Honeywell_Satellite_Radio_KNI

Honeywell - Confidential

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ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC.

KNI 582

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The documents and information contained herein ("the Materials") are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc (collectively "Honeywell"). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned-subsidiaries or a formally designated third party service provider thereunder; and direct recipients of Materials from Honeywell's Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement.

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KNI 582

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OF LAW, OR OTHERWISE.

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KNI 582

TABLE OF CONTENTS

SECTION 1

GENERAL INFORMATION

1.1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 1.2 EQUIPMENT DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 1.3 TECHNICAL CHARACTERISTICS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1 1.4 UNITS AND ACCESSORIES SUPPLIED . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4 1.4.1 KNI 582 RMI CONFIGURATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4 1.4.2 KNI 582 RMI INSTALLATION KIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4 1.5 ADDITIONAL EQUIPMENT REQUIRED, BUT NOT SUPPLIED. . . . . . . . . . 1-5 1.6 LICENSE REQUIREMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-6

SECTION 2

INSTALLATION

2.1 GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2.2 UNPACKING AND INSPECTING EQUIPMENT . . . . . . . . . . . . . . . . . . . . . . 2-1 2.3 KNI 582 RMI INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1 2.4 POST INSTALLATION CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

SECTION 3

OPERATION

3.1 GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1 3.2 NORMAL OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1

KNI 582

LIST OF FIGURES

Figure 2-1 KNI 582 Outline and Mounting Drawing . . . . . . . . . . . . . . . . . . . . . . . 2-5 Figure 2-2 Connector Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-7 Figure 2-3 KNI 582 Pin Functions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8 Figure 2-4 KNI 582/KDF 805/KNR 665A/KNR 615 Interconnect . . . . . . . . . . . . . 2-9 Figure 2-5 KNI 582/KDF 805/KNR 630 Interconnect . . . . . . . . . . . . . . . . . . . . . 2-11 Figure 2-6 KNI 582/KR 87/KNS 81/KN 53 Interconnect . . . . . . . . . . . . . . . . . . . 2-13 Figure 2-7 KNI 582/Bendix DF-2071A/Bendix CN2011A/

Collins ADF-60A/Collins VIR-30A Interconnect 2-15

Figure 2-8 KNI 582 Cable Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-17 Figure 2-9 KNI 582 Cable Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-18 Figure 2-10 KNI 582 Serial OBI Interface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-19 Figure 3-1 KNI 582 Control Functions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-2

KNI 582

SECTION 1

GENERAL INFORMATION

1.1 INTRODUCTION

This manual contains information relative to the physical, mechanical, and electrical characteristics of the KNI 582 Radio Magnetic Indicator. General installation instructions are also included.

1.2 EQUIPMENT DESCRIPTION

The KNI 582 Radio Magnetic Indicator (PN 066-3060-00/01/02/03/04/10/11/12/13) provides bearing information to either ADF or VOR stations by means of two pointers, each of which is read against the compass card. The type of information displayed by each needle (assuming applicable inputs are present) is determined by the corresponding front panel switch.

A servo drive compass card with a fixed lubber line displays aircraft heading information. A flag falls into view in the upper left corner of the display when the aircraft heading information being displayed is invalid.

1.3 TECHNICAL CHARACTERISTICS

Table 1-1 - KNI 582 RMI Technical Characteristics

KNI 582

1.4 UNITS AND ACCESSORIES SUPPLIED

1.4.1 KNI 582 Configurations

The KNI 582 RMI is available in the following versions:

1.4.2 KNI 582 RMI Installation Kit

KNI 582 RMI Installation Kit PN 050-01823-0000/0001. (solder type) KNI 582 RMI Installation Kit PN 050-01823-0002/0003. (crimp type)

The -0000/-0002 installation kit is used for black panel mounting. The -0001/-0003 installation kit is for gray panel mounting. (See Paragraph 2.3 KNI 582 RMI INSTALLATION for installation instructions.)

KNI 582

1.6LICENSE REQUIREMENTS None.

1.7CONTINUED AIRWORTHINESS INSTRUCTIONS 1.7.1 Equipment

The instructions for continued airworthiness given in the TC or STC approvals for this product supplements or supersedes the instructions for continued airworthiness in this manual.

Most Honeywell products are designed and manufactured to allow "on condition maintenance". On condition maintenance is described as follows; There are no periodic service requirements necessary to maintain continued airworthiness. No maintenance is required until the equipment does not properly perform its intended function. When service is required, a complete performance test should be accomplished following any repair action. Consult the appropriate unit Maintenance/Overhaul Manual for complete performance test information.

14 CFR Part 25.1529 Instructions for Continued Airworthiness is met per the following instructions:

A.The removal of the equipment is on the condition of failure. There is no re- quired maintenance.

1.7.2Wires/Coax Cables

During on-condition or regularly scheduled maintenance, inspect wires and coax cables following the guidelines listed in AC 43.13-1B Chapter 11, 12 as necessary.

KNI 582

SECTION 2

INSTALLATION

2.1 GENERAL

This section contains the suggestions and information to consider before installation of the KNI 582 Radio Magnetic Indicator into the aircraft. Close adherence to these suggestions will assure optimum performance from the equipment.

2.2 UNPACKING AND INSPECTING EQUIPMENT

Exercise extreme care when unpacking the equipment. Make a visual inspection of the unit for evidence of damage during shipment. If a claim for damage is to be made, save the shipping container to substantiate the claim. The claim should be promptly filed with the transportation company. It would be advisable to retain the container and packing material after all equipment has been removed, in the event that equipment storage or reshipment should become necessary. The KNI 582 RMI installation will conform to standards designated by the customer, installing agency and existing conditions as to unit location and type of installation.

2.3KNI 582 RMI INSTALLATION

A.Plan a location on the aircraft panel that is clearly visible to the pilot with the least practicable deviation from his normal position and from his line of vision when he is looking forward along the flight path.

B.Make certain that clearance is available for the installation of the cables and connectors, and also that normal vibration does not cause the unit to bump against other equipment cases.

C.If an instrument hole that meets the installation requirements is not available, cut a 3" ATI hole per Figure 2-1. Secure the unit with four 3/4" long 6-32 instrument screws.

D.The KNI 582 RMI may be secured in place from front or behind the panel.

2.4POST INSTALLATION CHECK

These are tests designed to show that the KNI 582 RMI is functioning accurately under broadly nominal conditions.

A.Compass Card Accuracy

1.With the aircraft on a known magnetic heading, this heading ??2?? should be under the lubber line of KNI 582 RMI.

KNI 582

2.The above step should be repeated for at least one additional heading 90?? from the first.

B.ADF Accuracy

1.Depending on the application, the KNI 582 RMI can be tested for either DC SIN/COS ADF or X, Y, Z, ADF by tuning in a station on the appropriate ADF.

2.In the DC SIN/COS Mode the needles should position the direction of the station +5??. Repeat for at least one more station.

3.Repeat Step 2 for X, Y, Z, ADF +5??.

C.VOR Accuracy

1.Depending on the application, the KNI 582 RMI can be tested for either OBI DIGITAL VOR, COMPOSITE VOR, or OBI SIN/COS VOR by tuning in a station on the appropriate VOR.

2.In the OBI DIGITAL VOR Mode, the single needle should point to the station +5??. Repeat for at least one more station.

3.Repeat Step 2 for COMPOSITE VOR +5??.

4.Repeat Step 2 for OBI SIN/COS VOR +5??.

D.VOR/LOC Composite Correction Adjustment

If it is necessary to make a VOR/LOC composite needle centering adjustment due to NAV receiver composite error, the KNI 582 RMI pointer can be adjusted externally using the following steps:

1.With a ramp-test NAV generator, generate an output so the NAV receiver can be tuned into a given bearing.

2.With the NAV receiver tuned to the generator frequency, insert a tuning tool into VOR/LOC composite adjustment hole (refer to Figure 2-1) and adjust R232 until the selected needle reads the same bearing the ramp generator.

3.Repeat Step 2 for verification of the adjustment for another bearing on the ramp with generator.

KNI 582

TEST DATA

Compass Card Accuracy

(Magnetic Heading) minus (KNI 582 RMI Indication) = Error

(??2?? Max.)

ADF (D.C. SIN/COS) Accuracy

(Station Heading) minus (KNI 582 RMI Indication) = Error

(??5?? Max.)

ADF (X, Y, and Z) Accuracy

(Station Heading) minus (KNI 582 RMI Indication) = Error

(??5?? Max.)

VOR (OBI DIGITAL) Accuracy

(Station Bearing) minus (KNI 582 RMI Indication) = Error

(??5?? Max.)

VOR (Composite) Accuracy

(Station Bearing) minus (KNI 582 RMI Indication) = Error

(??5?? Max.)

VOR (OBI SIN/COS) Accuracy

(Station Bearing) minus (KNI 582 RMI Indication) = Error

(??5?? Max.)

KNI 582

SECTION 3

OPERATION

3.1 GENERAL

The KNI 582 RMI display is discussed below:

The KNI 582 RMI repeats magnetic heading information from a directional gyro system. Aircraft heading is read under the lubber line of the KNI 582 RMI.

When an ADF receiver is tuned to a station and the appropriate pointer placed in the ADF mode, the arrow of the pointer indicates the magnetic heading to the ADF station. Thus, if the pilot desires to fly toward the station, he merely turns his aircraft to the magnetic heading indicated by the pointer.

When a VOR receiver is tuned to a VOR station and the appropriate pointer placed in the VOR mode, the arrow of the pointer indicates the magnetic heading to the VOR station. If the KNI 582 RMI is used in an area navigation system, the VOR pointer indicates magnetic heading to the waypoint. Should a localizer frequency be selected or the VOR receiver indicates a flagged condition, the VOR pointer is parked 90?? to the right of the lubber line.