89000109-002 xVue Touch Installation Manual
Rev 2 Page 7-3
© Honeywell International Inc. Do not copy without express permission of Honeywell.
For Use in Non-Certified Aircraft
(1) Set the BARO to 29.92 IN or 1013 HPA.
(2) Set the pitot/static tester to an altitude listed in 14 CFR Part 43 Appendix E Table 1, such that the
altitude is at least 3,000 ft. or more above the field elevation at a rate of 500 feet per minute
(fpm).
(3) Validate that the VSI needle shows a rate of 500 fpm climb.
(4) Set ground conditions on the pitot/static tester and perform the applicable test points.
(5) When the altitude set in the pitot/static tester is achieved and stabilized, verify that the KSD
100EXP altitude tape and standby altimeter display the same altitude as the pitot/static tester ±
the tolerance listed in 14 CFR Part 43 Appendix E Table 1.
The test tolerance values from 14 CFR Part 43 Appendix E Table 1 are listed in Table 7-1 for reference.
Table 7-1 Test Tolerance from 14 CFR Part 43 Appendix E Table 1
Altitude Equivalent Pressure
(Inches of Mercury)
Tolerance ± (Feet)
−1,000 31.018 20
0 29.921 20
500 29.385 20
1,000 28.856 20
1,500 28.335 25
2,000 27.821 30
3,000 26.817 30
4,000 25.842 35
6,000 23.978 40
8,000 22.225 60
10,000 20.577 80
12,000 19.029 90
14,000 17.577 100
16,000 16.216 110
18,000 14.942 120
20,000 13.75 130
22,000 12.636 140
25,000 11.104 155
30,000 8.885 180
35,000 7.041 205
40,000 5.538 230
45,000 4.355 255
50,000 3.425 280
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