SM74
AA30-301
Expansion Panel
INSTALLATION AND OPERATION MANUAL
REV 4.10 October 16, 2006
Northern Airborne Technology Ltd.
1925 Kirschner Road
Kelowna, BC, Canada.
V1Y 4N7
Telephone (250) 763-2232
Facsimile (250) 762-3374
Copyright 2006 by Northern Airborne Technology
CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
SM74 Rev. 4.10 |
AA30-301 Expansion Panel Manual |
Periodically NAT will release manual amendments. In order to maintain the most accurate and up to date manual these amendments should be carried out immediately upon receipt and recorded on the following amendment record.
Amendment |
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Changed |
Entered |
Note: Revision 4.00 was the first public release of this document
Insert any Amendment Instruction sheets after this page.
Oct 16, 2006 |
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ENG-FORM: 820-0110.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
SM74 Rev. 4.10 |
AA30-301 Expansion Panel Manual |
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Table of Contents |
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Section |
Title |
Page |
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1 |
Description |
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1.1 |
Introduction |
1-1 |
1.2 |
Purpose of Equipment |
1-1 |
1.3 |
Features |
1-1 |
1.4 |
Specifications |
1-1 |
1.4.1 |
Electrical Specifications |
1-1 |
1.4.2 |
Physical Specifications |
1-3 |
1.4.3 |
Environmental Specifications |
1-3 |
1.4.4 |
Certification |
1-4 |
2 |
Installation |
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2.1 |
Introduction |
2-1 |
2.2 |
Unpacking and Inspection |
2-1 |
2.2.1 |
Warranty |
2-1 |
2.3 |
Installation Procedures |
2-1 |
2.3.1 |
Warnings |
2-1 |
2.3.2 |
Cautions |
2-2 |
2.3.3 |
Cabling and Wiring |
2-2 |
2.3.4 |
Post-Installation Checks |
2-2 |
2.3.5 |
Adjustments |
2-3 |
2.4 |
Continued Airworthiness |
2-3 |
2.5 |
Accessories Required But Not Supplied |
2-4 |
2.6 |
Installation Drawings |
2-4 |
3 |
Operation |
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3.1 |
Introduction |
3-1 |
3.2 |
General |
3-1 |
3.3 |
Controls and Indicators |
3-1 |
3.3.1 |
Transmitter Selection |
3-2 |
3.3.2 |
Receiver Selection |
3-2 |
Oct 16, 2006 |
Page iii |
ENG-FORM: 820-0110.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
SM74 Rev. 4.10 |
AA30-301 Expansion Panel Manual |
Section 1 Description
This manual contains information on the AA30-301 Expansion Panel. All derivative products will be covered by manual supplements, which can be obtained from NAT as required.
Information in this section consists of purpose of equipment, features and specifications.
The AA30-301 is a Dzus-mounted 4-transceiver radio receiver expansion panel, designed to work in conjunction with the 380-series Audio Selector Panels.
The AA30-301 provides four ganged transmitter selector pushbutton switches and four receiver level panel potentiometers, each with an integral push-in / push-out selector switch, and utilizes the subassembly from a 247 Audio Mixing Amplifier for signal mixing, amplification and processing.
The AA30-301 is designed to be used in conjunction with a 380 panel to expand a single 380-series transmit microphone output into 4 outputs, and to expand a single
380-series receive audio input into 4 inputs.
The AA30-301 permits the audio system to support more receivers/transceivers than a single 380-series panel is capable of individually.
Power Supply |
Linear regulated |
supply with input reverse-polarity and |
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overvoltage protection. |
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Operating: |
Nominal |
28.0 |
Vdc |
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Minimum |
22.0 |
Vdc |
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Maximum |
30.3 Vdc |
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Current |
0.18 |
A max. (0.04 A nom.) |
Lighting: |
Nominal |
28.0 |
Vdc |
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Maximum |
30.3 Vdc |
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Current |
0.25 |
A max. (0.17 A nom.) |
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Oct 16, 2006 |
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ENG-FORM: 800-0108.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
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AA30-301 Expansion Panel Manual |
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SM74 Rev. 4.10 |
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Input Signals |
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Description |
Q'ty |
Level |
Impedance |
Circuitry Type |
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Receiver Audio (J101) |
4 |
Rated: |
2.1 kΩ |
audio, unbalanced |
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COM1 RX IN |
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5.5 Vrms |
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Range: |
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COM2 RX IN |
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COM3 RX IN |
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0.8 to 8.0 Vrms |
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COM4 RX IN |
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Transmitter Mic (J102) |
1 |
250 mVrms |
n/a |
direct connection |
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nominal |
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through switch |
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COM MIC IN |
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contact |
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Transmitter Key (J102) |
1 |
1 A max. |
n/a |
direct connection |
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through switch |
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COM KEY IN |
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contact |
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Output Signals |
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Description |
Q'ty |
Level |
Impedance |
Circuitry Type |
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Receiver Audio (J101) |
1 |
Rated: |
Output: 100 Ω |
audio, unbalanced |
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4.0 Vrms |
Rated Load: |
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RX AUDIO OUT |
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[27 mW] |
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600 Ω |
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Transmitter Mic (J102) |
4 |
n/a |
n/a |
direct connection, |
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COM1 MIC OUT |
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switch contact |
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COM2 MIC OUT |
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COM3 MIC OUT |
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COM4 MIC OUT |
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Transmitter Key (J102) |
4 |
n/a |
n/a |
direct connection, |
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COM1 KEY OUT |
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switch contact |
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COM2 KEY OUT |
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COM3 KEY OUT |
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COM4 KEY OUT |
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1.4.1.1Audio Performance (TSO-C139 and RTCA/DO-214 Class Ib)
Applicable to serial numbers 3001 and above.
Audio Frequency Response |
≤3 dB variance, 300 to 5500 Hz |
Spurious Response |
≥50 dB below Rated Output Power |
Distortion |
≤10% at Rated Output Power |
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≤3% THD+N at 10% Rated Output Power |
Output Regulation |
≤3 dB change |
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Page 1-2 |
Oct 16, 2006 |
ENG-FORM: 800-0108.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
SM74 Rev. 4.10 |
AA30-301 Expansion Panel Manual |
Crosstalk: Input to Output |
≥55 dB below reference signal |
Input to Input |
≥60 dB below reference signal |
Input to Mic Output |
≤1.0 mV |
Intermodulation Distortion |
≥30 dB below reference tones |
Audio Noise without signal |
≥50 dB below Rated Output Power |
Signal plus noise degradation |
>9 dB signal plus noise-to-noise |
Height |
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1.14" (28.8 mm) max |
Depth behind panel |
6.22" (158.0 mm) max excluding connectors |
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Width |
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5.02" (127.5 mm) max behind panel |
Weight |
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1.15 lb (0.52 kg) max |
Mounting |
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Dzus rail, 4 fasteners 5.366" horizontal spacing, |
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0.750" vertical spacing |
Faceplate |
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Laser-engraved edge-lit panel with blue/white |
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lighting |
Material/Finish |
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Chassis and cover are 5052-H32 brushed |
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aluminum with chromate conversion finish. |
Connectors: |
J101 |
Receive I/O and Power Connections |
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One male 25-pin D-subminiature connector |
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with jackpost hardware |
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J102 |
Mic and Key I/O Connections: |
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One female 25-pin D-subminiature connector |
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with jackpost hardware |
Installation kit: |
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AA12-IKC (D25P25SL-IKC) |
Temperature |
-55 °C to +70 °C |
Altitude |
+55,000 ft. |
Humidity |
>95%, 48 hours |
Shock |
6g for 11 ms in all axes |
Qualification: |
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Oct 16, 2006 |
Page 1-3 |
ENG-FORM: 800-0108.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
AA30-301 Expansion Panel Manual |
SM74 Rev. 4.10 |
Up to serial number 3000:
Internal Model 247 amplifier subassembly meets the requirements of TSO-C50c and RTCA/DO-160CEnv.Cat:[A2F2]-BA[CL]XXXXXXZ[BZ]AAATZ[XXC2]XX.
Serial number 3001 and higher:
RTCA/DO-160E Env. Cat. [(A2)(F2)-]BAB[(RBB1)(SM)]XXXXXXZZAZ[AC][TT]M[XXC1X]XXXX
Note: Refer to the Environmental Qualification Form in Section 2.6 of this manual for complete details of the environmental categories.
Applicable to serial number 3001 and above:
FAA TSO-C139 |
Aircraft Audio Systems and Equipment |
RTCA DO-214 Class Ib |
Audio Systems characteristics and minimum operational |
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performance standards for audio systems and equipment. |
End of section 1
Page 1-4 |
Oct 16, 2006 |
ENG-FORM: 800-0108.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
SM74 Rev. 4.10 |
AA30-301 Expansion Panel Manual |
Section 2 Installation
Information in this section consists of: unpacking and inspection procedures, installation procedures, post-installation checks, and installation drawings.
Unpack the equipment carefully and locate the warranty card. Inspect the unit visually for damage due to shipping and report all such claims immediately to the carrier involved. Note that each unit should have the following:
-AA30-301 Expansion Panel
-Warranty Card
-Operator’s Manual
-Release certification
Verify that all items are present before proceeding and report any shortage immediately to your supplier.
Complete the warranty card information and send it to NAT when the installation is complete. If you fail to complete the warranty card, the warranty will be activated on date of shipment from NAT.
Note: An appropriately rated facility, e.g. Certified Aircraft Repair Station, must install this equipment in accordance with applicable regulations. NAT Ltd’s warranty is not valid unless the equipment is installed by an authorized NAT Dealer. Failure to follow any of the installation instructions, or installation by a non-certified individual or agency will void the warranty, and may result in a non-airworthy installation.
Do not bundle any lines from this unit with transmitter coax lines. Do not bundle any audio or DC power lines from this unit with 400 Hz synchro wiring or AC power lines. Do not position this unit or wiring from this unit next to any device with a strong alternating magnetic field such as an inverter, or significant audio interference will result.
Oct 16, 2006 |
Page 2-1 |
ENG-FORM: 805-0107.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.
AA30-301 Expansion Panel Manual |
SM74 Rev. 4.10 |
In all installations, use shielded cable exactly as shown and ground as indicated.
Significant ground loop and noise problems may result from not following these guidelines.
The shielding and routing of the receive audio lines used in the AA30-301 installation is very critical and poor performance of the aircraft audio system will result if the installation shown on Interconnect drawing AA30\301\403-0 and -1 is not followed.
All unshielded wire shall be selected in accordance with AC43.13-1B Change 1,
Paragraphs 11-76 through 11-78. Wire types should be to MIL-W-22759 as specified in AC43.13-1B Change 1, Paragraphs 11-85, 11-86, and listed in Table 11-11. For shielded wire applications, use Tefzel MIL-C-27500 shielded wire with solder sleeves (for shield terminations) to make the most compact and easily terminated interconnect.
Follow the wiring diagrams in Section 2.6 as required.
Allow 3 inches from the end of the wire to the shield termination to allow the hood to be easily installed. Note that the hood is a ‘clamshell’ hood, and is installed after the wiring is complete.
All wiring should be at least 22 AWG, except power and ground lines, which should be at least 20 AWG. Ensure that all ground connections are clean and well secured.
2.3.4Post-Installation Checks
2.3.4.1 Voltage/Resistance Checks
Check the following:
a)P101 pin <13> for +28 Vdc avionics buss voltage.
b)P101 pin <12> for +28 Vdc lighting buss voltage.
c)P101 pins <15> <16> <18> <20> <22> and <25> for continuity to ground (power).
d)P101 pin <24> for continuity to ground (lighting).
2.3.4.2Power On Checks
WARNING:
High volume settings can cause hearing damage.
Set the headset volume control to the minimum volume setting prior to conducting audio tests, and slowly increase the headset volume level to a comfortable listening level.
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Oct 16, 2006 |
ENG-FORM: 805-0107.DOT |
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CONFIDENTIAL AND PROPRIETARY TO NORTHERN AIRBORNE TECHNOLOGY LTD.