Manual

PS Engineering Inc. ®
PAR200 Audio Selector Panel, COM radio Controller and Intercom System
Installation and Operator’s Manual
200-228-0000 Appendix E Rev. 4, Dec. 2013
Appendix E – Instructions for FAA Form 337 and continuing
airworthiness
9.1 Instructions for FAA Form 337, Audio Panels
One method of airworthiness approval is through an FAA Form 337, Major Repair and Alteration (Airframe, Power-
plant, Propeller, or Appliance) In the case of the PAR200, you may use the following text as a guide.
Installed audio selector and 6-place intercom, PS Engineering PAR200, part number 050-228-(XXXX) in (
location ) at station . Installed per AC43.13-2B, Chapter 2, paragraph 23 (Instrument Panel Mount-
ing). Installed per PS Engineering Installation Operators Manual p/n 200-228-(XXXX), revision (), dated (
).
These units are FAA-Approved under TSO C139 for audio amplifiers, and a partial TSO C169a for communi-
cations transceivers, and meets appropriate environmental qualifications outlined in RTCA DO-160G as ap-
propriate for this aircraft.
Interface to existing aircraft radios in accordance with installation manual and in compliance with practices
listed in AC43.13-2B, Chapter 2. All wires are Mil-Spec 22759 or 27500. Connection to aircraft dimmer bus
is ____________________. Power is supplied to the unit through a 3A circuit breaker (type and part number),
and total electrical load does not exceed % of the electrical system capacity with the PAR200 added.
Aircraft equipment list, weights and balance amended. Compass compensation checked. A copy of the opera-
tion instructions, contained in PS Engineering document 202-228-( ), revision ( ), dated ( ), is placed in the
aircraft records. All work accomplished listed on Work Order .
9.2 Instructions for Continuing Airworthiness, Audio System
Sample ICA Checklist for PS Engineering Audio System:
Section Item Information
1 Introduction Installation of audio control panel with integrated VHF communications con-
troller and intercommunications system.
2 Description Installation as described in manufacturer’s installation manual referenced on
FAA Form 337, including interface with other avionics audio as required.
3 Controls See installation and operator’s guide referenced on FAA Form 337.
4 Servicing None Required
5 Maintenance Instructions On Condition, no special instructions
6 Troubleshooting In the event of a unit problem, place the unit into “off,” “fail-safe” and/or
“emergency” mode. This allows pilot communications using COM 1. Follow
checkout instructions in the installation manual referenced on the FAA Form
337. For a specific unit fault, contact the manufacturer at [phone] for
special instructions.
7 Removal and replacement informa-
tion
Removal: Using a 3/32” Allen-head wrench, carefully unscrew the locking
screw located in the center of the unit. While turning the wrench CCW, gently
pull on the EDGES of the bezel until the unit is free from the mounting tray.
Installation: Engage the locking screw at the back. Turn the locking screw CW,
while applying slight pressure to the edges of the bezel. Do not over tighten!
8 Diagrams Not applicable
9 Special Inspection Requirements Not Applicable
10 Protective Treatments Not Applicable
11 Structural Data Not Applicable
12 Special Tools None
13 Not Applicable Not Applicable
14 Recommended Overhaul Periods None
15 Airworthiness Limitations Not Applicable
16 Revision To be determined by installer