Garmin PAV80 - Manual (Page 4)

PS Engineering
PAV80 Series IFE System
Installation and Operator’s Manual
200-800-0101 Page 1-1 Rev. 5 Feb. 2004
Section I GENERAL INFORMATION
1.1 INTRODUCTION
Quality cockpit and cabin entertainment has long been an elusive dream in general aviation. From marginal
performance to unapproved parts, pilots couldn’t enjoy the same entertainment in their aircraft as they
could in the family car.
The PAV80-Series represents such a product. This system combines a Digital Versatile Disc (DVD) player
with CD and MP3 capability with an AM/FM radio for ultimate in-flight entertainment capability.
Before installing and/or using this product, please read this manual completely. This will ensure that you
will take full advantage of all the advanced features in the PAV80.
1.2 SCOPE
This manual provides detailed installation and operation instructions for the PS Engineering PAV80-series
of IFE Systems. This includes the following units:
Model Part Number Description
PAV80 050-800-0100 Integrated DVD-IFE System with CD/MP3/AM/FM
PAV80 050-800-0200 European Version Tuner
PVT801 050-801-0100 5.6” LCD Video Display
Remote 051-803-0150 IR Remote Control
PVA802 050-802-0100 Remote Video Distribution Amplifier
Where the functions are identical to all units, it will be referred to herein as a PAV80. Otherwise, the appli-
cable units will be specified.
1.3 EQUIPMENT DESCRIPTION
The PAV80 System is a single panel mounted unit that contains a DVD player with MP3 media capability
and an AM/FM radio receiver. It also contains a high-fidelity stereo amplifier to provide the entertainment
output to the aircraft audio system. A single LCD monitor (PVT801) is included in the system. Up to four
external video displays can provide visual entertainment to the passengers, with the optional video distribu-
tion amplifier (PVA802).
An 8-digit LED display provides information about the systems modes and media in use. A remote control
is used for passenger control over the system.
1.4 APPROVAL BASIS
The PAV80 is FAA approved FAA-STC SA02707AT and manufactured under PMA. PQ1336CE.
All systems comply with relevant portions of EUROCAE ED-14D/DO-160D (Environmental Conditions
and Test Procedures for Airborne Equipment), ED12B/DO-178B (Software Considerations for Airborne
Equipment) and ED- 18/DO-214 (Audio Systems Characteristics and Minimum Operational Performance
Standards for Aircraft Audio Systems).
STC SAAT can be used as a basis for approval in other aircraft provided the generic installation manual,
Document Number 200-800-0002 or later approved revision, is followed.
Advisory Circulars AC43.13-1B Acceptable Methods, Techniques, and Practices - Aircraft Inspection and
Repair, and 43.13-2A - Acceptable Methods, Techniques, And Practices - Aircraft Alterations are to be
used to resolve any issues not specifically addressed by the Installation Manual. Instructions for Continu-
ing Airworthiness (ICA) are provided in the supplied data.