• Shopping Cart
    There are no items in your cart

SAE AS5681B

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Minimum Operational Performance Specification for Remote On-Ground Ice Detection Systems

Available format(s)

Hardcopy , PDF

Superseded date

03-09-2024

Superseded by

SAE AS5681C

Language(s)

English

Published date

17-05-2016

€160.44
Excluding VAT

1. SCOPE
2. REFERENCES
3. GENERAL DESIGN REQUIREMENTS
4. MINIMUM PERFORMANCE SPECIFICATION
5. MINIMUM PERFORMANCE SPECIFICATION IN
   ENVIRONMENTAL TEST CONDITIONS
6. MINIMUM OPERATIONAL PERFORMANCE TESTS
7. INSTALLED EQUIPMENT OPERATIONAL EVALUATION
8. NOTES
APPENDIX A - TEST MATRICES
APPENDIX B - DETAILED TEST PARAMETERS
APPENDIX C - ILLUMINATION REQUIREMENTS
APPENDIX D - DETERMINATION OF ROGIDS
             ACCEPTABLE LATENT FAILURE RATE

Describes the minimum performance requirements of Remote On-Ground Ice Detection Systems (ROGIDS).

DocumentType
Standard
Pages
54
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of Remote On-Ground Ice Detection Systems (ROGIDS). These systems are ground-based. They provide information that indicates whether frozen contamination is present on aircraft surfaces.Section 1 provides information required to understand the need for the ROGIDS, ROGIDS characteristics, and tests that are defined in subsequent sections. It describes typical ROGIDS applications and operational objectives and is the basis for the performance criteria stated in Section 3 through Section 5.Section 2 provides reference information, including related documents, abbreviations, and definitions.Section 3 contains general design requirements for the ROGIDS.Section 4 contains the Minimum Operational Performance Requirements for the ROGIDS, which define performance in icing conditions likely to be encountered during ground operations.Section 5 describes environmental test conditions that provide laboratory means of testing the overall performance characteristics of the ROGIDS in conditions that may be encountered in actual operations.Section 6 describes recommended test procedures for demonstrating compliance with Sections 3 and 4.Section 7 contains the operational evaluation requirements for verifying the performance of the ROGIDS when installed for in-service use.

FAA AC 120-107 : 2011 USE OF REMOTE ON-GROUND ICE DETECTION SYSTEM
SAE AS6285 Aircraft Ground Deicing/Anti-Icing Processes

FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
SAE ARP5945 Endurance Time Tests for Aircraft Deicing/Anti-icing Fluids SAE Type I
SAE ARP1971C Aircraft Deicing Vehicle – Self-Propelled
SAE AMS1424M Deicing/Anti-Icing Fluid, Aircraft SAE Type 1
SAE ARP926B FAULT/FAILURE ANALYSIS PROCEDURE
SAE AMS1428J Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 20-117 : 1982 HAZARDS FOLLOWING GROUND DEICING AND GROUND OPERATIONS IN CONDITIONS CONDUCIVE TO AIRCRAFT ICING
SAE J1211_201211 Handbook for Robustness Validation of Automotive Electrical/Electronic Modules
RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
FAA AC 120-58 : 0 PILOT GUIDE FOR LARGE AIRCRAFT GROUND DEICING
CFR 47(PTS0-19) : OCT 2017 TELECOMMUNICATION - FEDERAL COMMUNICATIONS COMMISSION
SAE ARP4761 GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
SAE ARP5485A Endurance Time Tests for Aircraft Deicing/Anti-icing Fluids SAE Type II, III, and IV
SAE ARP4737H Aircraft Deicing/Anti-icing Methods
EN 50081-2:1993 Electromagnetic compatibility - Generic emission standard - Part 2: Industrial environment
FAA AC 150/5300-14 : 2008 DESIGN OF AIRCRAFT DEICING FACILITIES
FAA AC 120-107 : 2011 USE OF REMOTE ON-GROUND ICE DETECTION SYSTEM
RTCA DO 216 : 1993 MINIMUM GENERAL SPECIFICATION FOR GROUND-BASED ELECTRONIC EQUIPMENT
EN 50082-2 : 95 AC 95 ELECTROMAGNETIC COMPATIBILITY - GENERIC IMMUNITY STANDARD - INDUSTRIAL ENVIRONMENT
FAA AC 135-16 : 0 GROUND DEICING AND ANTI-ICING TRAINING AND CHECKING
FAA AC 120-60 : 2004 GROUND DEICING AND ANTI-ICING PROGRAM
SAE ARP 4256 : 2001 DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT
FAA AC 135-17 : 0 PILOT GUIDE SMALL AIRCRAFT GROUND DEICING
ARINC 415 : LATEST OPERATIONAL/TECHNICAL GUIDELINES ON FAILURE WARNING & FUNCTIONAL TEST
FAA AC 00-34 : 0 AIRCRAFT GROUND HANDLING AND SERVICING

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.