89000109-002
xVue Touch Installation Manual
Rev 2
Page 7-2
© Honeywell International Inc. Do not copy without express permission of Honeywell.
For Use in Non-Certified Aircraft
7.2.1 Attitude Checkout
Attitude checkout was performed as outlined in Section 6.4.2 Magnetometer Compensation when the
airplane was leveled in pitch and roll or at known pitch and roll angles, the KSD 100EXP pitch and roll
attitude were visually matched to the known angles. Refer to Section 6.3 KG 71EXP Configuration
(ADAHRS) and Section 6.4 KMG 7010/MD32 Calibration (Magnetometer) for the initial heading checkout
completed with the xVue Touch System setup.
7.2.2 Heading Checkout
Heading checkout was performed as outlined in Section 6.4.2 Magnetometer Compensation using an
airport compass rose or a landing compass with an accuracy of ± 2 degrees for airplane orientation. The
heading value displayed on the PFD should be within ± 2 degrees of the airplane’s orientation.
7.2.3 Leak Test
Using the instructions provided in the airplane maintenance manual or with the pitot/static tester,
connect the tester to the airplane pitot static system and perform a leak check of the system. This may be
conducted concurrently with the Altitude Display/Vertical Display Checkout.
7.2.4 Altitude Display/Vertical Display and Standby Altimeter Checkout
The following procedure requires the pitot/static tester be connected to the airplane pitot static system
using the instructions provided in the airplane maintenance manual or with the tester. This may be
conducted concurrently with the Leak Test.
CAUTION
DO NOT, AT ANY TIME, EXCEED THE MAXIMUM VALUES OF AIRSPEED, VERTICAL SPEED,
AND ALTITUDE ESTABLISHED IN THE AIRPLANE AFM OR POH. EXCEEDING MAXIMUM
VALUES COULD DAMAGE THE KFD 900 SYSTEM OR ANY OF THE INSTRUMENTS
CURRENTLY INSTALLED.
CAUTION
DO NOT, AT ANY TIME, EXCEED THE MAXIMUM CAPABILITY FOR THE XVUE TOUCH
SYSTEM EQUIPMENT, AS DOCUMENTED IN SECTION 2.5 ENVIRONMENTAL
QUALIFICATION FORM (EQF).
CAUTION
SOME TEST POINTS LISTED IN TABLE 7-1 MAY EXCEED THE CAPABILITY OF SPECIFIC
AIRPLANES. TO AVOID HARMING INSTALLED EQUIPMENT, DO NOT EXCEED THE AIRPLANE
SERVICE CEILING AND MAXIMUM AIRSPEED SPECIFIED IN THE AFM OR POH.
NOTE
COMPLETE A PITOT AND STATIC LEAK CHECK PRIOR TO ANY ALTITUDE AND AIRSPEED
CHECKS.
