Honeywell Satellite Radio KNI 582 User Manual

INSTALLATION

MANUAL

KNI 582

RADIO MAGNETIC

INDICATOR

Manual Number 006-00193-0003

Revision 3, March/2007

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KNI 582

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KNI 582

REVISION HIGHLIGHTS

Date

Part Number

Rev

Description

006-00193-0003

Mar/2007

Replace all pages of the manual. This is a

complete reprint.

Removed NVG versions from the manual.

Rev 3, March/2007

©Honeywell International Inc. Do not print without express permission of Honeywell.

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KNI 582

TABLE OF CONTENTS

SECTION 1

GENERAL INFORMATION

1.1

1.2

1.3

1.4

1.4.1

1.4.2

1.5

INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

EQUIPMENT DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

TECHNICAL CHARACTERISTICS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

UNITS AND ACCESSORIES SUPPLIED . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

KNI 582 RMI CONFIGURATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

KNI 582 RMI INSTALLATION KIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

ADDITIONAL EQUIPMENT REQUIRED, BUT NOT SUPPLIED. . . . . . . . . . 1-5

LICENSE REQUIREMENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-6

1.6

SECTION 2

INSTALLATION

2.1

2.2

2.3

2.4

GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

UNPACKING AND INSPECTING EQUIPMENT . . . . . . . . . . . . . . . . . . . . . . 2-1

KNI 582 RMI INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

POST INSTALLATION CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

SECTION 3

OPERATION

3.1

3.2

GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1

NORMAL OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1

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KNI 582

LIST OF FIGURES

Figure 2-1

Figure 2-2

Figure 2-3

Figure 2-4

Figure 2-5

Figure 2-6

Figure 2-7

KNI 582 Outline and Mounting Drawing . . . . . . . . . . . . . . . . . . . . . . . 2-5

Connector Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-7

KNI 582 Pin Functions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8

KNI 582/KDF 805/KNR 665A/KNR 615 Interconnect . . . . . . . . . . . . . 2-9

KNI 582/KDF 805/KNR 630 Interconnect . . . . . . . . . . . . . . . . . . . . . 2-11

KNI 582/KR 87/KNS 81/KN 53 Interconnect . . . . . . . . . . . . . . . . . . . 2-13

KNI 582/Bendix DF-2071A/Bendix CN2011A/

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

Figure 2-8

Figure 2-9

Figure 2-10

Figure 3-1

KNI 582 Cable Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-17

KNI 582 Cable Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-18

KNI 582 Serial OBI Interface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-19

KNI 582 Control Functions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-2

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KNI 582

LIST OF TABLES

Table 1-1 - KNI 582 RMI Technical Characteristics. . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

Table 1-2 - KNI 582 RMI Configurations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

Table 1-3 - KNI 582 RMI Installation Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

Table 1-4 - Additional Equipment, Compatible with KNI 582 RMI . . . . . . . . . . . . . . . . 1-5

Rev 3, March/2007©Honeywell International Inc. Do not print without express permission of Honeywell.

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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

SPECIFICATION

TSO Compliance:

CHARACTERISTIC

Env. Cat. RTCA DO-160A

A1D1/A/SKP/XXXXXSABAAA

-20°C to +55°C

50,000 feet

Temperature:

Altitude:

Compass:

TSO C6c

ADF:

TSO C41c Class A

TSO C40a

VOR:

WEIGHT and DIMENSIONS:

See Figure 2-1 KNI 582 Outline and Mounting

Drawing.

Table 1-1 - KNI 582 RMI Technical Characteristics

Rev 3, March/2007

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KNI 582

SPECIFICATION

POWER REQUIREMENTS

Primary:

CHARACTERISTIC

11.33VDC 0.4A maximum

26VAC 400Hz 6VA

Lighting:

28V at 80mA maximum

5V at 460mA maximum

Note: 14V Installations may use 5V Versions

with dropping resistor.

COMPASS HEADING INPUT

COMPASS VALID

Operates from any slaved magnetic compass

with ARINC X, Y, and Z outputs. Z grounded

externally.

Valid = +27.5VDC

Invalid = 0VDC 2mA maximum

VOR/LOC COMPOSITE INPUT

(-04 Version TACAN

Compatible)

0.5VRMS 0° phase composite 30Hz variable AM

and 30Hz reference FM on a 9960Hz carrier

(ARINC Std.) (0.7VRMS maximum)

NAV SUPERFLAG

(Horizontally parked needle)

Flag < +3.5VDC

No Flag > +10VDC

ILS ENERGIZE

(Horizontally parked needle)

ILS < +1VDC (GND)

VOR = Open (+33VDC Maximum)

ADF X, Y, Z

Operates from any ADF receiver with ARINC X,

Y, Z outputs. Z grounded externally. 11.8VRMS

400Hz 180° index, positive rotation reference.

OBI SIN/COS

4 wire SIN/COS 10VRMS 400Hz. 0° when SIN =

0VRMS and COS = maximum positive VRMS.

Positive rotation reference with COS decreasing

and SIN increasing in-phase for increasing

degrees.

ADF DC SIN/COS

OBI DIGITAL

Common Mode: 0 to 5VDC

Differential: 3VDC 10%

Electrical Characteristics

A. Driver

1. Open collector referenced to ground

2. Maximum “low” voltage (with 2 receiver loads

(500 Ohm) returned to 10.35 volts) = 1.0V.

Table 1-1 - KNI 582 RMI Technical Characteristics (Cont)

Rev 3, March/2007

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KNI 582

SPECIFICATION

B. Receiver

CHARACTERISTIC

1. Input resistance = 1K 5% returned to +V

2. +V = 9.0V 15%

C. Interconnecting Lines

II Waveform Timing

A. Data

1. Maximum Shunt Capacity = 2000 pF

1. Data Rate - Approx. 1KHz

2. Negative Logic (“Low True”)

B. Clock

1. The negative going edge of the clock

waveform will be greater than 10us and less

than 250us from any data transistors point.

2. The minimum time that the clock spends in

either the high or low state will be greater

than 10us.

C. Sync

1. The sync pulse is a negative going pulse

following the data word.

2. The negative going edge of the sync pulse

will be a minimum of 70us and a maximum of

350us after the negative going edge of the

last clock pulse.

3. The sync pulse will be a minimum of 10us

wide and a maximum of 260us wide.

III Data Word Format

1. BCD, 0.1’s, 1’s, 10’s, 100’s

2. LSD to MSD

3. LSB to MSB

4. Maximum Word Rate = 12Hz

5. When “8” Bit of 100’s is High (False) = Flag.

6. When “4” Bit of 100’s is High (False) = ILS

Mode.

100°

(4)

10°

1°

.1°

(8)

Flag

ILS 2 & 1 MSB

LSB MSB

<---- Time

LSB MSB

LSB ABC

Table 1-1 - KNI 582 RMI Technical Characteristics (Cont)

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KNI 582

1.4 UNITS AND ACCESSORIES SUPPLIED

1.4.1 KNI 582 Configurations

The KNI 582 RMI is available in the following versions:

PART NUMBER DESCRIPTION

066-3060-00

066-3060-01

066-3060-02

066-3060-03

066-3060-04

066-3060-10

066-3060-11

066-3060-12

066-3060-13

Black Bezel, 27.5 VDC/26VAC Lights

Black Bezel, 5 VDC/5VAC Lights

Black Bezel, 27.5 VDC/26VAC Lights

Black Bezel, 5 VDC/5VAC Lights

Black Bezel, 5 VDC/5VAC Lights (TACAN Compatible)

Black Bezel, 27.5 VDC/26VAC Lights

Black Bezel, 5 VDC/5VAC Lights

Black Bezel, 27.5 VDC/26VAC Lights

Black Bezel, 5 VDC/5VAC Lights

Table 1-2 - KNI 582 RMI Configurations

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.)

PART NUMBER

DESCRIPTION

Bulletin

-00

-01

-02

-03

006-00540-0000

073-00044-0001

073-00045-0000

073-00045-0001

Mooring Plate

Black Adapter Plate

Gray Adapter Plate

Table 1-3 - KNI 582 RMI Installation Kit

Rev 3, March/2007

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KNI 582

PART NUMBER

DESCRIPTION

-00

-01

-02

-03

089-05115-0012

089-06461-0012

030-01157-0011

030-01176-0000

030-01188-0000

030-02350-0015

030-02414-0001

Scr. FHP 6-32 x 3/4

Socket Crmp 20G

HSG Conn 50S

Pin Polrzin Female

Conn Sub-Min F 50P

Hood & Lvr Mdfd

Table 1-3 - KNI 582 RMI Installation Kit (Cont)

1.5 ADDITIONAL EQUIPMENT REQUIRED, BUT NOT SUPPLIED

The following are navigation receivers, ADF receivers, and compass systems compatible

with the KNI 582 RMI.

NAV RECEIVERS

ADF RECEIVERS

COMPASS

KN 53:

TSO’d.

KR 85 (225 01/04) TSO’d KCS 305 TSO’d

KNS 80:

Env. DO-160, Area

NAV AC 90-45A

KR 87 TSO'd

KCS 55/55A TSO'd

KPI 550 TSO’d

KNS 81:

Area NAV AC 90-45A KDF 800 TSO’d

KX 155/165: TSO’d

KDF 805 TSO’d

KDF 8000 TSO’d

KX 170B:

KX 175B:

KNR 615:

KNR 630:

KNR 634:

KNR 665:

KNR 665A:

Non-TSO’d

TSO’d

Area NAV AC 90-45

Table 1-4 - Equipment Compatible with KNI 582 RMI

Crimping tools, mooring plates and power tools are referenced in individual installation

manuals.

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KNI 582

1.6 LICENSE REQUIREMENTS

None.

1.7 CONTINUED 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:

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

quired maintenance.

1.7.2 Wires/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.

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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.

2.3 KNI 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.

2.4 POST 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.

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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.

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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.)

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KNI 582

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KNI 582

Figure 2-2 Connector Assembly

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KNI 582

Figure 2-3 KNI 582 Pin Functions

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KNI 582

Figure 2-8 KNI 582 Cable Assembly

(Dwg No 155-02114-0000, R-AA)

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KNI 582

SECTION 3

OPERATION

3.1 GENERAL

The KNI 582 RMI display is discussed below:

A. Compass Card/Lubber Line:

B. Compass Flag:

This rotating card repeats gyro stabilized

magnetic compass information. Aircraft

heading is read from the compass card

under the orange lubber line.

This flag comes into view whenever the

compass system determines that the

heading is invalid or the indicated heading

has an error of 5° or more.

C. Pointers:

The arrow of either pointer indicates the

magnetic heading to a VOR station/area

navigation waypoint of an ADF station

depending on the position of the front panel

switches associated with the pointer.

3.2 NORMAL OPERATION

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.

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KNI 582

Figure 3-1 KNI 582 Control Functions

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