SAE AS 5498 : 2017
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 INFLIGHT ICING DETECTION SYSTEMS
Hardcopy , PDF
30-04-2022
English
05-12-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE AND REFERENCES
2. GENERAL DESIGN REQUIREMENTS
3. MINIMUM PERFORMANCE SPECIFICATION UNDER ENVIRONMENTAL
INFLIGHT ICING CONDITIONS
4. MINIMUM PERFORMANCE SPECIFICATION UNDER ENVIRONMENTAL
TEST CONDITIONS
5. TEST PROCEDURES
6. AIRCRAFT INSTALLATION GUIDANCE
7. NOTES
APPENDIX A - FIDS RESPONSE TIME REQUIREMENTS & RATIONALE
Includes Minimum Operational Performance Specification (MOPS) of ACTIVE on-board INFLIGHT Icing Detection Systems (FIDS).
| Committee |
AC-9C
|
| DevelopmentNote |
Supersedes SAE AS 6625 & SAE AS 8181 (11/2002)
|
| DocumentType |
Revision
|
| Pages |
76
|
| ProductNote |
THIS STANDARD ALSO REFERS TO SAE AIR 6440,DOT/FAA/AR-09/10
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| ARINC 403 : 1955 | GUIDANCE FOR DESIGNERS OF AIRBORNE ELECTRONIC EQUIPMENT |
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| FAA AC 23.1419-2 : 2007 | CERTIFICATION OF PART 23 AIRPLANES FOR FLIGHT IN ICING CONDITIONS |
| FAA AC 25-28 : 2014 | COMPLIANCE OF TRANSPORT CATEGORY AIRPLANES WITH CERTIFICATION REQUIREMENTS FOR FLIGHT IN ICING CONDITIONS |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| FAA AC 121.321-1 : 2011 | COMPLIANCE WITH REQUIREMENTS OF SECTION 121.321, OPERATIONS IN ICING |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| SAE ARP 5624 : 2013 | AIRCRAFT INFLIGHT ICING TERMINOLOGY |
| SAE AIR 1168/4 : 2016 | SAE AEROSPACE APPLIED THERMODYNAMICS MANUAL ICE, RAIN, FOG, AND FROST PROTECTION |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| SAE ARP 5905 : 2015 | CALIBRATION AND ACCEPTANCE OF ICING WIND TUNNELS |
| FAA AC 20-175 : 2011 | CONTROLS FOR FLIGHT DECK SYSTEMS |
| SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| FAA AC 25.1302-1 : 2013 | INSTALLED SYSTEMS AND EQUIPMENT FOR USE BY THE FLIGHTCREW |
| SAE AIR 4367 : 2012 | AIRCRAFT INFLIGHT ICE DETECTORS AND ICING RATE MEASURING INSTRUMENTS |
| FAA AC 25-25 : 2014 | PERFORMANCE AND HANDLING CHARACTERISTICS IN ICING CONDITIONS |
| MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| FAA AC 91-74 : 2015 | PILOT GUIDE: FLIGHT IN ICING CONDITIONS |
| SAE AS 8034 : 2011 | MINIMUM PERFORMANCE STANDARD FOR AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS |
| FAA AC 20-147 : 2014 | TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION |
| SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
| ARINC 415 : LATEST | OPERATIONAL/TECHNICAL GUIDELINES ON FAILURE WARNING & FUNCTIONAL TEST |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| FAA AC 25.1322-1 : 2010 | FLIGHTCREW ALERTING |
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