All rights reserved Jupiter Avionics Corporation (JAC) permits a single copy of this manual to be printed or downloaded for the express use of an installing agency. Any such electronic or printed copy of this manual must contain the complete text of this copyright notice.
SECTION 1 - DESCRIPTION System Overview The JA55-015 Speaker Panel - 4 Ohm - 15 Watt allows PA audio to be heard in the aircraft cabin. The JA55-015 operates using the audio provide from a speaker amplifier and requires no other external power.
JA55-015 Dzus Panel Speaker - 4 Ohm - 15 Watt Installation and Operating Manual Audio Frequency Response Speaker output audio frequency response ≤3dB from 300 to 6000 Hz Distortion Characteristics Audio output distortion at rated power ≤10% Audio output distortion at 10% of rated power ≤3%...
Installation Procedures 2.4.1 Installation Limitations Those installing the JA55-015, on or in a specific type or class of aircraft, must determine that the aircraft installation conditions meet standards. The JA55-015 may be installed only by following the applicable airworthiness requirements.
2.4.3 Mechanical Installation The JA55-015 can be mounted in any attitude and location with adequate space for the front panel and sufficient clearance for the connector and wiring harness. It requires no direct cooling. 2.4.4 System Operation The JA55-015 speaker input is routed to the speaker.
JA55-015 Dzus Panel Speaker - 4 Ohm - 15 Watt Installation and Operating Manual Appendix A - Installation Drawings Introduction The drawings necessary for installation and troubleshooting of the JA55-015 Dzus Panel Speaker - 4 Ohm - 15 Watt are in this Appendix, as listed below. Installation Drawings DOCUMENT...
Instructions for Continued Airworthiness Maintenance of the JA55-015 Dzus Panel Speaker - 4 Ohm - 15 Watt is “on condition” only. Refer to the JA55-015 Maintenance Manual. Periodic maintenance of the JA55-015 is not required. The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the Jupiter Avionics JA55-015 unit installation as part of a Type Certificate (TC) or Supplemental Type Certificate (STC) project to comply with CAR STD (AWM) 523/527/525/529.1529 or FAR 23/25/27/29.1529 “Instructions for Continued...
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Refer to the JA55-015 Maintenance Manual. 7. Removal and Replacement Information Refer to Section 2 of this manual - the JA55-015 Installation Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted. 8. Diagrams Refer to Appendix A of this manual - the JA55-015 Installation Manual - for installation drawings and interconnect examples.
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