PS Engineering Inc HSA13 Impedance Adapter User Manual

HSA13 Impedance Adapter

PS Engineering HSA13 Headset Impedance Adapter

The PS Engineering HSA13 Headset Impedance Adapter is an accessory device designed to provide impedance matching between a general aviation (150) audio panel or radio, and a low-impedance (5 microphone and/or 8 headphone. It is a remote-mounted device designed to match low impedance headset/helmet with high impedance systems.

Installation Instructions

1. Before installing the HSA13, read the installation manual completely.
2. In certified aircraft, warranty is not valid unless this product is installed by an Authorized PS Engineering dealer.
3. Replace dB Systems DB-213 with HSA13 050-213-0001 or Jupiter Avionics JP39 with HSA13 050-213-0100, as they are drop-in, pin-compatible replacements.

Operation Instructions

1. Before using the HSA13, read the operation manual completely.
2. The HSA13 provides impedance matching between a general aviation (150) audio panel or radio, and a low-impedance (5 ) microphone and/or 8 headphone.

Technical Information

• Part Number: 050-213-0001 (Microphone Impedance Adapter), 050-213-0100 (Headset Impedance Adapter)
• The unit is a remote-mounted device designed to match low impedance headset/helmet with high impedance systems.
• The HSA13 050-213-0001 is a drop-in, pin-compatible replacement for the dB Systems DB-213. The HSA13 050-213-0100 is a drop-in, pin-compatible replacement for the Jupiter Avionics JP39.
• For further technical information, contact the Publications Manager at PS Engineering, Inc., 9800 Martel Road, Lenoir City, TN 37772. Phone 865-988-9800.

Record of revisions:

GENERAL INFORMATION

INTRODUCTION

The HSA13 is an accessory device designed to provide impedance matching between a general aviation (150Ω) audio panel or radio, and a low-impedance (5 Ω) microphone and or 8Ω headphone.
Before installing and/or using this product, please read this manual completely. This will ensure that you will take full advantage of all the features in the HSA13.

SCOPE

This manual provides detailed installation and operation instructions for the PS Engineer-ing HSA13-series of Audio Amplifier Systems. This includes the following unit:

EQUIPMENT DESCRIPTION

The unit is a remote-mounted device designed to match low impedance headset/helmet with high impedance systems. The HSA13 050-213-0001 is a drop- in, pin-compatible re-placement for the dB Systems DB-213. The HSA13 050-213-0100 is a drop-in, pin-com-patible replacement for the Jupiter Avionics JP39.

APPROVAL BASIS – FAA-TSO

The HSA13 Headset Adapter is FAA authorized under TSO C139A (Audio Amplifiers). ED-14C/DO-160G (Environmental Conditions and Test Procedures for Airborne Equip-ment), and ED- 18/DO-214A (Audio Systems Characteristics and Minimum Operational Performance Standards for Aircraft Audio Systems).

Operation is subject to the following conditions:

This device may not cause harmful interference.
This device must accept any interference received, including interference that may cause undesired operation.

SPECIFICATIONS

EQUIPMENT SUPPLIED

One ea. of the following units:

HSA13 Installation Material:250-213-0100

EQUIPMENT REQUIRED BUT NOT SUPPLIED

Low Impedance microphone and or headset Audio control panel or radio requiring High Impedance microphone input. Interconnect Wiring

LICENSE REQUIREMENTS

None

SCOPE
This section provides detailed installation and interconnect instructions for the PS Engi-neering HSA13 Headset Adapter.
Please read this manual carefully before beginning any installation to prevent damage and post-installation problems. Installation of this equipment requires special tools and knowledge.

NOTE: An appropriately rated Certified Aircraft Repair Station must install this equip-ment in accordance with applicable regulations. PS Engineering, Incorporated warranty is not valid unless the equipment is installed by an authorized PS Engineering, Incorporated dealer. Failure to follow any of the installation instructions, or installation by a non-certi- fied individual or agency will void the warranty, and may result in an unairworthy instal-lation.

Certification Requirements
The HSA13 requires specialized knowledge and tools for an effective installation. An ap-propriately rated Certified Aircraft Repair Station must install this equipment in accord-ance with applicable regulations. PS Engineering, Incorporated warranty is not valid un-less the equipment is installed by an authorized PS Engineering, Incorporated dealer. Failure to follow any of the installation instructions, or installation by a non- certified in-dividual or agency will void the warranty, and may result in an unairworthy installation. This article meets the minimum performance and quality control standards required by a technical standard order (TSO). Installation of this article requires separate approval. Re-fer to AC 20-41A for information regarding Substitute TSO Aircraft Equipment.

Unpacking and Preliminary Inspection
Use care when unpacking the equipment. Inspect the units and parts supplied for visible signs of shipping damage. Examine the unit for loose or broken buttons, bent knobs, etc. Verify the correct quantity of components supplied with the list in Section 1.6. If any claim is to be made, save the shipping material and contact the freight carrier. Do NOT return units damaged in shipping to PS Engineering. If the unit or accessories show any sign of external shipping damage, contact PS Engineering to arrange for a replacement. Under no circumstances attempt to install a damaged unit in an aircraft. Equipment re-turned to PS Engineering for any other reason should be shipped in the original PS Engi-neering packaging, or other UPS approved packaging.

Equipment Installation Procedures

Cooling Requirements
Forced air-cooling of the HSA13 is not required. However the unit should be kept away from heat producing sources (i.e. defrost or heater ducts, dropping resistors, heat produc-ing avionics) without adequate cooling air provided.

Mounting Requirements
The HSA13 must be rigidly mounted to the aircraft structure. Installation must comply with FAA Advisory Circular AC 43.13-2A. The unit may be mounted in any area where adequate clearance for the unit and associated wiring bundle exist. The unit may be mounted in any position or orientation. Avoid installing the HSA13 close to high current devices or systems with high-voltage pulse type outputs, such as DME or transponders. To install the HSA13, select a location convenient to the headphone jack providing the input, and the audio panel. The unit may be installed in any position, on a surface that will allow for installation in accordance with AC43-13-2A.

Connector Assembly
The unit connector is a male DB9 connector. This is a crimp-type connector. The AMP Contact Crimping Tool, AMP 601966-1 (or MS22520 equiv.), with Positioning Tool 601966-5 must be used to ensure good quality harness. Ensure that proper strain relief and chafing precautions are made during wiring and in-stallation.

Cable Harness Wiring

Referring to the Appendix, assemble a wiring harness as required for the installation. All wires must be MIL-SPEC in accordance with current regulations. Two- and three-con-ductor shielded wire must be used where indicated, and be MIL-C-27500 or equivalent specification. Proper stripping, shielding and soldering technique must be used at all times. It is imperative that correct wire be used.
Refer to FAA Advisory Circular 43.13-2A for more information. Failure to use correct techniques may result in improper operation, electrical noise or unit failure. Damage caused by improper installation will void the PS Engineering warranty.

Noise
Due to the variety and the high power of radio equipment often found in today’s general aviation aircraft, there is a potential for both radiated and conducted noise interference. Ground loop noise occurs when there are two or more ground paths for the same signal (i.e., airframe and ground return wire). Large cyclic loads such as strobes, inverters, etc., can inject noise signals onto the airframe that are detected by the audio system. Follow the wiring diagram very carefully to help ensure a minimum of ground loop potential. Use only Mil Spec shielded wires (MIL-C-275000, or better).
Radiated signals can be a factor when low-level audio signals are “bundled” with current carrying power wires. Keep these cables physically separated.

Power
The HSA13 is powered by the audio system or radio microphone bias.

HSA13 (P2131) Pin Assignments

Adjustments

The HSA13 is factory adjusted to accommodate the typical requirements for most aircraft configurations. The microphone gain can be adjusted using Mic Gain adjustment pot.

Post Installation Checkout

Operational Checkout
Apply power to the aircraft and avionics. Speak into the microphone associated with the HSA13 and verify proper intercom and radio voice communication.

Final Inspection

Verify that the wiring is bundled away from all controls and no part of the installation in-terferes with aircraft control operation. Move all controls through their full range while examining the installation to see that no mechanical interference exists. Verify that the cables are secured to the aircraft structure in accordance with good practices, with ade-quate strain relief. Ensure that there are no kinks or sharp bends in the cables and coaxial cables. Verify that the cables are not exposed to any sharp edges or rough surfaces, and that all contact points are protected from abrasion.
Complete log documentation, weight and balance computation and other documentation as required. Sample instructions for continuing airworthiness can be found in §6.1.
Return completed warranty registration application to PS Engineering.

Section III OPERATION

Scope

This section provides detailed operating instructions for the PS Engineering HSA13, Part Number 050-213-0000, Headset Adapter. Please read it carefully before using the equip-ment so that you can take full advantage of its capabilities.

Operation

The HSA13 has no independent controls. See audio panel installation and operations manuals for information.

Section IV- Warranty and Service

Warranty

In order for the factory warranty to be valid, the installations in a certified aircraft must be accomplished by an FAA-certified avionics shop and authorized PS Engineering dealer. If the unit is being installed by a non- certified individual in an experimental aircraft, a factory-made harness must be used for the warranty to be valid. PS Engineering, Inc. warrants this product to be free from defect in material and workmanship for a period of one (1) year from the date of sale. During the twelve (12) months of the warranty period, PS Engineer-ing, Inc., at its option, will send a replacement unit at our expense if the unit should be determined to be defective after consultation with a factory technician. All transportation charges for returning the defective units are the responsibility of the purchaser. All do- mestic transportation charges for returning the exchange or repaired unit to the purchaser will be borne by PS Engineering, Inc. The risk of loss or damage to the product is borne by the party making the shipment, unless the purchaser requests a specific method of shipment. In this case, the purchaser assumes the risk of loss. This warranty is not transferable. Any implied warranties expire at the expiration date of this warranty. PS Engineering SHALL NOT BE LIABLE FOR INCIDENTAL OR CONSEQUENTIAL DAMAGES. This warranty does not cover a defect that has resulted from improper handling, storage or preservation, or un-reasonable use or maintenance as determined by us. This warranty is void if there is any attempt to dissem-ble this product without factory authorization. This warranty gives you specific legal rights, and you may also have other rights, which may vary from state to state. Some states do not allow the exclusion of limita-tion of incidental or consequential damages, so the above limitation or exclusions may not apply to you. All items repaired or replaced under this warranty are warranted for the remainder of the original warranty period. PS Engineering, Inc. reserves the rights to make modifications or improvements to the product without obligation to perform like modifications or improvements to previously manufactured products.

Factory Service

The unit is covered by a one-year limited warranty. See warranty information. Call PS Engineering, Inc. at 865-988-9800 before you return the unit. This will allow the service technician to provide any other sug-gestions for identifying the problem and recommend possible solutions.
After discussing the problem with the technician and you obtain a Return Authorization Number, ship product to:
[Note: PS Engineering will not be responsible for items shipped in US Mail.] PS Engineering, Inc.
Attn: Service Department
9800 Martel Rd
Lenoir City, TN 37772
865-988-9800 FAX 865-988-6619

Appendix A – Installation Drawing

Appendix B Connector layout and wiring

Connector wiring ****

Installation Wiring Diagram (050-213-0001 only)

Appendix C Instructions for Continuing Airworthiness,

Sample ICA Checklist for PS Engineering System:

Appendix D – RTCA DO160G Environmental Qualification Form

Model Number HSA13 Microphone Headset Adapter
Part Number: 050-213- (XXXX)
FAA TSO Number: C139a,
Manufacturer: PS Engineering Incorporated 9800 Martel Road
Lenoir City TN 37772

PS Engineering
HSA13 Headset Impedance Adapter Installation and Operator’s Manual

References

• PS Engineering Inc

Read User Manual Online (PDF format)

Read User Manual Online (PDF format)  >>

Download This Manual (PDF format)

Download this manual  >>