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Appendix d – Garmin PAV80 User Manual

Page 33

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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