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SAE AS 5681 : 2016

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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Superseded date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Superseded by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:2024

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).

Committee
G-12HOT
DocumentType
Revision
Pages
54
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

FAA AC 120-107 : 2011 USE OF REMOTE ON-GROUND ICE DETECTION SYSTEM
SAE AS 6285 : 2016 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 ARP 5945 : 2007 ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 1 AIRCRAFT DEICING/ANTI-ICING FLUIDS
SAE ARP 1971 : 2011 AIRCRAFT DEICING VEHICLE - SELF-PROPELLED
SAE AMS 1424 : 2016 FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1
SAE ARP926B FAULT/FAILURE ANALYSIS PROCEDURE
SAE AMS 1428 : 2017 FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4
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 J 1211 : 2012 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 ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
SAE ARP 5485 : 2007 ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE 2/3/4 AIRCRAFT DEICING/ANTI-ICING FLUIDS
SAE ARP 4737 : 2008 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

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