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
