BENDIXKing KLR 10 Guida utente

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Publication Number D201305000058, Revision 3 Initial 19 Jul 2013

Revised 19 Nov 2014

9201-B San Mateo Blvd

N.E.

Albuquerque, New Mexico 87113 U.S.A. CAGE:

6PC31

U.S.A.

CAGE: 6PC31

Telephone: 1 - 855-250-7027 (Toll Free U.S.A./Canada)

Telephone: 1-505-903-6148 (International Direct)

Website:

www.bendixking.com/support

System Installation

Manual

KLR 10 Lift Reserve

Indicator

Part Number CAGE

89000008-001001

89000008-001002

89000008-001003

89000008-001004

89000008-001005

6PC31

Legal Notice

Export Control

This document contains technical data and is subject to U.S. export regulations. These commodities,

technology, or software were exported from the United States in accordance with the export administration

regulations. Diversion contrary to U.S. law is prohibited.

ECCN: 7E994.

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19 Nov 2014

BendixKing by Honeywell

9201-B San Mateo Blvd. NE

Albuquerque, New Mexico 87112

Product Registration

For product registration go to BendixKing.com or call our customer support number below.

Customer Support

US and Canada - 1.855.250.7027

International – 1.505.903.6148

bendixking.com/support

At BendixKing we value your opinion and we are listening. For comments about this guide, please email

techsupport@bendixking.com.

Reproduction of this publication or any portion thereof by any means without the express written

permission of Honeywell International Inc. is prohibited. See Appendix for complete terms and conditions.

The information contained in this manual is for reference only. If any information

contained herein conflicts with similar information contained in the Airplane Flight

Manual, the information in the Airplane Flight Manual shall take precedence.

System Installation Manual - KLR 10 Lift Reserve Indicator

Pub. No. D201305000058 Record of Revisions

19 Nov 2014 Page RR-1

Revision History and Instructions

Manual System Installation Manual - KLR 10 Lift Reserve Indicator

Revision 3

Summary Complete revision to install and calibration instructions for clarity.

Manual System Installation Manual - KLR 10 Lift Reserve Indicator

Revision 2

Summary Technical changes to different sections.

Updated manual to comply with FAA Memo AIR100-14-110-PM01 requirements.

Manual System Installation Manual - KLR 10 Lift Reserve Indicator

Revision 1

Summary Revised footers.

Manual System Installation Manual - KLR 10 Lift Reserve Indicator

Revision -

Summary This is a new release.

System Installation Manual - KLR 10 Lift Reserve Indicator

Record of Revisions Pub. No. D201305000058

Page RR-2 19 Nov 2014

Record of Revisions

REVISION

NUMBER

REVISION

DATE

- JULY, 2013

1 JULY, 2013

2 FEBRUARY, 2014

3 NOVEMBER, 2014

System Installation Manual - KLR 10 Lift Reserve Indicator

Pub. No. D201305000058 Table of Contents

19 Nov 2014 Page TC-1

Table of Contents

Section ................................................................................................................................................Page

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

1.1 READ ME FIRST!! .......................................................................................................................... 1-1

Probe Placement............................................................................................................................. 1-1

Calibration ....................................................................................................................................... 1-2

1.2 Objective ......................................................................................................................................... 1-4

1.3 References...................................................................................................................................... 1-4

1.4 Revisions......................................................................................................................................... 1-4

1.5 Technical Support ........................................................................................................................... 1-4

1.6 Warranty Information....................................................................................................................... 1-4

1.7 Available Kits and Components ...................................................................................................... 1-5

1.8 System Description ......................................................................................................................... 1-6

1.9 Restrictions and Limitations ............................................................................................................ 1-7

1.10 KLR 10 Main Component Details.................................................................................................... 1-8

KLR 10 Indicator ............................................................................................................................. 1-8

KLR 10 Flush Panel Mounting Kit (Mount Option 1)....................................................................... 1-8

KLR 10 Swivel Mount Kit (Mount Option 2) .................................................................................... 1-9

KLR 10 Interface Module (IF Module)............................................................................................. 1-9

KLR 10 AOA Probe....................................................................................................................... 1-10

Blue and White Hose Kit ............................................................................................................... 1-11

1.11 ASTM F3011 Compliance Statement ........................................................................................... 1-11

1.12 Instructions for Continued Airworthiness ...................................................................................... 1-11

2PLANNING.......................................................................................................................................... 2-1

2.1 Preparation...................................................................................................................................... 2-1

2.2 Establish the Location for the KLR 10 Lift Reserve Indicator ......................................................... 2-1

2.3 Establish the Location for the IF Module ........................................................................................ 2-2

2.4 Establish the Location for the AOA probe....................................................................................... 2-2

2.5 Establish a Plan to Route the Sense Lines..................................................................................... 2-4

2.6 Establish a Plan for the Electrical Power ........................................................................................ 2-4

2.7 Optional Probe Heat Installation ..................................................................................................... 2-4

3INSTALLATION.................................................................................................................................. 3-1

3.1 Installation Of the Probe Mounting Plate ........................................................................................ 3-1

3.2 Installation Of the Sense Lines ....................................................................................................... 3-1

3.3 Install Wiring, Switch & Circuit Breaker for KLR 10 ........................................................................ 3-2

3.4 Install Wiring, Switch & Circuit Breaker for Probe Heat.................................................................. 3-3

3.5 Install the KLR 10 Swivel Mount (Optional) .................................................................................... 3-4

Glareshield Mounting Instructions................................................................................................... 3-4

3.6 Installation Of the KLR 10 Indicator ................................................................................................ 3-6

3.7 Installation Of the IF Module ........................................................................................................... 3-6

3.8 Installation Of AOA Probe............................................................................................................... 3-8

3.9Inspect the KLR 10 Installation ..................................................................................................... 3-11

4SETUP AND CALIBRATION.............................................................................................................. 4-1

4.1 Definitions: ...................................................................................................................................... 4-1

4.2 Theory of Operation: ....................................................................................................................... 4-2

4.3 On The Ground Zero Pressure Calibration..................................................................................... 4-3

Failure to Complete Zero Pressure Ground Calibration ................................................................. 4-3

4.4 Set Brightness of the KLR 10 Indicator (optional)........................................................................... 4-4

4.5 Master Volume Set.......................................................................................................................... 4-5

4.6 Calibration Flight Overview ............................................................................................................. 4-6

Pre-Flight Overview: Determine Set Points .................................................................................... 4-6

System Installation Manual - KLR 10 Lift Reserve Indicator

Table of Contents Pub. No. D201305000058

Page TC-2 19 Nov 2014

Table of Contents (cont)

Section ................................................................................................................................................ Page

In-Flight Overview............................................................................................................................4-6

4.7 In-Flight Optimum Alpha Angle (OAA) calibration...........................................................................4-8

Invalid Set Points.............................................................................................................................4-9

4.8 In-Flight Cruise Set Point Calibration ............................................................................................4-10

4.9 Exiting the Calibration Mode..........................................................................................................4-11

4.10 Completing the Calibration ............................................................................................................4-11

4.11 Post Calibration Testing ................................................................................................................4-12

5APPENDIX...........................................................................................................................................5-1

5.1 Acronyms and Abbreviations...........................................................................................................5-1

5.2 IF Module Connectors Pin Definitions .............................................................................................5-2

5.3 AOA Probe Angles ..........................................................................................................................5-3

Positive Probe Lock System............................................................................................................5-3

5.4 KLR 10 Indicator Controls ...............................................................................................................5-4

5.5 Operational and Environmental Limitations.....................................................................................5-4

5.6 Honeywell-Confidential....................................................................................................................5-5

5.7 Copyright - Notice............................................................................................................................5-6

System Installation Manual - KLR 10 Lift Reserve Indicator

Pub. No. D201305000058 Table of Contents

19 Nov 2014 Page TC-3

List of Illustrations

Figure Page

Figure 1-1: Install Probe Outside Propeller Arc......................................................................................... 1-1

Figure 1-2: AOA Location on Wing............................................................................................................ 1-2

Figure 1-3: Location to Enlarge Mounting Plate Slot................................................................................. 1-2

Figure 1-4: KLR 10 Indicator...................................................................................................................... 1-8

Figure 1-5: KLR 10 Flush Panel Mounting Kit ........................................................................................... 1-8

Figure 1-6: KLR 10 Swivel Mount.............................................................................................................. 1-9

Figure 1-7: KLR 10 Interface Module ........................................................................................................ 1-9

Figure 1-8: AOA Probe Sensor Fittings ................................................................................................... 1-10

Figure 1-9: AOA Probe and Mounting Plate ............................................................................................ 1-10

Figure 1-10: Blue and White Hose Kit ..................................................................................................... 1-11

Figure 2-1: AOA Probe in Wing ................................................................................................................. 2-3

Figure 3-1: Mounting Plate Alignment ....................................................................................................... 3-1

Figure 3-2: Swivel Mount on Glareshield................................................................................................... 3-4

Figure 3-3: Swivel Mount Template........................................................................................................... 3-4

Figure 3-4: Swivel Mount Instructions - Step 1.......................................................................................... 3-5

Figure 3-5: Swivel Mount Instructions - Step 2.......................................................................................... 3-5

Figure 3-6: Swivel Mount Instructions - Step 3.......................................................................................... 3-5

Figure 3-7: Sense Line Quick Release Fittings ......................................................................................... 3-7

Figure 3-8: KLR 10 Interface Module Sense Line Connectors.................................................................. 3-7

Figure 3-9: KLR 10 Interface Module Electrical Connectors ..................................................................... 3-8

Figure 3-10: AOA Probe Pin Positions-Left Side....................................................................................... 3-8

Figure 3-11: AOA Probe Pin Positions-Right Side .................................................................................... 3-9

Figure 3-12: Position of Probe Lock Plate at 50° Index Hole .................................................................... 3-9

Figure 3-13: Enlarging Mounting Plate Hole............................................................................................ 3-10

Figure 3-14: AOA Probe Connectors....................................................................................................... 3-10

Figure 4-1: Master Volume Controls.......................................................................................................... 4-5

Figure 4-2: OAA Set Point Flowchart ...................................................................................................... 4-14

Figure 4-3: Cruise Set Point Flowchart.................................................................................................... 4-15

Figure 5-1: Right Side Angles.................................................................................................................... 5-3

Figure 5-2: Left Side Angles ...................................................................................................................... 5-3

Figure 5-3: KLR 10 Indicator Controls ....................................................................................................... 5-4

System Installation Manual - KLR 10 Lift Reserve Indicator

Table of Contents Pub. No. D201305000058

Page TC-4 19 Nov 2014

List of Tables

Table Page

Table 1-1: Available Kits ............................................................................................................................1-5

Table 1-2: KLR 10 Kit Components ...........................................................................................................1-5

Table 1-3: AOA Probe Options ..................................................................................................................1-6

Table 1-4: KLR 10 Mounting Options.........................................................................................................1-6

Table 1-5: Probe Cover and Replacements...............................................................................................1-6

Table 2-1: Additional Load Formula ...........................................................................................................2-1

Table 2-2: Additional Load Formula for IF Module.....................................................................................2-2

Table 2-3: Additional Load Formula for AOA Probe ..................................................................................2-3

Table 2-4: Additional Drag Formula for AOA Probe...................................................................................2-3

Table 4-1: Indications and Annunciations During Calibration ..................................................................4-13

Table 5-1: Power Connector ......................................................................................................................5-2

Table 5-2: Auxiliary I/O Connector .............................................................................................................5-2

Table 5-3: Display Connector.....................................................................................................................5-2

System Installation Manual - KLR 10 Lift Reserve Indicator

Pub. No. D201305000058 General

19 Nov 2014 Page 1-1

CAUTION:

DO NOT POSITION THE AOA PROBE BEHIND OR NEAR THE PROPELLER ARC.

1 GENERAL

1.1 READ ME FIRST!!

Important Notes to Avoid Common Errors

Probe Placement

-PLANNING NOTE: The AOA probe must be positioned where it will be in clear, undisturbed

airflow through all normal flight maneuvers. The probe must be at least 2 feet outside the

propeller arc. It must not be downstream of any struts, tie-down rings, step-changes in the

leading edge (e.g. the end of a cuff), etc. See Figure Below and also see Section 2.4, Establish

the Location for the AOA probe.

Figure 1-1: Install Probe Outside Propeller Arc

-PLANNING NOTE: The AOA Probe is designed to be mounted at approximately 50 degrees to

the chord of the wing (see diagram below). This position balances the pressure readings between

the two pressure ports at low angles of attack. In order to achieve this, the probe will usually need

to be adjusted so that the angle between the leading edge of the probe and the plate is less than

50 degrees, especially when mounting the probe behind the maximum thickness of the wing. See

Section 3.1, Installation Of the Probe Mounting Plate.

-INSTALLATION NOTE: The probe has a convenient reference line on it where the cross section

changes from rectangular to wedge shaped. When this “Chord Marker” line is parallel to the

plate, the probe is at 50 degrees to the plate. Therefore, the Chord Marker should end up being

parallel to the wing chord (not the bottom surface of the wing). Angle the Probe so that the Chord

Marker is Parallel to the Chord of the Wing. See Section 2.4, Establish the Location for the AOA

probe.

System Installation Manual - KLR 10 Lift Reserve Indicator

General Pub. No. D201305000058

Page 1-2 19 Nov 2014

Figure 1-2: AOA Location on Wing

-INSTALLATION NOTE: It may be necessary to enlarge the slot in the plate in order to set the

probe at the correct angle. For many installations using the standard plate, the probe must be

swept forward 10 degrees or more. This may require removing some material from the plate so

that the probe may be mounted at the proper angle. This is as designed and keeps the hole in

the plate as small as possible for different installations.

Figure 1-3: Location to Enlarge Mounting Plate Slot

-INSTALLATION NOTE: The probe has detents that allow the angle to be changed in 5 degree

increments. The position of the blue locking plate determines which probe angle detent is

engaged. One side of the probe has detents that allows 10 degree angles – e.g. 30, 40, 50, 60,

etc.. The other side of the probe has detents that provide the 5 degree angles – e.g. 35, 45, 55,

65, etc. The blue locking plate will need to be positioned on either the left or right side of the

probe and with the locking pin either forward or aft, depending on the detent required. See

Section 3.8, Figure 3-10 and Figure 3-11.

Calibration

-CALIBRATION WARNING: On certified aircraft, the KLR 10 system should be calibrated to be

slightly conservative to the certificated stall warning system. This means that the final KLR 10

visual (flashing red down arrow) and aural (“Too Slow! Too Slow!” annunciation) should occur just

before the aircraft stall warning system activates.

Remove

material at this

location only

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