PS Engineering PXE7300 Installation Manual User Manual
Page 7
PS Engineering
PXE7300 Series IFE System
Installation and Operator’s Manual
200-973-0002
Page 2-1
April 2006
Section II - Installation
2.1
GENERAL INFORMATION
2.1.1 SCOPE
These sections provide detailed installation and interconnect instructions for the PXE7300
In-Flight En-
tertainment
System with integrated Compact Disc (CD) Player and AM/FM radio receiver.
Please read this manual carefully before beginning any installation to prevent damage and post-installation
problems. Installation of this equipment requires special tools and knowledge.
NOTE:
An appropriately rated Certified Aircraft Repair Station must install
this equipment in accordance with applicable regulations. PS Engi-
neering, Incorporated warranty is not valid unless the equipment is
installed by an authorized PS Engineering, Incorporated dealer. Fail-
ure to follow any of the installation instructions, or installation by a
non-certified individual or agency will void the warranty, and may re-
sult in an unairworthy installation.
2.2
Unpacking and Preliminary Inspection
Use care when unpacking the equipment. Inspect the units and parts supplied for visible signs of shipping
damage. Examine the unit for loose or broken buttons, bent knobs, etc. Verify the correct quantity of com-
ponents supplied with the list in Section 1.6 (B). If any claim is to be made, save the shipping material and
contact the freight carrier. Do NOT return units damaged in shipping to PS Engineering. If the unit or an
accessory shows any sign of external shipping damage, contact PS Engineering to arrange for a replace-
ment. Under no circumstances attempt to install a damaged unit in an aircraft. Equipment returned to PS
Engineering for any other reason should be shipped in the original PS Engineering packaging, or other
UPS approved packaging.
2.3
Equipment Installation Procedures
2.3.1 Cooling
Requirements
Forced air-cooling of the PXE7300 is not required. However, the unit should be kept away from heat pro-
ducing sources (i.e. defrost or heater ducts, dropping resistors, heat producing avionics) without adequate
cooling air provided.
2.3.2
Mounting Requirements
The PXE7300 must be rigidly mounted to the instrument panel or other structure of the aircraft structure
and within view and reach of the persons wishing access. Installation must comply with FAA Advisory
Circular AC 43.13-2A (or later revision). The unit may be mounted in any area where adequate clearance
for the unit and associated wiring bundle exist.
The unit must be installed within ±30° of horizontal along the pitch axis, and ±10° of horizontal along the
roll axis in level flight.
Avoid installing the PXE7300 close to high current devices or systems with high-voltage, pulse type out-
puts, such as DME or transponders.