Honeywell BENDIX KING KMH 880 System Installation Manual page 251

B B B B
Power Input
Voltage Spike Conducted
Audio Frequency Conducted Susceptibility
Induced Signal Susceptibility
Radio Frequency Susceptibility
Radio Frequency Emission
Lightning Induced Transient Susceptibility
Lightning Direct Effects
Icing
ESD
Notes:
1. Vibration Critical Frequencies – The following critical frequencies are mechanical resonances of the unit under
test that have peak acceleration amplitudes greater than twice the input acceleration amplitude. Observed
changes in performance of the unit under test are to be determined (TBD).
Vertical
(Top to Bottom)
TBD
2. Observed changes in the above resonant frequencies during the test are to be determined.
3. The unit shall comply with DO-160C, vibration category N and Y for helicopters.
4. RF susceptibility degradation information placed here if applicable.
5. The unit shall comply with A3E3 on all signal lines and A4E4 on the power leads.
Honeywell International Inc.
Environmental Qualification Form
TSO-4
16.0
17.0
18.0
19.0
20.0
21.0
22.0
23.0
24.0
25.0
Longitudinal
(Front to Back)
TBD
10609I00.ZIPCDL
KMH 880/KTA 870
Category BZ
Category A
Category BZ
Category A
Category RRR (See Note 4)
Category L
Category A3E3 (See note 5)
Category 1B
Category X (Not Tested)
Category A
Lateral
(Side to Side)
TBD
P/N 004-02050-4800
Rev 0, October/2000
Revision -