USER MANUAL
— Aircraft Interface Device
Page 11 of 13
Rosemount Aerospace Inc. Model 8730L Series
D06429976 Revision 06
UTC AEROSPACE SYSTEMS PROPRIETARY
SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE.
U.S. Export Classification: EAR: 7E994
3
CERTIFICATIONS
3.1 DO-160
The 8730L AID has been certified to operate within the following environmental conditions.
Test Description
DO-160G
Section
Test Category
Temperature and Altitude
4.5
Operating Low Temp., -40°C, Modified Cat B2
4.5
Operating High Temp., +55°C, Modified Cat B2
4.5
Short-Time Operating Low Temp., -40°C, Modified
Cat B2
4.5
Short-Time Operating High Temp., +70°C, Cat B2
4.5
Ground Survival Low Temp., -55°C, Cat B2
4.5
Ground Survival High Temp., +85°C, Cat B2
4.6.1
Steady State Altitude, 25,000 ft. Cat B2
4.6.2
Decompression, 51,000 ft. Cat A1
4.6.3
Overpressure, 170kPa (-15,000 ft.), Cat A1
Temperature Variation
5
Category B
Humidity
6
Category A Category B
Operational Shocks, Crash Safety
7
6g 11ms Shock Cat B
20g 11ms Crash Safety Impulse Cat B
20g Crash Safety Sustained Cat B
Vibration
8
Category S, Curve C Category U, Curve G
Fluid Susceptibility
11
Category F, as limited to a subset of fluids
Sand and Dust
12
Category S
Fungus Resistance
13
Category F
Magnetic Effect
15
Category Z, less than 0.3 m
Power Input
16
ZXX
Voltage Spike
17
A
Power Supply Audio Frequency Conducted Susceptibility
18
Z
Induced Signal Susceptibility
19
ZC
RF Conducted Susceptibility (10kHz
– 400MHz)
20
T
RF Radiated Susceptibility (100MHz
– 8GHz)
20
T
RF Conducted Emissions (150kHz
– 152MHz)
21
M
RF Radiated Emissions (100MHz
– 6GHz)
21
M
Lightning Indirect Effects
22
A1C1X
Electrostatic Discharge
25
A
