PS Engineering
PXE7300
Installation and Operator’s Manual
200-973-0002 Appendix D December. 2002
Appendix D- STC information and instructions for continuing
airworthiness
8.1 Instructions for FAA Form 337, PXE7300s
STC SA02572AT applied, with an FAA-Approved Model List (AML) to a broad range of aircraft makes and models.
Consult www.ps-engineering.com/STC-AML.shtml
for the list.
One method of airworthiness approval in other aircraft is through an FAA Form 337, Major Repair and Alteration
(Airframe, Powerplant, Propeller, or Appliance) In the case of the PXE7300, you may use the following text as a
guide.
This unit is installed in accordance with FAA-STC SA02572AT, which specifically references the installa-
tion manual.
Installed IFE System, PS Engineering PXE7300, part number 1197 (X) in ( location )
at station . In-
stalled per AC43.13-2, Chapter 2, paragraph 23 (Instrument Panel Mounting). Installed per PS Engineering
Installation Operators Manual p/n 200-971-(XXXX), revision (), dated ( ).
Interface to existing aircraft radios in accordance with installation manual and in compliance with practices
listed in AC43.13-2, Chapter 2. All wires are Mil-Spec 22759 or 27500. Connection to aircraft dimmer bus is
____________________. Power is supplied to the unit through a __A circuit breaker (type and part number
),
and total electrical load does not exceed
% of the electrical system capacity with the PXE7300 added.
Aircraft equipment list, weights and balance amended. Compass compensation checked. A copy of the opera-
tion instructions, contained in PS Engineering document 200-973-( ), revision ( ), dated ( ), is placed in the
aircraft records. All work accomplished listed on Work Order .
8.2 Instructions for Continuing Airworthiness, PXE7300s
Sample ICA Checklist for PS Engineering PXE7300s:
Section Item Information
1 Introduction Installation of In-Flight Entertainment 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,” or pull circuit breaker
labeled”IFE.”. Follow checkout instructions in the installation manual refer-
enced on the FAA Form 337. For a specific unit fault, contact the manufacturer
at (865) 988-9800 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
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