test mode. No
RF energy is transmitted in this mode.
d) WX Mode: Standard weather mapping mode. RF energy is being transmitted from the antenna
and returned reflections are displayed on the screen.
e) Ground MAP Mode: The sensitivity of the antenna is adjusted to better display ground related
features. RF energy is being transmitted in this mode and returned reflections are displayed on
the screen. Gain is adjustable.
Control Features
a) Horizontal Mode: The antenna sweeps in the horizontal plane at the desired tilt angle.

Airplane Flight Manual Supplement
i-linc MFD UPS Aviation Technologies
February 10, 2003 2345 Turner Rd. SE
Part #:560-1045-02 Rev A Salem, OR 97302
FAA Approved
Page 10 of 11 Date: February 26, 2003
b) Tilt Control: Adjusts the tilt when in the Horizontal Mode.
c) Vertical Mode: The antenna sweeps in the vertical plane at the desired bearing angle.
d) BRG Control: Adjusts the bearing when in the Vertical Mode.
e) Hold Mode: Freezes the last radar scan.
4.8.1 False Return Displays
Ground radar stations or other airborne weather Radars may occasionally cause interference with
the presentation of the return. The effect of this interference is to create one or more radial bands
of false signal or noise extending from the bottom center outward to the outer range scale. These
effects are usually of short duration and are dependent on the airplane’s position and range from
the ground station, the signal strength, and other factors. The i-linc MFD will present all data as
returned from the radar sensor data bus. Caution should be exercised when interpreting a weather
radar display.
4.9 DISPLAY OF SKYWATCH TRAFFIC
CAUTION
It is recommended to view all functions in the Track-UP mode to
avoid disorientation when transferring to the Traffic page.
The Traffic “Thumbnail” is NOT available to the pilot on the
Custom Map page when the map function is in
the North-Up mode or Desired Track (DTK) mode.
For installations that interface with the Goodrich SKYWATCH® Traffic Advisory System (TAS)
or Traffic Alert & Collision Avoidance System I (TCAS I), traffic data detected by the
SKYWATCH® will appear on the i-linc MFD. For detailed operating instructions regarding the
interface of the i-linc MFD with the SKYWATCH®, refer to the FAA Approved Flight Manual
Supplement for the SKYWATCH®, the Pilot’s Guide for the SKYWATCH® and the i-linc MFD
Pilot’s Guide for the SKYWATCH® System.

Airplane Flight Manual Supplement
UPS Aviation Technologies i-linc MFD
2345 Turner Rd. SE February 10, 2003
Salem, OR 97302 Part #:560-1045-02 Rev A
FAA Approved
Date: February 26, 2003 Page 11 of 11
5. PERFORMANCE
No change.
6. WEIGHT AND BALANCE
See current weight and balance data.
7. AIRPLANE & SYSTEM DESCRIPTIONS
See i-linc MFD Pilot’s Guide for a complete description of the i-linc MFD System.