Lynx NGT-9000s
Installation Manual
DESCRIPTION
SECT.
NO.
CAT.
DESCRIPTION
O
per
at
iona
l S
hoc
ks
and
C
ras
h S
af
et
y
Operational Shocks
7.2
B
3 shocks of 6g for 11 mS.
Crash Safety
7.3
B
One 20g Impulse shock in both directions
of each orthogonal axis for a total of 6 shocks.
Sustained Aircraft Type 5 (Helicopter and All Fixed-
Wing)
Test Type R (Random Orientation) per Table 7-1 of
DO-160F.
Vibration
8
S
Fixed Wing, Curve M, Sine
R
Robust Fixed Wing, Curves B & B1, Random
U2
Rotorcraft, Curve F and F1
Explosive Atmosphere
9
X
Not Applicable, Not Tested.
Waterproofness
10
X
Not Applicable, Not Tested.
Fluids Susceptibility
11
X
Not Applicable, Not Tested.
Sand and Dust
12
X
Not Applicable, Not Tested.
Fungus Resistance
13
X
Not Applicable, Not Tested.
Salt Spray
14
X
Not Applicable, Not Tested.
Magnetic Effect
15
Z
<0.3m for deflection of D
c
.
Power Input
16
BXX 14V and 28V DC inputs
Voltage Spike
17
A
600 V/2
µ
s from 50
Ω
source impedance
Audio Frequency
Conducted Susceptibility
18
Z
Engine driven alternator / generator with battery.
Induced Signal
Susceptibility
19
ZC
Interference free operation
RF Susceptibility
(Radiated and Conducted)
20
TT
Page B-2
Appendix B
0040-17001-01
January 15, 2015
Revision A
