BENDIXKing XVUE TOUCH Installation Manual page 172

(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
−1,000
0
500
1,000
1,500
2,000
3,000
4,000
6,000
8,000
10,000
12,000
14,000
16,000
18,000
20,000
22,000
25,000
30,000
35,000
40,000
45,000
50,000
89000109-002
Rev 2
© Honeywell International Inc. Do not copy without express permission of Honeywell.
For Use in Non-Certified Aircraft
Equivalent Pressure
(Inches of Mercury)
31.018
29.921
29.385
28.856
28.335
27.821
26.817
25.842
23.978
22.225
20.577
19.029
17.577
16.216
14.942
13.75
12.636
11.104
8.885
7.041
5.538
4.355
3.425
Tolerance ± (Feet)
20
20
20
20
25
30
30
35
40
60
80
90
100
110
120
130
140
155
180
205
230
255
280
xVue Touch Installation Manual
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