BendixKing KLR 10 - Manual (Page 8)

KLR 10 Pilot’s Guide
Introduction P/N D201306000109
Page 1-2 Rev 1 Feb 2014
The KLR 10 draws a minimal current of less than approximately ¼
amp (250mA) of electrical power. For the system to operate
correctly, it must be supplied electrical power within a range of 12 to
28VDC and be calibrated correctly.
The AOA probe must be kept clear of any obstructions and be
mounted securely, in clean air flow. The final AOA probe to wing
angle will be determined by the amount the bottom of the wing varies
from parallel to the cord of the wing. For most aircraft, the starting
angle is 50 degrees from the leading edge of the AOA probe
mounting plate. The KLR 10 system will adjust for differences within
a limited electrical signal range. AOA Probe angle readjustment
may be needed to allow for full scale electronic calibration.
Probe heat is an option, and if installed, requires less than 8 amps of
electrical power at 12 or 24VDC to operate. To extend the life of the
probe heat element, it is recommended that the probe heat not be
used for prolonged periods while on the ground.
The KLR 10, when properly calibrated in accordance with the
BendixKing KLR 10 Installation Manual part number
D201305000058, will have an accuracy of ±3% over the full scale of
the calibration. This accuracy is maintained over a sideslip range of
±15 degrees.
1.3 RESTRICTIONS AND LIMITATIONS
The KLR 10 Lift Indicator is non-required and is to be used only as
supplemental information to the pilot.
The KLR 10 Lift Indicator may not be used as a substitution for the
certified aircraft stall warning system.
No operational credit may be taken for such items as reduced
approach speed and shorter landing distances.