BENDIXKing KLR 10 User guide

Page T-1
Publication Number D201305000058, Revision 3 Initial 19 Jul 2013
Revised 19 Nov 2014
© Honeywell International Inc. Do not copy without express permission of Honeywell.
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: [phone] (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
6PC31
6PC31
6PC31
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.

Page T-2
19 Nov 2014
© Honeywell International Inc. Do not copy without express permission of Honeywell.
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
[e-mail].
COPYRIGHT NOTICE
© 2013, 2014, BendixKing by Honeywell. All rights reserved.
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

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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

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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

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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
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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
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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

System Installation Manual - KLR 10 Lift Reserve Indicator
Pub. No. D201305000058 General
19 Nov 2014 Page 1-3
-CALIBRATION NOTE: There are three calibration set points for the KLR 10. The ZERO set
point, the OAA set point, and the CRUISE set point. The ZERO set point is done ONE TIME
immediately after installation while the aircraft is in the hangar with no air movement over the
probe. When the ZERO set point is created, ALL other calibration points are removed and must
be reset. See Section 4.3.
-CALIBRATION NOTE: The OAA and CRUISE set points can be entered as often as desired or
necessary without resetting the ZERO set point. The system is designed to easily change the
OAA and CRUISE set points when desired as the owner gains experience with the system. It is
normal to change the OAA and CRUISE set points several times to get the system indications as
desired.
-CALIBRATION NOTE: For the OAA Set Point: Calculate the expected Vs (clean wing stall
speed) for the loading and environmental conditions during the calibration flight. Then multiply
that Vs Indicated Air Speed (IAS) by 1.3. This 1.3Vs IAS is the target airspeed to fly the aircraft
trimmed for straight and level, non accelerating flight for the OAA set point. If your aircraft Pilot
Operating Handbook (POH) does not have performance information for calculating 1.3Vs based
on the actual calibration flight weight and atmospheric conditions, use the POH Vs (bottom of the
green arc) multiplied by 1.3. In this case, try to fly the calibration flight as near gross weight as
possible as this is the loading condition for which the POH Vs is calculated. At NO time is a stall
required during calibration. See Section 4.6.
-CALIBRATION NOTE: For the Cruise Set Point: Calculate the Maneuvering Speed (Va)
correcting for the current aircraft loading and atmospheric conditions. This Va IAS is the target
airspeed to fly the aircraft trimmed for straight and level, non accelerating flight for the CRUISE
set point. If your aircraft’s POH does not have performance information for calculating Va for the
aircraft loading and atmospheric conditions during the calibration flight, use the Va in the POH
and fly the calibration flight as close to gross weight as possible. See Section 4.6.
-CALIBRATION NOTE: There are two common set point errors encountered when attempting to
set the OAA and CRUISE set points during the calibration flight. Both of these errors are due to
the AOA probe being set at the wrong angle relative to the airflow, resulting in an out-of-range
differential pressure reading between the two ports.
oINVALID SET POINT –Too Low: The system will announce “Invalid Set Point” and flash
the BOTTOM RED bar and the TOP of the BLUE donut . This means
that the probe angle is too small and should be INCREASED by at least 5 degrees. See
Section 4.7.
oINVALID SET POINT –Too High: The system will announce “Invalid Set Point” and flash
the TOP YELLOW bar and the BOTTOM of the BLUE donut . This
means that the probe angle is too large and should be DECREASED by at least 5
degrees. See Section 4.7.
oNOTE: Remember that the CHORD MARKER is designed to be nearly parallel to the
CHORD LINE of the wing, NOT the bottom surface of the wing.
oNOTE: Remember that the blue locking plate on the probe can be mounted in one of four
directions (left or right of probe, pin forward or aft) in order to capture the probe detents at
5 degree increments.
-CALIBRATION NOTE: After successfully calibrating the KLR 10 system, gain some experience
with the system indications and performance through normal flight maneuvers and regimes. If
you feel that the indications and warnings are happening too soon or too late, perform the OAA
and CRUISE set point calibration steps again.

System Installation Manual - KLR 10 Lift Reserve Indicator
General Pub. No. D201305000058
Page 1-4 19 Nov 2014
1.2 OBJECTIVE
This manual is designed to guide the installer and user through the planning, installation, documentation
and calibration of the KLR 10 Lift Reserve Indicator.
1.3 REFERENCES
For more information, we have included references with the instructions. These references may be used
as acceptable data when documenting the installation.
1.4 REVISIONS
When a revision is required of this manual, the manual will be revised in its entirety.
1.5 TECHNICAL SUPPORT
Contact BendixKing customer support lines at 1-855-250-7027 (USA & Canada) / 1-505-903-6148
(International) or [e-mail].
1.6 WARRANTY INFORMATION
Seller’s obligation and Buyer’s sole remedy under this warranty is repair or replacement, at Seller’s election, of
any Product Nonconformance. All Products repaired or replaced are warranted only for the unexpired portion of
the original warranty period.
BendixKing offers a two year warranty from date of purchase against manufacturer defect for material and
labor. After expiration of standard warranty, repair coverage will be available for a fixed fee of $200 per
occurrence until five years from date of purchase. After that, repairs are subject to parts and labor cost.
Seller assumes round trip shipping costs for Nonconforming Products in an amount not to exceed normal
surface shipping charges to and from Seller’s nearest warranty repair facility for such Products. The party
initiating transportation bears the risk of loss or damage to Products in transit. If Seller reasonably determines,
after analysis of the returned Product, that a Nonconformance does not exist, then Buyer will pay all expenses
related to the improper return including, but not limited to, analysis and shipping charges.
Seller will not be liable under this warranty for: (1) maintenance, repair, installation, handling, packaging,
transportation, storage, operation or use of Products which is improper or otherwise not in compliance with
Seller’s instruction; (2) Product alteration, modification or repair by anyone other than Seller or those
specifically authorized by Seller; (3) accident, contamination, foreign object damage, abuse, neglect or
negligence after Product shipment to Buyer; (4) damage caused by failure of a Seller supplied Product not
under warranty or by any hardware or software not supplied by Seller; (5) use of counterfeit or replacement
parts that are neither manufactured nor approved by Seller for use in Seller-manufactured Products; (6)
products not manufactured by BendixKing (but manufacturer’s warranty is passed through to Buyer to the
extent permitted); or (7) Products normally consumed in operation or which have a normal life inherently
shorter than the foregoing warranty period including, but not limited to, consumables (e.g. flashtubes, lamps,
batteries, storage capacitors). Seller has no obligation under this warranty unless Buyer maintains records that
accurately document operating time, maintenance performed and the nature of the unsatisfactory condition of
Seller’s Product. Upon Seller’s request, Buyer will give Seller access to these records for substantiating
warranty claims.
THESE WARRANTIES ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER
WRITTEN, EXPRESS, IMPLIED, STATUTORY OR OTHERWISE, INCLUDING, BUT NOT LIMITED TO, THE
IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR PARTICULAR PURPOSE. IN NO
EVENT WILL SELLER BE LIABLE FOR ANY INCIDENTAL, CONSEQUENTIAL, SPECIAL, OR INDIRECT
DAMAGES, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES AND NOTWITHSTANDING
THE FAILURE OF THE ESSENTIAL PURPOSE OF ANY LIMITED REMEDY.
NO EXTENSION OF THIS WARRANTY WILL BE BINDING UPON SELLER UNLESS SET FORTH IN
WRITING AND SIGNED BY SELLER'S AUTHORIZED REPRESENTATIVE.
Manufactured for BendixKing,
A Division of Honeywell International Inc.
Albuquerque, NM 87113, USA

System Installation Manual - KLR 10 Lift Reserve Indicator
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1.7 AVAILABLE KITS AND COMPONENTS
A complete KLR 10 SYSTEM contains one kit from Table 1-1, one AOA Probe from Table 1-3, and
one Indicator Mount from Table 1-4. There are 5 different KLR 10 kits that can be ordered from Table
1-1 that differ only in the length of the Blue and White Hose Kit and the size of the Mounting Plate. The
components for these kits are found in Table 1-2.
NOTE: The Hose Kit is comprised of two hoses, one blue and one white. This manual also refers to
these hoses as sense lines and uses these terms interchangeably.
Table 1-1: Available Kits
PART NUMBER DESCRIPTION QTY
89000008-001001 With 9 in X 9 in plate, 25 ft Hose Kit 1
89000008-001002 With 6 in Round Plate, 36 ft Hose Kit 1
89000008-001003 With 8 in Elliptical Plate, 36 ft Hose Kit 1
89000008-001004 With 3.5 in Round Plate, 25 ft Hose Kit 1
89000008-001005 With High Wing/Strut Mount, 25 ft Hose Kit 1
Table 1-2: KLR 10 Kit Components
DESCRIPTION QTY
KLR 10 Indicator 1
KLR 10 Indicator Cable 1
KLR 10 Interface Module 1
KLR 10 Interface Module Power Cable 1
KLR 10 Auxiliary Cable 1
Blue and White Hose Kit (see table 1-1 for hose lengths specific to each kit) 1
Mounting Plate (see table 1-1 for mounting plate specific to each kit) 1
Small Flat-Head Screwdriver for Calibration 1
Protractor 1
Installation Manual 1
Pilot’s Guide 1
Certificate of Conformity 1

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Table 1-3: AOA Probe Options
PART NUMBER DESCRIPTION QTY
89000008-001 Standard AOA Probe 1
89000008-543001 12 VDC Heated AOA Probe
1
89000008-544001 24 VDC Heated AOA Probe
1
Table 1-4: KLR 10 Mounting Options
The table below shows the list of optional components for the KLR 10 system:
Table 1-5: Probe Cover and Replacements
PART NUMBER DESCRIPTION QTY
89000008-684001 KLR 10 Probe Cover with Flag 1
89000008-002 Hose Kit, 36 ft (Replacement) 1
89000008-004 9 in X 9 in Mounting Plate (Replacement) 1
1.8 SYSTEM DESCRIPTION
The KLR 10 measures pressure at two points from an Angle of Attack (AOA) probe mounted to the wing
in reference to the wing chord that conveys changing pressures, via sense lines, to the KLR 10 IF
module. The IF module converts the differential pressure into an electronic signal that is transmitted
to the display indicator which then conveys the appropriate AOA or lift information to the pilot. In addition
to the visual display, the IF module also can connect to the remote audio interface by an I/O connection.
The I/O connection provides warning annunciations to the pilot’s head set.
The KLR 10 is a stand-alone system and does not interface or replace any existing instruments or
displays and is not considered essential for flight.
PART NUMBER DESCRIPTION QTY
89000008-685001 KLR 10 Flush Panel Mount 1
89000008-686001 KLR 10 Glareshield Swivel Mount 1

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1.9 RESTRICTIONS AND LIMITATIONS
1. This AOA system has not been determined to be suitable for installation in any specific aircraft by
BendixKing. It may be installed in a type-certificated aircraft, provided that it has been determined
suitable for installation by an appropriately rated mechanic by means such as field approval or as
a minor alteration.
2. Installation of the KLR 10 in a commuter or transport category airplane is prohibited!
3. Installation of the KLR 10 as a replacement for or modification to an existing approved stall
warning system is prohibited!
4. The KLR 10 is non-required and is to be used only as supplemental information to the pilot.
5. The KLR 10 may not be used as a substitution for the certified aircraft stall warning system.
6. No operational credit may be taken for such items as reduced approach speed and shorter
landing distances.
7. The KLR 10 is required to have a placard located in plain view, that is unable to be altered or
obstructed, and that must state the following phrase exactly with no changes:
"Not for use as a primary instrument for flight".

System Installation Manual - KLR 10 Lift Reserve Indicator
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1.10 KLR 10 MAIN COMPONENT DETAILS
KLR 10 Indicator
The KLR 10 Indicator is 2.35 in tall X 1.55 in wide X 1.26 in deep.
Figure 1-4: KLR 10 Indicator
KLR 10 Flush Panel Mounting Kit (Mount Option 1)
Mounting ears are included in the Flush Panel Mounting Kit that attach to either side of the KLR 10
Indicator as shown in the figure below.
Note: If the KLR 10 is ordered with the optional swivel mount, the mounting ears are not included in
the kit, but can be ordered as an optional accessory with purchase of Flush Mount Kit
89000008-685001.
Figure 1-5: KLR 10 Flush Panel Mounting Kit

System Installation Manual - KLR 10 Lift Reserve Indicator
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KLR 10 Swivel Mount Kit (Mount Option 2)
An optional mounting kit is available for a vertical swivel mount that mounts above the glareshield, see
Figure 1-6 below.
.
Figure 1-6: KLR 10 Swivel Mount
KLR 10 Interface Module (IF Module)
The IF module is 1.63 in tall X 5.81 in wide X 2.58 in deep and weighs 0.8 lbs.
Figure 1-7: KLR 10 Interface Module

System Installation Manual - KLR 10 Lift Reserve Indicator
General Pub. No. D201305000058
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Figure 1-8: AOA Probe Sensor Fittings
KLR 10 AOA Probe
The AOA Probe is mounted on a mounting plate (plate size will vary, see Table 1-1). In some installations
the mounting plate is cut to fit the existing opening.
Figure 1-9: AOA Probe and Mounting Plate
AOA Probe and 2 fittings = 0.23 lbs.
9 in x 9 in plate + hardware = 0.40 lbs (Mounting plate size may vary)
Add 0.25 lbs with an optional heated probe.

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Blue and White Hose Kit
The blue and white hoses are 25 ft or 36 ft long depending on the kit (see Table 1-1). The hoses act as
sense lines to transfer pressure information from the AOA probe sense holes (see Figure 1-9) to the
interface module. Do not remove the black caps until ready to connect hoses to IF module and AOA
Probe.
.
Figure 1-10: Blue and White Hose Kit
The blue and white hoses weigh 0.02 lbs for each foot in length.
1.11 ASTM F3011 COMPLIANCE STATEMENT
The KLR 10 Revision GAG and subsequent versions comply with all aspects of ASTM F3011-13().
1.12 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
While not required, it is recommended to verify proper operation every 24 calendar months. Operation
can be verified by determining in-flight set points OAA and Cruise compared to previous segment
indications as described in section 4: Setup and Calibration.

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