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FAA AC 25.1419-2 : 2009

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

COMPLIANCE WITH THE ICE PROTECTION REQUIREMENTS OF SECTION 25.1419(E), (F), (G), AND (H)
Available format(s)

Hardcopy , PDF

Superseded date

10-27-2014

Language(s)

English

Published date

01-01-2009

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Definition of Terms
4. Compliance with section 25.1419(e)(1) and (e)(2)
5. Compliance with section 25.1419(e)(3)
6. Compliance with section 25.1419(f)
7. Compliance with section 25.1419(g)
8. Compliance with section 25.1419(h)
Appendix 1 - RELATED DOCUMENTS

Specifies an acceptable means for showing compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) 25.1419(e), (f), (g), and (h), Ice protection. Part 25 contains the airworthiness standards applicable to transport category airplanes.

DocumentType
Standard
Pages
12
PublisherName
Federal Aviation Administration
Status
Superseded
SupersededBy

FAA AC 25.1329-1 : 2016 APPROVAL OF FLIGHT GUIDANCE SYSTEMS
FAA AC 25-25 : 2014 PERFORMANCE AND HANDLING CHARACTERISTICS IN ICING CONDITIONS

FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA AC 25.1419-1 : 0 CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES FOR FLIGHT IN ICING CONDITIONS
FAA AC 20-117 : 1982 HAZARDS FOLLOWING GROUND DEICING AND GROUND OPERATIONS IN CONDITIONS CONDUCIVE TO AIRCRAFT ICING
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
FAA AC 25-25 : 2014 PERFORMANCE AND HANDLING CHARACTERISTICS IN ICING CONDITIONS
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 25-7 : 2012 FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES

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PDF - English
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