SAE AS5681B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
03-09-2024
English
17-05-2016
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Superseded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 |
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