FAA 8110.54 : 2010
Current
The latest, up-to-date edition.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS
Hardcopy , PDF
English
01-01-2010
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Chapter 1 - General Information
Chapter 2 - Regulatory Requirements for ICA
Chapter 3 - ICA Format and Types of Data
Chapter 4 - Required Manuals or Sections
Chapter 5 - ACO and AEG Responsibilities
Chapter 6 - Distributing ICA and Changes
Appendix A - Part 23 Airplane ICA Checklist
Appendix B - Part 25 Airplane ICA Checklist
Appendix C - Part 27 Rotorcraft ICA Checklist
Appendix D - Part 29 Rotorcraft ICA Checklist
Appendix E - Manned Free Balloon ICA Checklist
Appendix F - Aircraft Engine ICA Checklist
Appendix G - Propeller ICA Checklist
Appendix H - Related Publications
Appendix I - Definitions
Appendix J - Acronyms
Appendix K - Administrative Information
Appendix L - FAA Form 1320-19 Directives Feedback
Information
Describes aircraft certification office (ACO), engine certification office (ECO) (from now on both referred to as "ACO") and aircraft evaluation group (AEG) staffs how to review instructions for continued airworthiness (ICA) and find their provisions acceptable, or approved, as appropriate.
| DevelopmentNote |
Supersedes FAA 8110.50 (07/2005)
|
| DocumentType |
Standard
|
| Pages |
69
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| Supersedes |
| FAA AC 43.13-2 : 2008 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT ALTERATIONS |
| FAA AC 91-81 : 2008 | FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE |
| FAA 8300.16 : 2014 | MAJOR REPAIR AND ALTERATION DATA APPROVAL |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| FAA AC 20-180 : 2013 | APPROVED MODEL LIST SUPPLEMENTAL TYPE CERTIFICATE (AML-STC) |
| FAA AC 33-9 : 2010 | DEVELOPING DATA FOR MAJOR REPAIRS OF TURBINE ENGINE PARTS |
| FAA AC 120-102 : 2012 | INCORPORATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTO AN OPERATOR'S MAINTENANCE PROGRAM |
| FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
| FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
| FAA AC 21-45 : 2010 | COMMERCIAL PARTS |
| FAA AC 121-22 : 2012 | MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES |
| FAA 8110.104 : 2007 | RESPONSIBILITIES AND REQUIREMENTS FOR IMPLEMENTING PART 26 SAFETY INITIATIVES |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 33-8 : 2009 | GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION |
| FAA AC 120-104 : 2011 | ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE |
| FAA 8100.15 : 2013 | ORGANIZATION DESIGNATION AUTHORIZATION PROCEDURES |
| FAA AC 91-82 : 2012 | FATIGUE MANAGEMENT PROGRAMS FOR IN-SERVICE ISSUES |
| SAE ARP6461 | Guidelines for Implementation of Structural Health Monitoring on Fixed Wing Aircraft |
| FAA 8150.1 : 2017 | TECHNICAL STANDARD ORDER PROGRAM |
| FAA 8430.21 : 0 | FLIGHT STANDARDS DIVISION, AIRCRAFT CERTIFICATION DIVISION, AND AIRCRAFT EVALUATION GROUP RESPONSIBILITIES |
| FAA 8100.15 : 2013 | ORGANIZATION DESIGNATION AUTHORIZATION PROCEDURES |
| FAA AC 21-23 : 2004 | AIRWORTHINESS CERTIFICATION OF CIVIL AIRCRAFT, ENGINES, PROPELLERS, AND RELATED PRODUCTS IMPORTED TO THE UNITED STATES |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 33.4-2 : 0 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS: IN-SERVICE INSPECTION OF SAFETY CRITICAL TURBINE ENGINE PARTS AT PIECE-PART OPPORTUNITY |
| FAA AC 121-22 : 2012 | MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES |
| FAA AC 25-26 : 2007 | DEVELOPMENT OF STANDARD WIRING PRACTICES DOCUMENTATION |
| FAA 8110.52 : 2017 | TYPE VALIDATION AND POST-TYPE VALIDATION PROCEDURES |
| FAA AC 25-19 : 2011 | CERTIFICATION MAINTENANCE REQUIREMENTS |
| FAA AC 33.4-3 : 2005 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS; AIRCRAFT ENGINE HIGH INTENSITY RADIATED FIELDS (HIRF) AND LIGHTNING PROTECTION FEATURES |
| FAA AC 33.4-1 : 0 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS |
| FAA AC 25.1529-1 : 2007 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OF STRUCTURAL REPAIRS ON TRANSPORT AIRPLANES |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| FAA 8110.42 : 2014 | PARTS MANUFACTURER APPROVAL PROCEDURES |
| FAA AC 35.4-1 : 0 | PROPELLER INSTRUCTIONS FOR CONTINUED AIRWORTHINESS |
| FAA AC 21-40 : 2007 | GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE |
| FAA 8110.37 : 2011 | DESIGNATED ENGINEERING REPRESENTATIVE (DER) HANDBOOK |
| FAA AC 20-114 : 1981 | MANUFACTURER'S SERVICE DOCUMENTS |
| FAA AC 25-27 : 2010 | DEVELOPMENT OF TRANSPORT CATEGORY AIRPLANE ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS USING AN ENHANCED ZONAL ANALYSIS PROCEDURE |
| FAA 8100.8 : 2011 | DESIGNEE MANAGEMENT HANDBOOK |
| FAA 8150.1 : 2017 | TECHNICAL STANDARD ORDER PROGRAM |
| FAA AC 43.13-1 : 0 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR |
| FAA 8110.104 : 2007 | RESPONSIBILITIES AND REQUIREMENTS FOR IMPLEMENTING PART 26 SAFETY INITIATIVES |
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