SAE AS5116C
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Minimum Operational Performance Specification for Ground Ice Detection Systems
Hardcopy , PDF
28-08-2007
English
28-08-2007
1 SCOPE
1.1 Applications of This Document
1.2 Functional Description of System
1.2.1 Onboard GIDS
1.2.2 Ground-Based GIDS
1.3 Composition of a GIDS
2 REFERENCES
2.1 Applicable Documents
2.1.1 SAE Publications
2.1.2 EUROCAE/RTCA or EUROCAE/SAE Publications
2.1.3 JAA/FAA Requirements, Regulations
2.1.4 Transport Canada Regulations
2.1.5 CEN/IEC/ISO Publications
2.1.6 ARINC Documents
2.1.7 MIL Documents
2.1.8 Weather Related Documents
2.2 Definitions and Abbreviations
2.2.1 Definitions
2.2.2 Abbreviations
3 GENERAL DESIGN REQUIREMENTS
3.1 Introduction
3.2 Airworthiness and Operational Requirements
3.2.1 Onboard GIDS
3.2.2 Ground-Based GIDS
3.3 Complex Hardware and Software Design
3.3.1 Onboard GIDS
3.3.2 Ground-Based GIDS
3.4 Technical Requirements
3.4.1 Materials
3.4.2 Workmanship
3.4.3 Electrical Bonding and Grounding
3.4.4 Interchangeability
3.4.5 Marking
3.5 Minimum Structural Requirements
3.5.1 Exposure During Normal Operations
3.5.2 Foreign Object Damage (FOR)
3.6 Human Factors
3.6.1 Hazards
3.6.2 Displays
3.7 Safety Requirements
3.7.1 Design for Safely
3.7.2 Failure Analysis
3.7.3 Detection Reliability
3.8 GIDS Operation
3.8.1 GIDS Controls
3.8.2 Data Processing
3.8.3 Onboard GIDS Activation
3.8.4 Built In Test Equipment (BITE)
3.8.5 Nuisance Alarms
3.8.6 Operating Weather Conditions
3.9 Qualification Tests
3.9.1 Responsibility for Testing
3.9.2 Test Article
3.9.3 Effects of Tests
3.10 Reports and Declarations
3.10.1 Summary Test Report
3.10.2 Substantiating Test Data/Analysis
3.10.3 Operating Procedures
3.10.4 Declarations
4 MINIMUM PERFORMANCE SPECIFICATION
4.1 Frozen Contamination Detection
4.1.1 Detection Threshold
4.1.2 Frozen Contamination Above the Detection Threshold
4.2 Fluid Condition Monitoring
4.3 Monitored Surface Finish and GIDS Performance
5 MINIMUM PERFORMANCE SPECIFICATION UNDER ENVIRONMENTAL TEST
CONDITIONS
5.1 Introduction
5.2 Testing
5.3 Onboard GIDS
5.4 Ground-Based GIDS
6 TEST PROCEDURES
6.1 General
6.1.1 Test Plan, Procedures and Reports
6.1.2 Power Input Voltage
6.1.3 Power Input Frequency
6.1.4 Ambient Conditions
6.1.5 Warm-up Period
6.1.6 Test Procedures
6.2 Detection Indication
6.3 Detailed Test Procedures
6.3.1 Frozen Contamination Detection
6.3.2 Fluid Condition Monitoring
6.3.3 Area Detection and Visibility Tests for Remote GIDS
7 INSTALLED EQUIPMENT PERFORMANCE
7.1 Introduction
7.1.1 Test Plan, Procedures and Reports
7.2 Installed Equipment Requirements
7.2.1 General
7.2.2 Technical
7.3 Installed Equipment Performance
7.3.1 Onboard GIGS
7.3.2 Ground-Based GIDS
7.4 Conditions of Test
7.4.1 Safety Precautions
7.4.2 Power Input
7.4.3 Associated Equipment and Systems
7.4.4 Environment
7 4 5 Warm-up period
7.5 Test Procedures for Installed Equipment Performance
7.5.1 General
7.5.2 Ground Test/Procedure
7.5.3 Flight Test/Procedure
APPENDIX A
APPENDIX B
Specifies minimum performance requirements of Ground Ice Detection Systems (GIDS). These systems may be mounted onboard the airplane, or be ground-based. Also provides information for indication and/or control.
DocumentType |
Standard
|
Pages |
63
|
PublisherName |
SAE International
|
Status |
Withdrawn
|
Supersedes |
This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of Ground Ice Detection Systems (GIDS). These systems may be mounted onboard the airplane, or be ground-based. They may provide information for indication and/or control.
SAE AS6285 | Aircraft Ground Deicing/Anti-Icing Processes |
ARINC 403 : 1955 | GUIDANCE FOR DESIGNERS OF AIRBORNE ELECTRONIC EQUIPMENT |
SAE AMS1424M | Deicing/Anti-Icing Fluid, Aircraft SAE Type 1 |
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 |
ISO 11077:2014 | Aircraft ground equipment De-icers Functional requirements |
EN 50020:2002 | Electrical apparatus for potentially explosive atmospheres - Intrinsic safety 'i' |
SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
SAE J1211_201211 | Handbook for Robustness Validation of Automotive Electrical/Electronic Modules |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
IEC 60079-11:2011 | Explosive atmospheres - Part 11: Equipment protection by intrinsic safety "i" |
SAE AIR4367A | Aircraft Inflight Ice Detectors and Icing Rate Measuring Instruments |
SAE ARP4737H | Aircraft Deicing/Anti-icing Methods |
EN 50081-2:1993 | Electromagnetic compatibility - Generic emission standard - Part 2: Industrial environment |
SAE ARP798A | Design Criteria for White Incandescent Lighted Aerospace Instruments |
SAE ARP582D | Lighting, Integral, For Aircraft Instruments: Criteria for Design of Red Incandescent Lighted Instruments |
ARINC 408A : 1976 | AIR TRANSPORT INDICATOR CASES AND MOUNTING |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
RTCA DO 216 : 1993 | MINIMUM GENERAL SPECIFICATION FOR GROUND-BASED ELECTRONIC EQUIPMENT |
SAE ARP4102/8A | Flight Deck Head-Up Displays |
EN 50082-2 : 95 AC 95 | ELECTROMAGNETIC COMPATIBILITY - GENERIC IMMUNITY STANDARD - INDUSTRIAL ENVIRONMENT |
EN 12312-6:2017 | Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment |
SAE ARP 4102/7 : 1988 | ELECTRONIC DISPLAYS |
SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
ARINC 415 : LATEST | OPERATIONAL/TECHNICAL GUIDELINES ON FAILURE WARNING & FUNCTIONAL TEST |
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