Garmin operation manual Instructions for FAA Form 337, PAV80s

PS Engineering

PAV80

Installation and Operator’s Manual

Appendix D- STC information and instructions for continuing airworthiness

8.1Instructions 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 .

8.2Instructions 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-	Removal: Using a 3/32” Allen-head wrench, carefully unscrew the locking
	tion	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

200-800-0101 Appendix D Rev. 5, Feb. 2004