DO-160

DO-160

Product catalog summary
Contact Information
Ebertstraße 30a, 52134 Herzogenrath, Germany
Phone: +49 (0) 2407 577-0
Email: [email protected]
Website: www.head-acoustics.com
DO-160 Compliance Summary – HEADlab
This document provides a summary of the compliance of HEADlab products with the RTCA DO-160 standards, which outline environmental conditions and test procedures for airborne equipment. The document is a data sheet, last updated on December 25, and is subject to change.
Key Parameters and Conditions
  • Temperature: Severe operating conditions are tested under Category A1, with a range of -15 °C to +55 °C, and an extended tested range of -20 °C to +60 °C. Operation below -20 °C requires thermal isolation.
  • Steady State Altitude: Tested under Category A2, including cabin loss of pressure from 2000 ft to 14000 ft in 2 minutes and 1.5 bar pressure.
  • Temperature Variation: Category C.
  • Humidity: Category C.
  • Operational Shocks: Category D, with 30 g, 20 ms, 3 axes, both directions.
  • Crash Safety: Category E, with impulse 20 g, 20 ms, 3 axes, and sustained 9 g, 3 s, 3 axes.
  • Operational Vibrations: Category S, with sine sweep 6 g, 10 Hz to 2000 Hz, 1 oct/min., 3 axes. Note: SNR of analog modules may be reduced during vibration excitation.
  • Magnetic Effect: Category A.
  • EMC Emission: Category M.
Tested Products
  • labCTRL II.1 (Code 3704)
  • labSAR I.1 (Code 3705.1)
  • labSWP-8 (Code 3707.2-8)
  • labSSD I (Code 3706.1)
  • labVF6 II (Code 3752)
  • labV12 II (Code 3753)
  • labV24 II (Code 3755)
Summary
The HEADlab products listed have been rigorously tested for environmental resistance and reliability according to the RTCA DO-160 guidelines. These tests ensure that the equipment performs safely and consistently under demanding conditions, meeting the high requirements for use in aircraft applications.
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Catalog excerpts

DO-160-1

DATA SHEET Conformities of HEAD/ab products in aircraft applications based on Environmenta/ Conditions and Test Procedures for Airborne Equipment (RTCA DO-160) The following HEAD/ab products have been extensively tested for environmental resistance and reliability in accordance with the RTCA DO-160 test guideline Environmenta/ Conditions and Test Procedures for Airborne Equipment. DO-160 defines stringent and aviation-proven test methods that help ensure equipment performs safely and consistently under demanding real-world conditions. This data sheet summarises the tested products and the tests performed according to selected parameters. The results serve as proof that the devices meet the high requirements for use in aircraft applications. RESULTS > /abCTRL II.1 (Code 3704) 1 Cat. A1 specifies -15 °C to +55 °C. Tested range -20 °C to +60 °C. 2 Operation below -20 °C requires thermal isolation. 3 Also tested: cabin loss of pressure from altitude 2000 ft to 14000 ft in 2 minutes. 4 Also tested: 1.5 bar pressure. 5 SNR of analog modules may be reduced during vibration excitation. Contact Information E-Mail: [email protected] DO-160 Compliance Summary - HEAD/ab, Rev. 01, Subject to change, last update: 12/25 Website: www.head-acoustics.com

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All HEAD acoustics GmbH catalogs and technical brochures

  1. HRT I

    8  Pages

  2. HRR I

    3  Pages

  3. labSAR I

    6  Pages

  4. labM6 II

    7  Pages

  5. labV8x3-Iso II

    11  Pages

  6. labV24 II

    7  Pages

  7. labV12 II

    7  Pages

  8. labVF6-Iso II

    9  Pages

  9. labVF6 II

    7  Pages

  10. labCOMPACT12 II

    10  Pages

  11. BHS II

    4  Pages

  12. RC X.1

    3  Pages

  13. SQuadriga III

    26  Pages

  14. MCP I.24

    1  Page

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