B. kni 415/416 indicator, B. kni 415/416 indicator -8 – Honeywell KA 54 User Manual

Page 34

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KRA 405B RADAR ALTIMETER INSTALLATION MANUAL

Page 2-8

006-10536-0010 Rev. 10

Oct/2005

c.

For direct mounted units perform the following steps:

1.

Mark, punch, then drill mounting holes, being

careful not to damage adjacent equipment or ca-

bles.

2.

Using four (4) #6-32 screws, secure the unit in

the position selected.

(2)

Dual Installation

The KRA 405B R/T fulfills all altitude accuracy specifications

when in dual installation mode. Mutual interaction is not

operationally significant. See

FIGURE 2-7 DUAL RADAR ALTIM-

ETER SYSTEM TYPICAL ANTENNA INSTALLATIONS

.

The secondary unit in a dual installation is selected by a

hardware strap as described in Note 3 of

FIGURE 2-17 KRA 405B

RADAR ALTIMETER SYSTEM INTERCONNECT

.

NOTE:

The operation of the primary unit is no different

than the operation of a unit in a single radar al-

timeter installation.

(3)

Zero Feet Calibration

The KRA 405B Receiver/Transmitter DOES NOT require an AID.

The KRA 405B R/T has provisions to calibrate to zero (0) feet

during installation, such that the radar altitude is 0 feet

when the aircraft is taxiing or stationary on the ground. Re-

fer to section 2.6.

A. POST INSTALLATION CALIBRATION

for the

calibration procedure.

There are provisions to allow the indicated 0 foot point to

be offset from the calibrated 0 foot point to accommodate in-

stallations where the indicator reads 0 feet at the point the

wheels first touch down. The offset is then stored in a con-

figuration module.

B.

KNI 415/416 INDICATOR

(1)

Plan a location on the aircraft panel that is clearly visible

to the pilot with the least deviation from his normal scan

pattern while in an approach.

(2)

Avoid mounting the unit close to heater vents or other high

heat sources.

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