PS Engineering PAV80 Installation Manual - Manual (Page 33)

PS Engineering
PAV80
Installation and Operator’s Manual
200-800-0101 Appendix D Rev. 6, Sept. 2005
Appendix D- STC information and instructions for contin
uing
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