This document and the information contained herein is the proprietary data of SANDIA aerospace Corporation.
No part of this document may be transmitted, reproduced, or copied in any form or by any means without the prior
written consent of SANDIA aerospace. Due to SANDIA aerospace’s continued product and quality improvement
programs, information contained in this document is subject to change without prior notice
Copyright 2010 SANDIA aerospace Corporation, All right rights reserved. Printed in USA
Information Subject To Export Control Laws
Record of Revisions
Revision
-120120222DRN 402L. Harrison
-220120308ECN 3884L. Harrison
-320130311ECN 3916L. Harrison
-420130926ECN 4004L. Harrison
DateDescriptionApproval
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Table of Contents
Record of Revisions ....................................................................................................................................1
Table of Contents .......................................................................................................................................2
List of Illustrations .....................................................................................................................................3
Section 1 General Description ...................................................................................................................4
This manual describes the installation of the SANDIA aerospace STX 165 and STX 165 Mode C transponders. It is
intended for use by FAA certi! ed repair stations to install the STX 165 and STX 165R transponders and includes both mechanical and electrical installation information. Calibration, system con! guration and checkout procedures are included.
The installer should ensure that all functions are operating according to their intended purpose in their particular installation.
1.2 STX 165 / STX 165R Product Description
The STX 165 is a self contained, panel mounted Mode A/C transponder with a built-in 35K foot altitude encoder. The
built-in encoder supplies altitude data to the STX 165 for altitude reporting (Mode C) and outputs the altitude data on an
RS 232 data bus for interface to other avionics systems that require altitude data. A SANDIA aerospace STP 78 OAT
probe, P/N 305561-91 can be installed as an option. When the STP 78 is installed, the STX 165 will display OAT (Outside Air Temperature), Density Altitude and Icing Alert.
The STX 165R is a Remote Mode A/C transponder that accepts attitude data from altitude encoders, such as the SANDIA
SAE 5-35, in either a Gilham Grey code or RS 232 format.
Both units rely to ATCRABS interrogations with one of 4096 possible ‘squawk’ codes.
1.3 Technical Characteristics
1.3.1 Physical Characteristics
1.3.1.1 STX 165 Panel Mount
1/2 3ATI Panel Cut OutBehind Panel Dimensions1.78”H x 3.5”W x 7.34”L (4.52cm x 8.89cm x 18.64cm)
Weight: 1.30 Lbs. (.59 kg)
1.3.1.2 STX 165R Remote Mount Unit
Dimensions:3.5” H x 1.8”W x 6.9”L (8.89cm x 4.57cm x17.53cm)
Weight: 1.16 Lbs. (.526 kg)
1.3.2 Electrical Characteristics- STX 165 and STX 165R
Power Out: 200 Watts Nominal
1.3.3.1 STX 165 Panel Mount
Operational Voltage: 11-32VdcCurrent: All Current readings are with the encoder heater onAircraft Power PRF Squawk Code Watts Current
TSO: C74d (transponder)
C88b (encoder) STX 165 panel mount only
Software: DO-178B Level C
Environmental: DO-160F
STX 165 [(A4C4)X]CAB(SM)XXXXXXZBAB[BC][TT]M[XXXXX]XXXX
STX165R [(A4C4)X]CAB(SM)XXXXXXZBAB[BC][TT]M[XXXXX]XXXX
FCC ID YJL-DAF-JDX
“The conditions and test required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install the article either on or within a speci! c type
or class of aircraft to demonstrate that the aircraft installation conditions are within the TSO standards.
The article may be installed only if installation of the article is approved by the Administrator.
306100-00
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Environmental Quali• cation Form for the STX 165 Mode C Transponder
MANUFACTURER: SANDIA AEROSPACE
ADDRESS: 3700 OSUNA RD NE, SUITE 711, ALBUQUERQUE, NM 87109
REVISION & CHANGE NUMBER OF DO-160 : REV F DATED December 6, 2007
DATE OF TESTS: 2012
CONDITIONSECTIONDESCRIPTION OF TESTS CONDUCTED
Temperature and Altitude
Low Temperature
High Temperature
In-Flight Loss of Cooling
Altitude
Decompression
Overpressure
4.3
4.5.5
4.5.2
4.5.4
4.6.1
4.6.2
4.6.3
Equipment Tested to Category A4/C4
-20oC Operating Cold Temp
+55oC Operating High Temp
Test not Applicable
35,000 feet
30,000 feet
-15,000 feet
Temperature Variation5.0Tested to Category C, 2C/Min
Humidity6.0Tested to Category A
Operational Shock and Crash
7.0Tested to Category B, Aircra Type 5. Random Orientation
Safety
Vibration8.0Tested to Category S, Aircra Zone 2, Vib curve M
Explosion9.0Equipment Identi ed as Category X, No Test Performed
Waterproofness10.0Equipment Identi ed as Category X, No Test Performed
Fluids Susceptibility11.0Equipment Identi ed as Category X, No Test Performed
Sand and Dust12.0Equipment Identi ed as Category X, No Test Performed
Fungus13.0Equipment Identi ed as Category X, No Test Performed
Salt Spray14.0Equipment Identi ed as Category X, No Test Performed
Magnetic E ect15.0Equipment is Category Z
Power Input16.0Tested to Category B
Voltage Spike17.0Tested to Category A
Audio Frequency Susceptibility18.0Tested to Category B
Induced Signal Susceptibility19.0Tested to Category BC
Radio Frequency Susceptibility20.0Tested to Category TT
Radio Frequency Susceptibility21.0Tested to Category M
Lightning Induced Transient
22.0Equipment Identi ed as Category X, No Test Performed
Susceptibility
Lightning Direct E ects23.0Equipment Identi ed as Category X, No Test Performed
Icing24.0Equipment Identi ed as Category X, No Test Performed
Electrostatic Discharge25.0Equipment Identi ed as Category X, No Test Performed
Flammability26.0Equipment Identi ed as Category X, No Test Performed
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