PS Engineering PAC45A Installation And Operation Instructions Manual

PS Engineering PAC45A Installation And Operation Instructions Manual

Special mission audio controller system with multitalker and intellivox
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Special Mission Audio Controller System
with MultiTalker™ and IntelliVox®
Patented under one or more of the following;
No. 4,941,187; 5,903,227; 6,160,496 and 6,493,450, 7,391,877
In certified aircraft, warranty is not valid unless this product is installed by an
Any reproduction or retransmittal of this publication, or any portion thereof, without the expressed written permission of PS En-
gineering, Inc. is strictly prohibited. For further information, contact the Publications Manager at PS Engineering, Inc., 9800
Martel Road, Lenoir City, TN 37772. Phone (865) 988-9800, email contact@ps-engineering.com.
9800 Martel Road
Lenoir City, TN 37772
www.ps-engineering.com
PAC45A
Document P/N 200-045-1000
Revision 2, March 2019
Audio Control System with Intercom
System Installation and Operation Manual
Authorized PS Engineering dealer.
PS Engineering, Inc. 2019 ©
Copyright Notice

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Summary of Contents for PS Engineering PAC45A

  • Page 1 Any reproduction or retransmittal of this publication, or any portion thereof, without the expressed written permission of PS En- gineering, Inc. is strictly prohibited. For further information, contact the Publications Manager at PS Engineering, Inc., 9800 Martel Road, Lenoir City, TN 37772. Phone (865) 988-9800, email contact@ps-engineering.com.
  • Page 2: Table Of Contents

    2.7.1 U .................... 2-7 NSWITCHED UDIO EVEL 2.7.2 A ........................2-7 DJUSTMENTS 2.7.3 L ....................2-9 OGIC WITCH PTIONS PAC45A P ..........................2-10 IN ASSIGNMENTS ............................2-11 IRING HECKOUT 2.10 O ..........................2-12 PERATIONAL HECKOUT 2.10.1 R ..................2-12 EQUIRED QUIPMENT 2.10.2 A...
  • Page 3 ARRANTY .............................. 4-1 ACTORY ERVICE Appendix A – PAC45A Installation Drawings ............A Appendix B – Radio Interconnect Wiring ..............B Appendix C – Intercom Interconnect Wiring ............C Appendix D – Control Head Interconnect Wiring ............ D Appendix E – Unit Connector Wiring Reference ............E J451 C ..............................
  • Page 4: Section I - General Information

    Night Vision Compatible EQUIPMENT DESCRIPTION The PAC45A is a state-of-the-art audio isolation amplifier and audio selector that contains an automatic voice activated (VOX) intercom system. It can switch up to eight transceivers (COM 1 to 8) and eight navigation receivers (AUX 1 to 8) that can be configured as desired.
  • Page 5: Approval Basis Faa Tso (Pending)

    APPROVAL BASIS FAA TSO (Pending) 1.1.2 Limitations This article meets the minimum performance and quality control standards required by a technical standard order (TSO). Installation of this article requires separate approval. Refer to Advisory Circular 20-41A for information on TSO installation approval. Operation is subject to the following conditions: This device may not cause harmful interference.
  • Page 6: Equipment Supplied

    EQUIPMENT SUPPLIED The following units comprise the PAC45A System: Model Description Part Number HUB45AR Remote-mounted Audio Hub for analog I/O and processing 050-045-1001 CTL45A Control Head for pilot or copilot positions 050-045-2000 CTL45A-M Panel-mounted Control Head for Observers 050-045-3000 CTL45A-NVG...
  • Page 7 EQUIPMENT REQUIRED BUT NOT SUPPLIED Circuit Breakers: 1 ea.; 5 amp PULL TYPE REQUIRED for HUB45G, 1 A for CTL45As Optional Circuit Breakers: 1 ea.; 1 amp PULL TYPE REQUIRED for PAC45A aural alerts, 1 ea. 1 A for failsafe power...
  • Page 8: Configuration

    Configuration The PAC45A System is comprised of a single PAC45A HUB (HUB45R) and up to four CTL45 Control Head “building blocks” to facilitate flexibility as well as simplicity. Bluetooth Telephone Telephone COM1-8 Pilot NAV 1-2 HUB45AR Copilot Aux 3-8 UNSW1-5...
  • Page 9: Section Ii - Installation

    2.3 Equipment Installation Procedures 2.3.1 Cooling Requirements Forced air-cooling of the PAC45A is not required. However, the units 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.
  • Page 10: Audio Controller Connector Assembly

    P451 J452 J454 Figure 2-1 - PAC45A Connector Layout Figure 2-2 - Connector assembly NOTE: Pass the wire bundle through the Cover Nut before inserting pins in the connector shell. Insert the screw or thumbscrews through the top half of the shell (B), and apply the E-Ring to the unthreaded portion, and bend the E-ring holder back and forth to break it from the holder.
  • Page 11: Cable Harness Wiring

    2.4.2 Power The PAC45A is compatible with 28 Volt DC systems. A five (5) Amp circuit breaker is required for all installations. Power and ground wires should be #22AWG connect power to P451 Pin 42. Connect airframe ground to P451 Pin 20 and 21 only.
  • Page 12: Audio Controller Interface

    Alert power, P451 Pin 41, The PAC45A has an independent alert system with the ability to play alerts even when the audio controller is powered off. To take full advantage of this isolation a separate one (1) Amp circuit breaker is required.
  • Page 13: Cockpit Voice Recorder

    Alerts with level trigger will play continuously until the Acknowledge button (ACK) is pressed (remote ACK P454-23 grounded), or the input level reverts. When power is applied to the alerts and not the PAC45A audio controller, it will play the message continu- ously until the remote acknowledge is selected.
  • Page 14: Oxy (P453-26)

    2.6 Wired Telephone/Satellite Communication input The PAC45A can accommodate a wired cell phone interface on J452 Pins 58, 59, and 38. Both Bluetooth and wired Telephone and be accommodated, however, only ONE can be active at a time. Low impedance satellite phones might require a tactical radio adapter, PS Engineering P/N 12100.
  • Page 15: User Adjustments

    The PAC45A is factory set for typical installation. However, several installation adjustments are avail- able. No computer is required. 2.7.1 Unswitched Audio Level Unswitched inputs one through five are installation adjustable through the side of the PAC45A unit. 2.7.2 Adjustments On the side of the PAC45A/HUB45R are 15 adjustment potentiometers.
  • Page 16 10. External PA Sidetone 11. External COM 1 Sidetone 12. External COM 2 Sidetone 13. Alert volume (adjusts the level of the internal audio alerts and annunciations generated by the PAC45A) 14. Green backlight level 15. White backlight level 200-045-1000 Page 2-8 Rev.
  • Page 17: Logic Switch Options

    2.7.3 Logic Switch Options The PAC45A has switches accessible through the side of the HUB45R to set specific functions TOP ROW BOTTOM ROW SWITCH FUNCTION POSITION SWITCH FUNCTION POSITION COPILOT CONTROL HEAD FAILSAFE ALERTS TO CREW INSTALLED FAILSAFE ALERTS TO...
  • Page 18: Pac45A Pin Assignments

    2.8 PAC45A Pin assignments P451 J452 Description Description Ground Lighting Common Ground Music Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground Ground...
  • Page 19: Wiring Checkout

    After wiring is complete, verify power is ONLY on pins 41, 42 & 62 of J451 and airframe ground on pins 20 & 21. Failure to do so will cause serious internal damage and void PS Engineering's warranty. CAUTION: Do not connect or disconnect (...
  • Page 20: Operational Checkout

    2.10 Operational Checkout 2.10.1 Required Test Equipment In order to return an aircraft to service after installation of the PAC45A, the installer must have access to headset(s), and be able to establish 2-way communications on appropriate radios. Equivalent test equipment is acceptable as long as the testing requirements can be met.
  • Page 21: Bluetooth Checkout

    2.10.3.1 Bluetooth TEL Checkout Pair the PAC45A with a Bluetooth telephone device. Verify that the pilot headset is connected to the cellular telephone system (if installed). The telephone function will allow any person heard by the pilot on the inter- com, also heard on the telephone.
  • Page 22: Section Iii Operation

    The radio is automatically selected to receive incoming radio calls when the XMT is selected. With a PAC45A, you will never transmit on a radio that you are not receiving. The selected audio is indicated by both knob position and the green text.
  • Page 23: Navaid Selection

    PS Engineering PAC45A Audio Selector Panel and Intercom System Installation and Operator’s Manual Intercom and other audio is not spatially processed, only the eight communications transceivers. NOTE: You must use stereo headsets, in stereo mode for this feature. This adjustment allows the eight Spatial Audio inputs to be “relocated” on any of nine (9) pre-defined “Head Related Transfer Function”...
  • Page 24: Intercom Volume Control

    PS Engineering PAC45A Audio Selector Panel and Intercom System Installation and Operator’s Manual The system is designed to block continuous tones; therefore, people humming or whistling in monotone may be blocked after a few moments. For consistent performance, any headset microphone must be placed within ¼-inch of your lips, preferably against them.
  • Page 25: Speaker Operation

    To activate the cockpit speaker, press and hold the ICS button for one second. This will place all received audio over the cockpit speaker. 3.8 Alert Audio The PAC45A incorporates an independent alert audio system that can store nine audio messages recorded by the user, and played back when triggered by an external source. 200-045-1000 Page 3-4 Rev.
  • Page 26: Section Iv - Warranty And Service

    (2) years from the date of sale. During the first twelve (12) months of the two-year warranty period, PS Engineering, Inc., at its option, will send a replacement unit at our expense if the unit should be determined to be defective after consultation with a factory technician.
  • Page 27: Appendix A - Pac45A Installation Drawings

    Appendix A – PAC45A Installation Drawings Figure 5-1 - CTL45A Front View Figure 5-2 CTL45A Top View 200-045-1000 Appendix A Rev. 2, March 2019...
  • Page 28 Figure 5-3 - HUB45AR Top View P453 P451 J452 J454 Figure 5-4 - HUB45AR Rear Connector View 200-045-1000 Appendix A Rev. 2, March 2019...
  • Page 29 BLUETOOTH ANT CONN J455 Figure 5-5 HUB4A5R Front View Figure 5-6 - HUB45AR Side Views 200-045-1000 Appendix A Rev. 2, March 2019...
  • Page 30: Appendix B - Radio Interconnect Wiring

    Appendix B – Radio Interconnect Wiring Com 1 Audio Hi P452 Com 1 Lo Nav 1 Audio Hi Com 1 Mic Audio Hi P452 Nav 1 Audio Lo J451 Com 1 Mic Key Com 1 Mic Low Nav 2 Audio Hi Nav 2 Audio Lo Com 2 Audio Hi Com 2 Audio Low...
  • Page 31: Appendix C - Intercom Interconnect Wiring

    Appendix C – Intercom Interconnect Wiring Pilot Mic Audio Hi P451 Pilot Mic Lo Pilot Mic PTT Copilot Mic Audio Hi Copilot Mic Lo Copilot Mic PTT P454 P AX 4 I CS - PTT OBSR 1 Mic Audio Hi P AX 3 I CS - PTT OBSR 1 Mic PTT N o C onnect...
  • Page 32: Appendix D - Control Head Interconnect Wiring

    Appendix D – Control Head Interconnect Wiring PAC45 HUB LRU RX- RS422 TX - RX+ RS422 TX + TX- RS422 RX - TX+ RS422 RX + PILOT CTL45 HEAD P455 LIGHTING IN POWER AIRCRAFT GND P455 J455 NO CONNECTION J454 RX- RS422 TX - RX- RS422 TX - RX+ RS422 TX +...
  • Page 33: Appendix E, Unit Connector Wiring Reference

    Appendix E, Unit Connector Wiring Reference 9.1 J451 Connections C om 1 M ic A ud io H i C om 1 M ic K ey P451 C om 1 M ic L ow C om 2 M ic A ud io H i C om 2 M ic K ey C om 2 M ic L ow C om 3 M ic A ud io H i...
  • Page 34: J452 Connections

    9.2 J452 Connections Com 1 Audi o Hi Com 1 Lo Com 2 Audi o Hi Com 2 Audi o Low Com 3 Audi o Hi Com 3 Audi o Lo PAC45 CONNECTOR J452 Com 4 Audi o Hi MALE O N HARNESS Com 4 Audi o Low Com 5 Audi o Hi Com 5 Lo...
  • Page 35: J453 Connections

    9.3 J453 Connections P453 FEMALE ON HARNESS 9.4 J454 Connections J4 54 M A LE O N H A R N E S S P ILO T O B S E R V E R 2* C TL4 5A O B S E R V E R 1 C TL4 5A C O P ILO T C TL45 A...
  • Page 36: J455 Connections

    9.5 J455 Connections RX- RS422 TX - J455 RX+ RS422 TX + MALE ON HARNESS TX- RS422 RX - TX+ RS422 RX + P455 FEMALE ON HARNESS LIGHTING POWER AIRCRAFT GND ON CTL *OBS #2 OR PILOT PAC45G CTL45 HEAD HUB LRU * PILOT AND OBSVR #2 CONNECTIONS...
  • Page 37: Appendix F - Instructions For Faa Form 337 And Continuing Airworthiness

    Aircraft equipment list, weights and balance amended. Compass compensation checked. A copy of the operation instruc- tions, contained in PS Engineering document 202-045-( ), revision ( ), dated ( ), is placed in the aircraft records. All work accomplished listed on Work Order 10.2 Instructions for Continuing Airworthiness, Audio System...
  • Page 38: Appendix G - Rtca Do160G Environmental Qualification Form

    Appendix G – RTCA DO160G Environmental Qualification Form 11.1 Model Number PAC45A Audio Selector Panel/Intercom Remote Hub Part Number: 050-045-( ) FAA TSO Number: C139a, Manufacturer: PS Engineering Incorporated 9800 Martel Road Lenoir City TN 37772 Conditions Section Conducted Tests...
  • Page 39: Model Number Ctl45, Audio Selector Control Panel

    11.2 Model Number CTL45, Audio Selector Control Panel Part Number: 050-045-(02XX, -03XX, -62XX, -63XX ) FAA TSO Number: C139a Manufacturer: PS Engineering Incorporated 9800 Martel Road Lenoir City TN 37772 Conditions Section Conducted Tests Temperature and Altitude Equipment tested to CAT D1 Low Temperature 4.5.1...

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