the aztalan group LLC.

TESTING REQUIREMENTS FOR AIRBORNE APPLICATIONS

 

RTCA DO-160G ENVIRONMENTAL

Section 4 Temperature and Altitude

Section 5 Temperature Variation

Section 6 Humidity

Section 7 Operational Shocks and Crash Safety

Section 8 Vibration

Section 9 Explosive Atmosphere

Section 10 Waterproofness

Section 11 Fluid Susceptibility

Section 12 Sand and Dust

Section 13 Fungus

Section 14 Salt Fog

Section 24 Icing

Section 26 Fire and Flammability

 

RTCA DO-160G ELECTROMAGNETIC

Section 15.0 – Magnetic Effect

Section 16.0 – Power Input

Section 17.0 – Voltage Spike

Section 18.0 – Audio Frequency Conducted Susceptibility – Power Inputs

Section 19.0 – Induced Signal Susceptibility

Section 20.0 – Radio Frequency Susceptibility (Radiated and Conducted)

Section 21.0 – Emission of Radio Frequency Energy

Section 22.0 – Lightning Induced Transient Susceptibility

Section 23.0 – Lightning Direct Effects

Section 25.0 – Electrostatic Discharge (ESD)

 

 

BOEING AH-64

 

 

A320 AIRBUS

 

 

787  BOEING DREAMLINER

 

BFG STORM SCOPE

 

 

LOCKHEED C130 UPGRADE

 

AUSTRAILIAN AIRFORCE PC-7

 

HORIZONTAL SITUATION

I           NDICATOR