Bose A20 Aviation With Bluetooth Owners Guide - Page 40

FAA Technical Standards Order, Environmental categories cited refer to RTCA/DO-160F and RTCA/DO-214 - a20 aviation headset specifications

Page 40 highlights

Technical Information FAA Technical Standards Order The Bose® A20® Aviation Headset that are approved to TSO and ETSO C139 are appropriately marked. The product interface, cables, and microphones have been designed to function in or withstand exposure to the following environmental conditions: Condition Category Altitude and temperature A1 Salt fog S AF conducted susceptibility B Humidity B Magnetic effect Z Power input B RF susceptibility T Temperature and altitude A1 Vibration S, R, and U Voltage spike A Shock drop 12 times, 1 m onto concrete Explosive atmosphere Passed Environmental categories cited refer to RTCA/DO-160F and RTCA/DO-214 (March 2, 1993). The conditions and tests required for TSO approval of this are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. This device complies with FCC and ISED Canada RF radiation exposure limits for general population. It must not be collocated or operating in conjunction with any other antenna or transmitter. 40 - English

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Technical Information
40 - English
FAA Technical Standards Order
The Bose
®
A20
®
Aviation Headset that are approved to TSO and ETSO C139 are
appropriately marked. The product interface, cables, and microphones have been
designed to function in or withstand exposure to the following environmental
conditions:
Condition
Category
Altitude and temperature
A1
Salt fog
S
AF conducted susceptibility
B
Humidity
B
Magnetic effect
Z
Power input
B
RF susceptibility
T
Temperature and altitude
A1
Vibration
S, R, and U
Voltage spike
A
Shock drop
12 times, 1 m onto concrete
Explosive atmosphere
Passed
Environmental categories cited refer to RTCA/DO-160F and RTCA/DO-214
(March 2, 1993).
The conditions and tests required for TSO approval of this are minimum perfor-
mance standards. It is the responsibility of those installing this article either on or
within a specific type or class of aircraft to determine that the aircraft installation
conditions are within the TSO standards. TSO articles must have separate approval
for installation in aircraft. The article may be installed only if performed under 14
CFR part 43 or the applicable airworthiness requirements.
This device complies with FCC and ISED Canada RF radiation exposure limits for
general population. It must not be collocated or operating in conjunction with any
other antenna or transmitter.