Honeywell KNI 582 User Manual

INSTALLATION

MANUAL

KNI 582

RADIO MAGNETIC

INDICATOR

Manual Number 006-00193-0003

Revision 3, March/2007

Honeywell - Confidential

THIS DOCUMENT AND ALL INFORMATION AND EXPRESSION CONTAINED HEREIN ARE THE
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ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL
INC.

KNI 582

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KNI 582

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Copyright Notice

Copyright 1988, 2007 Honeywell International Inc. All rights reserved.

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. MLA-2

KNI 582

REVISION HIGHLIGHTS

Part Number Rev Date Description

006-00193-0003 3 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. RH-1

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

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

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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. LOT-1

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 CHARACTERISTIC

TSO Compliance: Env. Cat. RTCA DO-160A

A1D1/A/SKP/XXXXXSABAAA

Temperature: -20°C to +55°C

Altitude: 50,000 feet

Compass: TSO C6c

ADF: TSO C41c Class A

VOR: TSO C40a

WEIGHT and DIMENSIONS: See Figure 2-1 KNI 582 Outline and Mounting

Drawing.

Table 1-1 - KNI 582 RMI Technical Characteristics

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KNI 582

SPECIFICATION CHARACTERISTIC

POWER REQUIREMENTS

Primary: 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 Operates from any slaved magnetic compass

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

COMPASS VALID Valid = +27.5VDC

Invalid = 0VDC 2mA maximum

VOR/LOC COMPOSITE INPUT

(-04 Version TACAN
Compatible)

NAV SUPERFLAG

(Horizontally parked needle)

ILS ENERGIZE

(Horizontally parked needle)

0.5VRMS 0° phase composite 30Hz variable AM
and 30Hz reference FM on a 9960Hz carrier
(ARINC Std.) (0.7VRMS maximum)

Flag < +3.5VDC
No Flag > +10VDC

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 Common Mode: 0 to ± 5VDC

Differential: 3VDC ± 10%

OBI DIGITAL

I 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)

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SPECIFICATION CHARACTERISTIC

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

2. +V = 9.0V ± 15%

C. Interconnecting Lines 1. Maximum Shunt Capacity = 2000 pF

II Waveform Timing

A. Data 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.

KNI 582

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° 10° 1° .1°

(8)
Flag

(4)
ILS 2 & 1 MSB LSB MSB LSB MSB LSB ABC

<---- Time

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

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 1-3

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 Black Bezel, 27.5 VDC/26VAC Lights

066-3060-01 Black Bezel, 5 VDC/5VAC Lights

066-3060-02 Black Bezel, 27.5 VDC/26VAC Lights

066-3060-03 Black Bezel, 5 VDC/5VAC Lights

066-3060-04 Black Bezel, 5 VDC/5VAC Lights (TACAN Compatible)

066-3060-10 Black Bezel, 27.5 VDC/26VAC Lights

066-3060-11 Black Bezel, 5 VDC/5VAC Lights

KNI 582

066-3060-12 Black Bezel, 27.5 VDC/26VAC Lights

066-3060-13 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 -00 -01 -02 -03

006-00540-0000 Bulletin 1 1 1 1

073-00044-0001 Mooring Plate 1 1 1 1

073-00045-0000 Black Adapter Plate 1 0 1 0

073-00045-0001 Gray Adapter Plate 0 1 0 1

Table 1-3 - KNI 582 RMI Installation Kit

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KNI 582

PART NUMBER DESCRIPTION -00 -01 -02 -03

089-05115-0012 Scr. FHP 6-32 x 3/4 4 0 4 0

089-06461-0012 Scr. FHP 6-32 x 3/4 0 4 0 4

030-01157-0011 Socket Crmp 20G 0 0 49 49

030-01176-0000 HSG Conn 50S 0 0 1 1

030-01188-0000 Pin Polrzin Female 0 0 1 1

030-02350-0015 Conn Sub-Min F 50P 1 1 0 0

030-02414-0001 Hood & Lvr Mdfd 1 1 1 1

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

KR 87 TSO'd KCS 55/55A TSO'd

NAV AC 90-45A

KNS 81: Area NAV AC 90-45A KDF 800 TSO’d KPI 550 TSO’d

KX 155/165: TSO’d KDF 805 TSO’d

KX 170B: Non-TSO’d KDF 8000 TSO’d

KX 175B: TSO’d

KNR 615: TSO’d

KNR 630: TSO’d

KNR 634: TSO’d

KNR 665: Area NAV AC 90-45

KNR 665A: 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:

A. 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.

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 1-6

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.

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-2

TEST DATA

Compass Card Accuracy

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

ADF (D.C. SIN/COS) Accuracy

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

ADF (X, Y, and Z) Accuracy

KNI 582

(±2° Max.)

(±2° Max.)

(±5° Max.)

(±5° Max.)

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

VOR (OBI DIGITAL) Accuracy

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

VOR (Composite) Accuracy

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

VOR (OBI SIN/COS) Accuracy

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

(±5° Max.)

(±5° Max.)

(±5° Max.)

(±5° Max.)

(±5° Max.)

(±5° Max.)

(±5° Max.)

(±5° Max.)

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KNI 582

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-4

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-5

KNI 582

Figure 2-1 KNI 582 Outline and Mounting Drawing

(Dwg No 155-05353-0000, Rev 0)

KNI 582

Figure 2-2 Connector Assembly

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-7

KNI 582

Figure 2-3 KNI 582 Pin Functions

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-8

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permi ssion of Honeywell. 2-9

KNI 582

Figure 2-4 KNI 582/KDF 805/KNR 665A/KNR 615 Interconnect

(Dwg No 155-01383-0000, Rev 5)

KNI 582

Figure 2-5 KNI 582/KDF 805/KNR 630 Interconnect

(Dwg No 155-01384-0000, Rev 5)

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permi ssion of Honeywell. 2-11

KNI 582

Figure 2-6 KNI 582/KR 87/KNS 81/KN 53 Interconnect

(Dwg No 155-01385-0000, Rev 4)

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permi ssion of Honeywell. 2-13

KNI 582

Figure 2-7 KNI 582/Bendix DF-2071A/Bendix CN2011A/

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

(Dwg No 155-01386-0000, Rev 5)

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permi ssion of Honeywell. 2-15

KNI 582

Figure 2-8 KNI 582 Cable Assembly

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

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-17

KNI 582

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 2-18

Rev 3, March/2007 ©Honeywell In ternational Inc. Do not print without express permission of Honeywell. 2-19

KNI 582

Figure 2-10 KNI 582 Serial OBI Interface

(Dwg No 155-01563-0013, Rev 0)

SECTION 3

OPERATION

3.1 GENERAL

The KNI 582 RMI display is discussed below:

A. Compass Card/Lubber Line: This rotating card repeats gyro stabilized

magnetic compass information. Aircraft
heading is read from the compass card
under the orange lubber line.

B. Compass Flag: 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.

KNI 582

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.

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 3-1

KNI 582

Figure 3-1 KNI 582 Control Functions

Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 3-2