FAA AC 23.1419-2 : 2007
Current
The latest, up-to-date edition.
CERTIFICATION OF PART 23 AIRPLANES FOR FLIGHT IN ICING CONDITIONS
Hardcopy , PDF
English
01-01-2007
1. What is the purpose of this AC?
2. Who does this AC apply to?
3. Cancellation
4. Applicability
5. Related Regulations and Documents
6. Related Reading Material
7. Background
8. Planning
9. Design Objectives
10. Analyses and Ground Testing
11. Flight Test Planning
12. Flight Tests
13. Performance and Flying Qualities
14. Ice Shedding
15. Placarding and AFM
16. Instructions for Continued Airworthiness
17. Ground Deicing Fluids
Appendix 1 Definitions
Appendix 2 Guidelines for Determining Certification Basis on
Flight in Icing Approval STCs and Amended TCs
Appendix 3 Guidelines for Supplemental Type Certificates (STC)
and Amended Type Certificates on Airplanes
Appendix 4 Guidelines for Certifying Ice Protection Systems
on Airplanes Not for Flight in Icing Approval
("Non-Hazard" Basis)
Appendix 5 Guidelines for Approval of Replacement Parts for
Airframe Deicing Systems
Appendix 6 Part 23 Subpart B Tests for Section 23.1419 at
Amendment 23-43
Appendix 7 Ice Contaminated Tailplane Stall
Appendix 8 AFM Limitations and Normal Procedures Sections
Provides an acceptable means, but not the only means, of demonstrating compliance with the ice protection requirements in Title 14 of the Code of Federal Regulations (14 CFR) part 23.
DevelopmentNote |
Supersedes FAA AC 23.1419-2A. (08/2003) Supersedes FAA AC 23.143-1. (07/2007)
|
DocumentType |
Standard
|
Pages |
114
|
PublisherName |
Federal Aviation Administration
|
Status |
Current
|
Supersedes |
FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
FAA AC 23.143-1 : 0 | ICE CONTAMINATED TAILPLANE STALL (ICTS) |
FAA AC 20-147 : 2014 | TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION |
FAA AC 23-11 : 2009 | 14 CFR PART 23 TYPE CERTIFICATION OF AN AIRPLANE ORIGINALLY CERTIFICATED TO EUROPEAN AVIATION SAFETY AGENCY (EASA) (CS-VLA) STANDARDS OR JOINT AVIATION REQUIREMENTS - VERY LIGHT AIRPLANE (JAR-VLA) |
SAE AS 5498 : 2017 | MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
SAE ARP 6852 : 2017 | METHODS AND PROCESSES FOR EVALUATION OF AERODYNAMIC EFFECTS OF SAE-QUALIFIED AIRCRAFT GROUND DEICING/ANTI-ICING FLUIDS |
SAE ARP 5904 : 2002(R2012) | AIRBORNE ICING TANKERS |
FAA AC 91-74 : 2015 | PILOT GUIDE: FLIGHT IN ICING CONDITIONS |
I.S. EN 91-74:2002 | PILOT GUIDE FLIGHT IN ICING CONDITIONS |
FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
FAA AC 20-138 : 2014 | AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS |
SAE AIR 1168/4 : 2016 | SAE AEROSPACE APPLIED THERMODYNAMICS MANUAL ICE, RAIN, FOG, AND FROST PROTECTION |
FAA AC 20-149 : 2015 | INSTALLATION GUIDANCE FOR DOMESTIC FLIGHT INFORMATION SERVICE - BROADCAST |
BS 2G 135:1967 | Specification for electrically-heated pitot and pitotstatic pressure heads |
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