UPS Aviation Technologies i-linc MFD Supplemental Manual Download Page 10

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

 

D

ISPLAY OF 

S

KYWATCH 

T

RAFFIC

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.

Summary of Contents for i-linc MFD

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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