User's Manual

UL-801 Installation Manual
Page 110
23-20-06 15 December 2011
ENVIRONMENTAL QUALIFICATION FORM
NOMENCLATURE Configuration Module
PART NO. 108009
TSO NUMBER TSO-C160
MANUFACTURER
Universal Avionics Systems Corporation
3260 East Universal Way
Tucson, AZ 85756-5097
Conditions
DO-160F
Section #
Category Description of Conducted Tests
Temperature and Altitude 4 A2 E1
Inside or outside pressure vessel
−55°C to +70°C
Maximum altitude—70,000 feet
For the E1 levels that, per RTCA/DO-160F, are declared
by the manufacturer, the corresponding levels for A2 are
used.
In-Flight Loss of Cooling 4.5.4 X There is no fan on this product.
Temperature Variation 5 B
Equipment in non-temperature controlled area of
airplane.
5 degrees/minute
Humidity 6 A Standard humidity
Operational Shocks and
Crash Safety
7 B, E
Equipment in fixed-wing and helicopters tested for
operational shock and safety.
Vibration 8 S Test category S—Standard
Explosion Atmosphere 9 H
Equipment H—including hermetically sealed, contains
hot spot surfaces and non-spark producing.
Environment 2—atmosphere where flammable mixture
exist only because of spillage or leakage.
Waterproofness 10 W
Equipment subjected to falling water in course of normal
airplane operations.
Fluids Susceptibility 11 X
Not tested—Fluid contamination not commonly
encountered.
Sand and Dust 12 X Not tested—Not subject to blowing sand and dust.
Fungus Resistance 13 X
Not tested—Equipment not exposed to severe fungus
contamination.
Salt Fog 14 X
Not tested—Equipment not subjected to salt
atmosphere.