Sandel SN4500 Manual

82009-PG-ERR-F2 SANDEL SN4500 PILOT’S GUIDE ERRATA PAGE 1OF 2
SN4500 EHSI
Pilot’s Guide Effectivity and Errata
Insert this update ahead of the cover page of the Pilot’s Guide referenced
below.
Date:
Effectivity:
Errata:
23-APR-2015
SN4500 Software Version A2.06 &
2.05
Pilots Guide 82009-PG-F
With the exception of the
superseding information contained
in this document, operation of the
SN4500 is as described in the
SN4500 Pilot’s Guide referenced
above.
`
There are no errata for this update.

82009-PG-ERR-F2 SANDEL SN4500 PILOT’S GUIDE ERRATA PAGE 2OF 2
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SN4500
Primary Navigation Display
with
Reversionary Attitude Mode
and
LNAV Roll Steering
Pilot’s Guide

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE II
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82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE III
Pilot information
Publication Date: 05-SEP-2012
This guide provides information on the use and operation of the SN4500
Primary Navigation Display.
Information in this manual is current as of publication or revision date.
Specifications and operational details are subject to change without notice
at the discretion of Sandel Avionics, Inc.
Copyright
Copyright 2012 Sandel Avionics, Inc.
May be covered by one or more US and foreign patents, including:
US Patent Nos. 6,259,378, 6,670,892, 6,507,288, 6,750,788,
6,972,695, and 7,187,304. Australia Patent No. 750,651. China
Patent No. 1211639C. Israel Patent Nos. 135,174, 153,460, and
155,983.
All rights reserved. No part of this manual may be reproduced, stored or
distributed without written permission of Sandel Avionics, Inc. Additional
copies of this manual are available from:
Sandel Avionics, Inc.
2401 Dogwood Way
Vista, CA 92081
USA
Tel: [phone]
Fax: [phone]
www.sandel.com
Revision notice
The “Effectivity, Errata, and Revision History” allow the use of this Pilot
Guide with a specific software release. The “Effectivity, Errata, and
Revision History” specifically lists the software to which this Pilot’s Guide
applies and corrects any errors or omissions in this revision of the Pilot’s
Guide. Document number 82009-PG-ERR, Effectivity, Errata, and
Revision History” can be found on page XII of this Pilot’s Guide.

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE IV
Operational and legal issues
The information displayed on the SN4500 is generated by external
equipment. It is the pilot’s responsibility to ensure the correct
configuration and use of the external equipment. The SN4500 is subject to
all legal and operational limitations of the equipment supplying data to it.
Always refer to your approved Aircraft Flight Manual Supplement for
operation and limitations on the use of installed equipment.
Note: Because aircraft vary in their installed equipment, it is important to
note that what is displayed on the SN4500 may vary depending on the
presence or absence of equipment.
Please keep in mind that it is required by Federal Aviation Regulations to
have on board current charts appropriate to the flight. The moving map on
the SN4500 does not fulfill this requirement. A current internal database is
not required but is recommended. The internal database supplies
supplemental data only (such as nearest airports, navaids and airspace).
Flight plan waypoints and IFR approaches are supplied to the SN4500 by
the associated IFR approved GPS receiver. Supplemental data is intended
for positional awareness only and should not be used for primary
navigation.

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE V
Approvals
The FAA has approved the SN4500 under the following TSOs:
C3d: Turn and Slip Instrument
C4c: Bank and Pitch Instruments
C6d: Direction Instrument, Magnetic (Gyroscopically
Stabilized
C34e: ILS Glide Slope Receiving Equipment
C35d: Airborne Radio Marker Receiving Equipment
C36e: Airborne ILS Localizer Receiving Equipment
C40c: VOR Receiving Equipment
C41d: Airborne ADF Equipment
C113: Airborne Multipurpose Electronic Displays
C118: Traffic Alert and Collision Avoidance System Airborne
Equipment, TCAS I
C119b: Traffic Alert and Collision Avoidance System Airborne
Equipment, TCAS II
The following RTCA certification levels also apply to this product:
DO-160E: Environmental (Categories listed in Chapter 13)
DO-178B: Software Level C
DO-254: Hardware Level C
Installation of the SN4500 in a type-certificated aircraft must be performed
in accordance with the Sandel SN4500 Installation Manual, document
number 82009-IM applicable revision.

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE VI
Conventions Used in This Manual
The name of a button is placed within square brackets when the button is
described in text. For example, “…press the [VUE] selection button to …”
This manual uses terms, which should be familiar to aviation-minded
readers, such as “selected radial” and “magnetic heading”. Terms, which
are specific to the SN4500, will be placed in the glossary.

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE VII
Table of Contents
Pilot information III
Copyright III
Revision notice III
Operational and legal issues IV
Approvals V
Conventions Used in This Manual VI
Table of Figures X
Effectivity, Revision and Errata History XII
CHAPTER 1 WELCOME TO THE SN4500 1-1
What is the SN4500 1-1
CHAPTER 2 DISPLAY OVERVIEW 2-1
SN4500 Physical Features 2-1
Display Areas 2-1
Indicators 2-2
Data Color Coding 2-5
CHAPTER 3 BASIC OPERATION 3-1
Overview 3-1
Power-up Display 3-1
Selecting the Data 3-2
Selecting the Primary NAV Source 3-3
Selecting and Displaying Bearing Pointers 1 & 2 3-4
Displaying the Map Data 3-4
360-degree FULL View and 70-degree ARC View 3-5
Auto-Slewing the Course Pointer 3-5
Remote Course and Heading Knobs 3-6
Heading Bug Sync 3-6
MEM Function 3-6
Display Brightness (AUTO/MANUAL CONTROL SELECTION) 3-6
Display Brightness (INTERNAL BRIGHTNESS CONTROL) 3-7
Display Brightness (EXTERNAL BRIGHTNESS CONTROL) 3-7
Button Brightness 3-8
CHAPTER 4 NAV OPERATION 4-1
NAV Menu 4-1
GPS Mode Selection 4-1

82009-PG, REV F SANDEL SN4500 PILOT’S GUIDE PAGE VIII
GPS APPR Switch 4-2
Auto-Slew Function 4-2
Course Pointer Display Function 4-3
GPS INTEG / WAAS Annunciations 4-4
CHAPTER 5 LNAV / ROLL STEERING 5-1
Overview 5-1
What is “Roll Steering”? 5-1
LNAV and LNAV ARM 5-1
Intercepting an Active Leg (LNAV ARM) 5-2
“No Intercept” Message 5-3
LNAV Capture 5-3
HDG Preset Function during LNAV 5-3
HDG SYNC during LNAV 5-3
Flying a GPS approach 5-3
Flying a GPS transition to LOC/ILS 5-4
Flying a missed approach after an ILS 5-4
Cancelling LNAV Operations 5-4
Autopilot mode Selection Summary 5-4
Heading Bug Depiction Summary 5-5
ADVISORY MESSAGES ASSOCIATED WITH LNAV 5-5
CHAPTER 6 BEARING POINTERS 6-1
Bearing Pointers 6-1
BRG Menu 6-2
CHAPTER 7 MAP OPERATIONS 7-1
Overview 7-1
Internal Database 7-2
Map Controls and Displays 7-2
Map Memories 7-3
MAP DATABASE ITEMS 7-4
Getting Started - Example 7-5
Map Setup 7-6
Map Memory Settings 7-8
Storing Settings into Preset Memories 1-4 7-8
Removing a Map Memory from the Rotation Sequence 7-9
Restoring Default Settings 7-10
Copying Map Settings into the Scratchpad 7-11