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PS Engineering 

PXE7300 Series IFE System  

Installation and Operator’s Manual 

200-973-0002 

Page 2-7 

April 2006 

13.  Repeat step 10 for COM 2, and other transmitters. 

a.  Tune Nav 1 to local station and perform a standard VOT test in accordance with 14 CFR 91.171.  
b.  Note the indicated VOR bearing on both systems. 
c.  Turn the PXE7300 on and off, and observe any change in the VOR indication that could be attrib-

uted to the PXE7300. 

2.8 Final 

Inspection 

Verify that the wiring is bundled away from all controls and no part of the installation interferes with air-
craft control operation. Move all controls through their full range while examining the installation to see 
that no mechanical interference exists. Verify that the cables are secured to the aircraft structure in accor-
dance with good practices, with adequate strain relief. Ensure that there are no kinks or sharp bends in the 
cables and coaxial cables. Verify that the cables are not exposed to any sharp edges or rough surfaces, and 
that all contact points are protected from abrasion. 

Complete logbook entry, FAA Form 337, weight and balance computation and other documentation as 
required. Sample text for FAA Form 337 and instructions for continuing airworthiness can be found in 
Appendix F. 

Return completed warranty registration application to PS Engineering.

 

Summary of Contents for PXE7300

Page 1: ...eration Manual PS Engineering Inc 2006 Copyright Notice Any reproduction or retransmittal of this publication or any portion thereof without the expressed written permission of PS Engi neering Inc is...

Page 2: ...TION 2 2 2 3 4 CONNECTOR ASSEMBLY 2 3 2 4 CABLE HARNESS WIRING 2 3 2 4 1 NOISE 2 3 2 4 2 POWER 2 4 2 4 3 BACKLIGHTING 2 4 2 4 4 ANTENNA 2 4 2 4 5 UNSWITCHED SUMMED AUDIO 2 5 2 4 6 AUX ENTERTAINMENT AU...

Page 3: ...ESS D 8 1 INSTRUCTIONS FOR FAA FORM 337 PXE7300S D 8 2 INSTRUCTIONS FOR CONTINUING AIRWORTHINESS PXE7300S D 8 3 MASTER DRAWING LIST D 8 4 USE OF APPROVED MODEL LIST D APPENDIX E RTCA DO160D EUROCAE ED...

Page 4: ...mounted unit that contains a CD 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 audi...

Page 5: ...current Lighting Current 800 mA 5 mA Audio Specifications Output Impedance 150 1000 Audio Output 38 mW each channel no clipping 1 THD Distortion 1 THD Music Freq Response 3 dB 14 Hz 22 kHz FCC Type Ac...

Page 6: ...FAA TSO approved Make Model Part Number PM1000II 11920 11922 PM3000 11931 11932 PMA6000 Series 6000 all PMA7000 Series 7000 all PCD7100 11950 11951 PMA4000 11942 PS Engineering PAC24 050 240 all SL10...

Page 7: ...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 access...

Page 8: ...Install the tray using six FHP 6 32 x screws The unit must be supported at front and rear of the mounting tray See Appendix B The tray mounting can be made in any area that exists for adding addition...

Page 9: ...2 4 Cable Harness Wiring Referring to the appropriate Appendix assemble a wiring harness as required for the installation All wires must be MIL SPEC in accordance with current regulations Two and thre...

Page 10: ...Volt DC systems A two 2 Amp PULL TYPE breaker is required Power and ground wires must be a twisted 18 AWG pair Connect airframe power ground to Pin 22 only See Appendix B for typical circuit breaker l...

Page 11: ...tainment input DVD external XM Radio tuner etc The audio input is Pin 16 R Pin 17 L with respect to Pin K To enable the mode add an internal jumper on the pins marked J2 or apply a ground to Pin 20 of...

Page 12: ...ation on AM and FM 7 Verify that aux audio is presented to the output if connected 8 Evaluate the audio interface to be certain that the IFE audio is muted during intercom and radio com munication a I...

Page 13: ...aft control operation Move all controls through their full range while examining the installation to see that no mechanical interference exists Verify that the cables are secured to the aircraft struc...

Page 14: ...ount of information contained 3 2 1 Power Volume Control 1 The PXE7300 system is turned on and off by pushing the volume left hand knob The left knob is the volume control Turning the knob clockwise w...

Page 15: ...AUX if enabled 3 3 Radio Reception The passive AM FM antenna part number 510 730 0001 included is optimized for FM radio perform ance Therefore when used for AM reception the operator may only receiv...

Page 16: ...r Pre select Frequency Recall Mode Table 1 Modes 3 5 Pre recorded File Playback Option 1 ONLY The PXE7300 is designed to play up to five special files on a recorded MP3 disc This can be used for pas s...

Page 17: ...ABLE FOR INCIDENTAL OR CONSEQUENTIAL DAMAGES This warranty does not cover a defect that has resulted from improper handling storage or preservation or un reasonable use or maintenance as determined by...

Page 18: ...imited to displaying up to 22 characters in each of these fields Click on the appropriate field to modify the track title artist or album To modify the filename select the Rename Files button in the l...

Page 19: ...wed from front DATE REV 0 ECO REVISIONS DRAWING NUMBER INCORPORATED ENGINEERING SHEET 120 973 8801 Lenoir City Tn 37772 865 988 9800 9800 Martel Road 1 OF 1 BY 08 28 02 GLP DESCRIPTION TITLE SIZE DATE...

Page 20: ...em locations FS 76 5 Top of windshield Instrument Panel FS 59 9 ELEV VIEW From Copilot Side Antenna PXE7300 NOTE Install wire bundle and cable clamps as required IAW AC43 13 1B Section 8 WIRING INSTAL...

Page 21: ...02 DATE SIZE TITLE DESCRIPTION GLP 08 28 02 BY 1 OF 1 9800 Martel Road 865 988 9800 Lenoir City Tn 37772 120 973 0430 SHEET ENGINEERING INCORPORATED DRAWING NUMBER REVISIONS ECO 1 REV DATE Front of t...

Page 22: ...REV 08 28 02 DATE SIZE TITLE DESCRIPTION GLP 08 28 02 BY 1 OF 1 9800 Martel Road 865 988 9800 Lenoir City Tn 37772 120 973 8802 SHEET ENGINEERING INCORPORATED DRAWING NUMBER REVISIONS ECO 0 REV DATE...

Page 23: ...14 R 15 S Shield Ground Z 28 V Dimmer 14 V Dimmer A 1 21 C 3 6 A REV DATE SHEET OF TITLE DWN CKD APR DATE DATE DATE 14 28 VDC Aircraft Power 2 A Breaker AUX Enable IFE Audio Out R Audio Lo PXE7300 Co...

Page 24: ...ions contained in PS Engineering document 200 973 revision dated is placed in the aircraft records All work accomplished listed on Work Order 8 2 Instructions for Continuing Airworthiness PXE7300s Sam...

Page 25: ...aker Location X 120 973 8802 New 28 Aug 02 Users Guide 202 730 0001 1 Nov 2002 8 4 Use of Approved Model List STC SA02572AT can be used as a basis for approval in those airplanes listed in the Approve...

Page 26: ...PS Engineering PXE7300 Installation and Operator s Manual 200 973 0002 Appendix E April 2006...

Page 27: ...3 Equipment tested Category B Vibration 8 0 Equipment tested to Category S Explosion 9 0 Category X not tested Waterproofness 10 0 Category X not tested Fluids Susceptibility 11 0 Category X not test...

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