Shadin Avionics AIS-360 ARINC User manual

AIS-360 ARINC LS/HS ADAPTER
P/N: 833610-01
INSTALLATION MANUAL
REV A
Shadin Avionics
6831 Oxford Street
St. Louis Park, MN 55426
USA
Sales: [phone]
Customer Service: [phone]
WWW.SHADIN.COM
MANUAL P/N: IM833610-01

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
PAGE CONTROL CHART
SECTION NO.DESCRIPTION PAGE
1. OVERVIEW
1.1 The Manual 1-1
1.2 Product Description 1-1
1.3 Specifications 1-2
2. INSTALLATION PROCEDURE
2.1 Mounting 2-1
2.2 Electrical Connections 2-1
3. ENVIRONMENTAL QUALIFICATION FORM 3-1
Environmental Qualification Form (Cont.) 3-2
4. INSTALLATION DRAWINGS AND INSTALL KIT PARTS LIST
Drawing No. Description/ Part Number REV
N/A Installation Dwg, AIS 833610-01 A
N/A Install Kit, P/N 833610 A

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
REVISION LOG
REV.
DATE
APP’D
ERN#
CHANGE
–
08-25-2010
ZK
1008/006
Baseline Release
A
09-22-2014
ZK
1409/004
Updated Vibration Test categories, Installation
Dwg and Install Kit Parts List
The information in this manual is subject to change without notification. To ensure complete and current updates,
note the Revision Log above and call Technical Assistance for updated information.

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
Page: 1-1
1. OVERVIEW
1.1 THE MANUAL
This manual is intended to guide the proper installation of the AIS-360 ARINC LS/HS Adapter. Installation
instructions should be read and followed.
1.2 PRODUCT DESCRIPTION
The AIS-360 ARINC LS/HS Adapter (P/N 833610-01) has two ARINC 429 Low speed input channels and two
ARINC 429 High speed output channels.
This unit receives any label on the ARINC 429 Low Speed input and outputs it on an ARINC 429 High Speed
bus with up to 440μsec delay.
All label data is unchanged and the update rate remains identical in the conversion.
(See example below).
Receive Low Speed ARINC 429
Output High Speed ARINC 429
Label
Rate
Description
Data
Label
Rate
Delay
314
50msec
True Heading
Unchanged
314
50msec
≤440μsec
The Block Diagram below depicts the intended use of the converter in the aircraft installation.
AIS-360
ARINC LS/HS ADAPTER
P/N 833610-01
ARINC 429
Low Speed Source
Ch 1
ARINC 429
Low Speed Source
Ch 2
ARINC 429
High Speed Destination
Ch 1
ARINC 429
High Speed Destination
Ch 2

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
Page: 1-2
1.3 SPECIFICATIONS
Physical Specifications
Dimensions: 8.50”L x 4.00”W x 1.59”H
Weight: 0.9 lbs
Mounting: Screw size #8
Mounting Locations: 7.878”L x 1.752”W
Electrical and Functional
Power Supply Voltage: +18VDC to +33VDC
Supply Current: 100mA Max
Protection: Not internally fused
Inputs: ARINC 429: Low Speed, 12-14.5Kbps 1%
Outputs: ARINC 429: High Speed, 100Kbps 1%
Environmental
RTCA/DO-160F Categories:
A2-CAB[R(B, B1) U2(F, F1)]XXXXXXZ[AXX]AR[CC][WW]M[A3J33]XXAX
Operating Temperature: -15 C to +70 C
Storage Temperature: -55 C to +85 C
Operating Altitude: Up to 50,000ft
In-Flight loss of Cooling: Equipment can run indefinitely with no cooling
MIL-HDBK-217 MTBF 30,000 hours

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
Page: 2-1
2. INSTALLATION PROCEDURE
2.1 MOUNTING
The AIS-360 ARINC LS/HS Adapter (P/N 833610-01) should be mounted in a partially controlled temperature,
and pressurized or un-pressurized locations.
The converter should be mounted according to Installation Dwg, P/N ID833610-01.
2.2 ELECTRICAL CONNECTIONS
Connection to Power Supply +28 VDC
833610-01
Description
J1:3, 22
To
+28VDC-IN
J1:2, 21
To
Power GND-IN
Inputs
833610-01
Description
J1:27
To
ARINC-429-RXA-1
J1:28
To
ARINC-429-RXB-1
J1:29
To
ARINC-429-RXA-2
J1:30
To
ARINC-429-RXB-2
Outputs
833610-01
Description
J1:8
To
ARINC-429-TXA-1
J1:9
To
ARINC-429-TXB-1
J1:10
To
ARINC-429-TXA-2
J1:11
To
ARINC-429-TXB-2

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
Page: 3-1
3.0 ENVIRONMENTAL QUALIFICATION FORM (EQF)
This Environmental Qualification Form describes qualification testing performed on the 833610-00 Data
Converter. The 833610-01 is qualified by similarity to the 833610-00 converter. The 833610-01 is therefore
qualified to RTCA/DO-160F standards.
NOMENCLATURE: AIS-360 ARINC LS/HS ADAPTER
TYPE/MODEL/PART NO: 833610-01 TSO NUMBER:
MANUFACTURER'S SPECIFICATION AND/OR OTHER APPLICABLE SPECIFICATION:
RTCA/DO-160F
MANUFACTURER: Shadin Avionics
ADDRESS: 6831 Oxford Street, St. Louis Park, Minnesota 55426-4412
CONDITIONS
SECTION
DESCRIPTION OF
TESTS CONDUCTED
Temperature and Altitude
4.0
Tested to Category A2.
Low Temperature
High Temperature
-15˚C
+70˚C
Altitude
Decompression
Overpressure
50,000ft
55,000ft
-15,000ft
Temperature Variation
5.0
Tested to Category C.
Humidity
6.0
Tested to Category A.
Operational Shock and Crash Safety
7.0
Tested to Category B.
Vibration
8.0
Tested to Category R (B, B1).
Tested to Category U2 (F, F1)
Explosion
9.0
Identified as Category X.
Not tested.
Waterproofness
10.0
Identified as Category X.
Not tested.
Fluids Susceptibility
11.0
Identified as Category X.
Not tested.

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
Rev: A
P/N 833610-01
Page: 3-2
ENIRONMENTAL QUALIFICATION FORM (Cont.)
CONDITIONS
SECTION
DESCRIPTION OF
TESTS CONDUCTED
Sand and Dust
12.0
Identified as Category X.
Not tested.
Fungus
13.0
Identified as Category X.
Not tested.
Salt Spray
14.0
Identified as Category X.
Not tested.
Magnetic Effect
15.0
Tested to Category Z.
Power Input
16.0
Tested to Category AXX.
Voltage Spike
17.0
Tested to Category A.
Audio Frequency Susceptibility
18.0
Tested to Category R.
Induced Signal Susceptibility
19.0
Tested to Category CC.
Radio Frequency Susceptibility
20.0
Tested to Category WW.
Radio Frequency Emission
21.0
Tested to Category M.
Lightning Induced Transient Susceptibility
22.0
Tested to Category A3J33.
Lightning Direct Effects
23.0
Identified as Category X.
Not tested.
Icing
24.0
Identified as Category X.
Not tested.
Electrostatic Discharge
25.0
Tested to Category A.
Fire, Flammability
26.0
Identified as Category X.
Not tested.

IM833610-01A.DOC IM833610-01 Shadin Avionics
INSTALLATION MANUAL
AIS-360 ARINC LS/HS ADAPTER
P/N 833610-01
SECTION 4.0
INSTALLATION DRAWINGS AND
INSTALL KIT PARTS LISTS
The following drawings are arranged in the sequence specified on page i of the Page Control Chart.

0.70±0.10
17.8±2.5
4.20±0.10
106.7±2.5
45.7±2.5
1.80±0.10
7.22
183.4
8.50
215.9
4.00
7.878
200.1
4.83
4X
17.8
0.190
3
44.5
2X
101.6
0.70
3.20 1.752
81.3
4.238
107.65
PIN 1
PIN 37
5
1.47
37.3
0.686
17.42
40.4
1.59
4.00
101.6
C
B
UNLESS OTHERWISE SPECIFIED:
REV
P/N
PROJECTION
DRAWN PER ASME 14.5M-2009
ID833610-01A.PDF
AIS 833610-01
SHEET 1 OF 1SCALE: N/A
A
54321
D
SIZE
F/N
0.005
N/A
INSTALLATION DWG,
DIMENSIONS ARE IN INCHES
SHADIN AVIONICS PROPRIETARY INFORMATION ALL RIGHTS RESERVED
ST. LOUIS PARK, MN 55426
CAGE CODE:
MATERIAL
FINISH
ENG APPR.
CHECKED
DRAWN HWL
ZK
ZK 8/24/2010
8/24/2010
ID833610-01
8/24/2010
A
0Z5P5
A
TOLERANCES:
X/X 1/64
X.X 0.1
X.X 0.1
X.XX 0.01
X.XXX
THIRD ANGLE
N/A
REVISIONS
ERN # REV. DATE B APP'D DESCRIPTION
1008/006 - 8/24/2010 HWL ZK BASELINE RELEASE
1409/004 A 9/12/2014 EG ZK ADDED CHASSIS-GND, REDRAWN
NOTES:
1. DIMENSIONS SHOWN IN INCH [mm] FOR REFERENCE ONL .
2. PH SICAL SIZE, EXCLUDING SCREW HEADS:
- 8.50" (L) X 4.00" (W) X 1.47" (H)
MOUNTING SCREW SIZE IS NO. 8.
4. WEIGHT = 0.9 LBS
J1 CONNECTOR
- 37 PIN D-SUB, MALE
- WIRE T PE "STP" IS SHIELDED TWISTED PAIR
6. MATING CONNECTOR IS A STANDARD 37 PIN FEMALE D-SUB.
- STP WIRE SHIELDS SHOULD BE TIED TO MATING CONNECTOR SHELL.
3
5
5
WHERE USED
NEXT ASSEMBL USED ON
IM833610-01 833610-01
WHERE USED
NEXT ASSEMBL USED ON
IM833610-01 833610-01
PIN SIGNAL NAME DESCRIPTION TYPE (REF) PAIR (REF)
1 CHASSIS-GND CHASSIS GROUND N/A N/A
2 POWER-GND-IN POWER RETURN SINGLE N/A
3 +28V-IN 28 VDC POWER POSITIVE SINGLE N/A
4 RESERVED N/A N/A N/A
RESERVED N/A N/A N/A
6 RESERVED N/A N/A N/A
7 RESERVED N/A N/A N/A
8 ARINC-429-TXA-1 ARINC 429 OUTPUT #1 (LINE A) STP PIN 9
9 ARINC-429-TXB-1 ARINC 429 OUTPUT #1 (LINE B) STP PIN 8
10 ARINC-429-TXA-2 ARINC 429 OUTPUT #2 (LINE A) STP PIN 11
11 ARINC-429-TXB-2 ARINC 429 OUTPUT #2 (LINE B) STP PIN 10
12 RESERVED N/A N/A N/A
13 RESERVED N/A N/A N/A
14 RESERVED N/A N/A N/A
1 RESERVED N/A N/A N/A
16 RESERVED N/A N/A N/A
17 RESERVED N/A N/A N/A
18 RESERVED N/A N/A N/A
19 RESERVED N/A N/A N/A
20 SPARE 1 UNUSED PIN N/A N/A
21 POWER-GND-IN POWER RETURN SINGLE N/A
22 +28V-IN 28 VDC POWER POSITIVE SINGLE N/A
23 RESERVED N/A N/A N/A
24 RESERVED N/A N/A N/A
2 RESERVED N/A N/A N/A
26 RESERVED N/A N/A N/A
27 ARINC-429-RXA-1 ARINC 429 INPUT #1 (LINE A) STP PIN 28
28 ARINC-429-RXB-1 ARINC 429 INPUT #1 (LINE B) STP PIN 27
29 ARINC-429-RXA-2 ARINC 429 INPUT #2 (LINE A) STP PIN 30
30 ARINC-429-RXB-2 ARINC 429 INPUT #2 (LINE B) STP PIN 29
31 RESERVED N/A N/A N/A
32 RESERVED N/A N/A N/A
33 RESERVED N/A N/A N/A
34 RESERVED N/A N/A N/A
3 RESERVED N/A N/A N/A
36 RESERVED N/A N/A N/A
37 RESERVED N/A N/A N/A
J1 CONNECTOR PIN OUT

Shadin Avionics
File Name: IK833610A.DOC
DIRECTORY: IKXXXX
ERN Date: September 8, 2011 ERN #: 1109/004
Rev: A Release Date: 10-07-2011
Sec.: IX Approved: ZK
Page 1 of 1
PARTS LIST Part #: IK833610
Drawing #s: NA Description: INSTALL KIT, P/N 833610
FN P/N QTY. DESCRIPTION MFG. MFG.# DESIGNATION COMMENTS
Shadin Avionics Confidential & Proprietary Information - ALL RIGHTS RESERVED
5 230055 20 CONTACT, Crimp D-Sub, Fem, 20-24, M39029/63-368 POS M39029/63-368
(FC6020D) 12 pcs needed, 8 pcs are spares.
10 230082 1 CONN HOOD, 37 Pin D-Sub ST CIN DC-24660
15 232002 1 CONN SHELL, 37 Pin D-Sub, Fem Crimp AMP 205167-1
20 239001 1 TOOL, Insertion/Extraction DAN M81969/1-02
25 512101 2 RETAINER CLIP, "Bow Tie" Style KEY 2061K
30 753217 1 Thermal Label, 4"x 1" ULI S-8601
35 PK1001 1 BAG, 2.5 x 3, 4 MIL Zip Lock
40 PK1007 1 BAG, 6 x 8, 4 MIL
28 items