INTEGRA ARINC e-NAV
DESCRIPTION, INSTALLATION,
OPERATION MANUAL
PAGE: 11 of 14
REF.: DOC13033
INDEX: B
DATE: SEP 14/2016
© Orolia S.A.S.
6.3. Environmental Characteristics
ENVIRONMENTAL CATEGORIES FORM FOR INTEGRA e-NAV ARINC
Qualification
Tests Title
ED62A references
(when applicable)
DO-160F
Section
Category
Temperature / Altitude
ED-62A (SPECIAL) Class1 4.0
As per ED-62A
Low Temperature
ED-62A (SPECIAL) -40°C
4.5.1
As per ED-62A
High Temperature
Activation
ED-62A (SPECIAL) +55°C
4.5.2 /3
As per ED-62A
In Flight Loss of Cooling
N/A
4.5.4
X
Altitude
ED-62A (SPECIAL) 50,000
ft
4.6.1
As per ED-62A
Decompression
ED-62A (SPECIAL)
4.6.2
As per ED-62A
Overpressure
§ 4.4.3 / ED-62A
4.6.3
As per ED-62A
Temperature variation
5
B
Humidity
6
C
Ops. shocks and crash
safety
ED-62A (SPECIAL)
7
As per ED-62A
Vibrations
Fixed Wings
8
R (C&C1)
Helicopters
U(G)
(1)
Explosion proofness
N/A
9
X
Waterproofness
10
R
Fluid susceptibility
N/A
11
X
Sand and dust
N/A
12
X
Fungus
N/A
13
X
Salt spray
14
S
Magnetic effect
15
A
Power input
16
Z
Voltage spike conducted
susceptibility
17
A
Audio frequency
conducted susceptibility
18
Z
Induced signal
susceptibility
19
ZC
Radio frequency
susceptibility
20
Conducted: T
Radiated: L
Radio frequency
emission
21
H
Lightning transient
susceptibility
22
A2G33
Lightning direct effects
N/A
23
X
Icing
N/A
24
X
ESD
25
A
Fire, Flammability
ED-62A (SPECIAL FLAME) 26
As per ED-62A
Summary of Contents for INTEGRA ARINC e-NAV
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