PS Engineering
PAV80
Installation and Operator’s Manual
200-800-0101
Appendix D
Rev. 5, Feb. 2004
Appendix
D-
STC information and instructions for continuing airworthiness
8.1
Instructions for FAA Form 337, PAV80s
The STC was developed using an Approved Model List (AML). One method of airworthiness approval is through an
FAA Form 337,
Major Repair and Alteration (Airframe, Powerplant, Propeller, or Appliance)
In the case of the
PAV80, you may use the following text as a guide.
This unit is installed in accordance with FAA-STC SA02707AT, which specifically references the installa-
tion manual.
Installed IFE System, PS Engineering PAV80, part number 050-800-01XX) 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 200-800-(0101), 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 PAV80 added.
Aircraft equipment list, weights and balance amended. Compass compensation checked. A copy of the opera-
tion instructions, contained in PS Engineering document 200-800-( ), revision ( ), dated ( ), is placed in the
aircraft records. All work accomplished listed on Work Order
.
8.2
Instructions for Continuing Airworthiness, PAV80s
Sample ICA Checklist for PS Engineering PAV80s:
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,” “fail-safe” and/or
“emergency” mode. This allows pilot communications using aircraft radios.
Follow checkout instructions in the installation manual referenced 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
