PS Engineering PMA7000BT System Installation And Operation Manual Download Page 13

PS Engineering

PMA7000BT Series Audio Selector Panel and Intercom System

Installation and Operator’s Manual

200-780-0204

Page 2-6

Rev. 1, July 2015

2.5.8

Backlighting

The PMA7000BT has an automatic dimming of the pushbutton green annunciator LEDs and marker lamps
controlled  by  a  photocell.  Control  of  the  unit  backlighting (white  LEDS) is  through  the  aircraft  avionics
dimmer. Connect the dimmer control line to J1 pin D for 14 volt systems, and to J1 pin F for 28 volt sys-
tems. Pin E is light ground.

If an external dimmer control is not used, a constant low level back light illumination can be established for
nighttime  viewing.  Pin  D  or  F  (depending  on  system  voltage)  must  be  tied  to  power  (J1,  pin  20)  for  the
back lighting system to work. The photocell mounted in the unit face will automatically adjust the intensity
of the push-button green annunciator LEDs.

2.5.9

Unswitched inputs

J1, pins T, 17, U and X are unswitched, unmuted inputs. These inputs are presented to the pilot and copilot
regardless of the audio configuration, and  will always  mute the entertainment inputs. These 510

Ω inputs

can be used for altimeter DH audio, GPS waypoint audio, autopilot disconnect tones, or any other critical
audio signal. J1

Pin T is provided to the pilot’s headset even when the unit is off, or in fail

-safe mode.

If the KMA 24 installation include

s “External Speaker” or “Internal Speaker” connections to J1 Pins X and

U respectively), these will have to be disconnected to avoid interference with the Unswitched inputs #3 and
#4.

NOTE: Inputs 1, 2 and 4 are fixed (1:1), and any audio level adjustments must be made at the input source.
Input 3 (Bottom Connector pin U) has adjustable attenuation.

2.5.10 PA Mute (J1, Pin 18)

Pin 18 of J1 is a TTL logic output that is pulled low during PTT operation. This serves as an input to exter-
nal public address system to prevent feedback during transmissions.

2.5.11 Public Address Function (J2, Pin 18)

By connecting the top connector (J2), Pin 18 to ground, the pilot’s microphone audio is placed on the cabin
speaker output. When the pilot’s PTT is activated, his voice is heard ove

r the speaker. The copilot can con-

tinue to use the selected com.

We recommend installing a toggle switch to connect the cabin speaker output (pin W, bottom connector) to
a rear or public address speaker instead of the cockpit speaker close to the pilot. This will prevent feedback.

2.5.12

Control Output (J2, Pin A)

Pin A of the top connector is pulled to ground whenever the AUX button is depressed. This serves as a con-
trol line for external devices, such as an entertainment system that the pilot wishes to control.

This could be used in conjunction with a PA to control J2, Pin 18, as well as an external relay to change to
the cabin speaker from the cockpit.

This pin can also be used to control passenger Karaoke Mode, by connecting to pin V of the J2.

This pin can also be used to control Alternate Intercom Mode (2.4.15.1), by connecting J1 pin 14 to J2 pin
A.

2.5.13 Intercom wiring

The top connector (J2) is for the intercom and additional functions. See Appendix for intercom connection
configurations.  It  is  critical  to  the proper  operation  of  this  system  to  have  this  connector  wiring  made  in
accordance with these diagrams. Use 2- and 3-conductor, MIL-spec cable as shown. Connect the shields at
the audio panel end only, and tie to the audio low inputs as shown.

NOTE: The top connector harness can be custom made by PS Engineering, Inc. Simply call the factory and
obtain  a  wire  harness  work-sheet.  The  harness  will  be  made  to  your  specifications  and  fully  functionally
tested. All hardware is included.

Summary of Contents for PMA7000BT

Page 1: ...C35d Patented under one or more of the following No 4 941 187 5 903 277 6 160 496 and 6 493 450 PS Engineering Inc 2015 Copyright Notice Any reproduction or retransmittal of this publication or any po...

Page 2: ...2 4 2 5 2 POWER 2 4 2 5 3 COMMUNICATIONS PUSH TO TALK 2 4 2 5 4 AUDIO PANEL INTERFACE 2 5 2 5 5 COM 3 DUPLEX SAT PHONE FUNCTION FOR COM 3 2 5 2 5 6 TRANSMIT INTERLOCK 2 5 2 5 7 SWAP MODE 2 5 2 5 8 BAC...

Page 3: ...MODES 3 4 3 6 4 ENTERTAINMENT INPUT 3 5 3 7 SATELLITE TELEPHONE MODE 3 6 3 8 BLUETOOTH INTERFACE 3 6 3 8 1 PAIRING AND UNPAIRING BLUETOOTH DEVICES 3 6 3 8 2 BLUETOOTH TELEPHONE MODE 3 7 3 9 MARKER BEA...

Page 4: ...prohibited by regulation PS Engineering is not responsible for unauthorized airborne use of cellular telephones For airborne use the PMA7000BT must be interfaced with an approved system There are four...

Page 5: ...roval The PMA7000BT series Audio Selector Panels are FAA approved under TSO C50c Audio Amplifiers and TSO C35d Marker Beacon Receivers In addition they are approved by the Joint Airworthiness Au thori...

Page 6: ...ce 150 600 Intercom Specifications Intercom Positions 6 places with individual IntelliVox circuits Music Inputs 2 Independent Stereo Music Muting 30 dB Soft Mute when Com or intercom active Distortion...

Page 7: ...g bar 1 430 007 0001 6 32 X 3 4 pan head Phillips screw 2 475 632 0038 6 32 Nut Flat 2 475 632 0003 6 32 Lock Nut 2 475 632 0004 Cable Clamp 1 625 001 0002 6 32 x Flat head Phillips screw 6 475 632 00...

Page 8: ...hnical standard order TSO Installation of this article requires separate approval Re fer to AC 20 41A for information regarding Substitute TSO Aircraft Equipment 2 2 Unpacking and Preliminary Inspecti...

Page 9: ...onnections if it was constructed so it can be relo cated to the PMA7000BT tray 2 3 2 Unit Installation Remove the existing audio panel by turning the 3 32 hex head screw counterclockwise while pulling...

Page 10: ...e connectors are a Molex crimp type and require the use of a Molex hand crimp tool EDP P N 11 01 0203 CR6115B or equiv The connectors are mounted to the unit tray with 4 40 screws 475 440 0007 from th...

Page 11: ...iring into the same shielded bundle Always use a 2 or 3 conductor shield wire as shown on the installation wiring diagram Radiated signals can be a factor when low level microphone signals are bundled...

Page 12: ...eceive audio from Com 3 in the headset and applies the pilot or copilot microphone to the Com 3 when the appropriate PTT is activated If J2 Pin J is connected to aircraft ground the PMA7000BT is force...

Page 13: ...8 Pin 18 of J1 is a TTL logic output that is pulled low during PTT operation This serves as an input to exter nal public address system to prevent feedback during transmissions 2 5 11 Public Address F...

Page 14: ...t 14 R 13 Alternate Music Interconnect Ent 1 Input NOTE Use the low level output of any additional entertainment device to connect to the audio panel Maximum signal level is 2 VAC p p DO NOT use a spe...

Page 15: ...to the type and speed of the aircraft is required not included Refer to aircraft and antenna manufacturer s installation instructions as well as AC43 13 2A or later revision Chapter 3 for information...

Page 16: ...m Installation and Operator s Manual 200 780 0204 Page 2 9 Rev 1 July 2015 Figure 2 3 PMA7000BT Adjustments Figure 2 4 PMA7000BT Adjustments Com 3 Volume Must remove ESD Sheet Speaker Volume Marker Vo...

Page 17: ...hook switches must be installed to have full access to the satellite phone systems The copilot hook switch is a SPST switch that connects pin L of J2 on the PMA7000BT to ground to place the copilot m...

Page 18: ...tertainment 2 In L J2 Top Connector Input Output Pilot Mic Audio Hi In Com 3 Audio Hi Com 1 Audio Hi Com 2 SPKR Load AUX Audio Input Hi Com 1 Spkr Load Com 2 Audio Hi Aircraft Power 11 33 VDC ADF Audi...

Page 19: ...be present in the right ear cup only 4 Switch on the unit by pressing the volume VOL knob 5 Check intercom operation 6 Push the Com 1 Xmt select button lower row 7 Verify that both of the Com 1 butto...

Page 20: ...the sensitivity in the field so as to prevent early detection of the marker beacons If your particular installation requires more or less sensitivity see adjustment section 2 6 and figure 2 1 2 12 Bl...

Page 21: ...ved or turned OFF the audio selector will be placed in the fail safe mode The power switch also controls the audio selector panel functions intercom and marker beacon receiver 3 3 Microphone XMT Selec...

Page 22: ...which receivers are selected by noting which of the green switch LEDs are illumi nated Push buttons labeled Nav 1 Nav 2 MKR Marker ADF DME AUX auxiliary and SPR Speaker are momentary type switches Wh...

Page 23: ...There is no field adjustment Through three individual signal processors the ambient noise appearing in all six microphones is constantly being sam pled Non voice signals are blocked When someone spea...

Page 24: ...he lower switch on the left side is a 3 position mode switch that allows the pilot to tailor the intercom function to best meet the current cockpit situation The description of the intercom mode funct...

Page 25: ...dible in passenger headsets 3 6 4 2 Soft Mute and Soft Mute inhibit The Soft Mute feature assures that the aircraft radio transmissions will not be missed due to entertainment playing When there is ra...

Page 26: ...hone and all four passengers will hear the conversation In ISO intercom mode when the PMA7000BT is in the Com 3 mode the pilot position is in the Phone Booth Only the pilot will hear the telephone and...

Page 27: ...pilot are connected to the telephone The pilot and copilot will have transmit capability on the other selected transceiver COM 1 or 2 simply by using their respective PTT switch In ISO intercom mode w...

Page 28: ...the Inner marker and has a 3000 Hertz dot tone The lamp and tone will be keyed at a rate of six times per second The audio from the Marker Beacon Receiver can be heard by selecting the MKR push button...

Page 29: ...is warranty is not transferable Any implied warranties expire at the expiration date of this warranty PS Engineering SHALL NOT BE LIABLE FOR INCIDENTAL OR CONSEQUENTIAL DAMAGES This warranty does not...

Page 30: ...3 mm 6 31in 160 3 mm Cutout size for front mount installation 1 315 in 33 4 mm 6 28 in 159 5 mm 3 00 in 76 2 mm CG Weight 1 5 lb with tray and connectors 68 kg Side View Rear View 6 65 in 167 mm J1 b...

Page 31: ...uld be grounded at audio panel only other end remains floating 3 Speaker and Pilot Headphone ground returns MUST be kept separate and connected to pin 22 4 All Power and Ground wires must be 18 gage w...

Page 32: ...or AGT or cellular phone 11 When pin 18 is switched to ground the PA mode is activated placing pilot microphone on speaker output when PTT active See Sect 2 5 13 2 3 B Copilot Phones L Copilot Phones...

Page 33: ...ed in the aircraft records All work accomplished listed on Work Order 8 2 Instructions for Continuing Airworthiness Audio System Sample ICA Checklist for PS Engineering Audio System Section Item Infor...

Page 34: ...idity 6 0 Equipment tested to Category A Shock 7 0 Equipment tested to Operational test only Operational 7 2 Equipment tested to Operational test only Crash Safety 7 3 Equipment tested to Operational...

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