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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

 

L

ANDMARK 

TAWS B

ASED 

T

ERRAIN

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

 

L

IGHTNING 

S

TRIKE 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

 

R

ADAR 

D

ISPLAY

:

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.

Содержание i-linc MFD

Страница 1: ...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 ma...

Страница 2: ...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 ANNUNCIATO...

Страница 3: ... 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 a...

Страница 4: ...ow 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...

Страница 5: ...n 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 pol...

Страница 6: ...FD 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 ac...

Страница 7: ...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...

Страница 8: ...ee 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...

Страница 9: ...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 Hand...

Страница 10: ... 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 Tra...

Страница 11: ...ruary 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 ...

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