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FAA AC 23-24 : 2005

Current
Current

The latest, up-to-date edition.

AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2005

1 What is the purpose of this Advisory Circular (AC)?
2 Who is affected by this AC?
3 What documents does this AC supersede?
4 What other publications are related to this AC?
5 How is this Advisory Circular (AC) related to other
   Federal Aviation Administration (FAA) ACs and Policy
   Statements?
6 What common STC projects does this AC address?
7 Where can the common STC project checklists be found?
8 How were the standard compliance checklist and the lists
   of applicable regulations for these common STC projects
   developed?
9 How should the compliance checklists in this AC be used
   in certification projects?
10 Should these checklists be combined into one for projects
   that cover more than one of these changes?
11 How should the standard checklist be filled in to generate
   a checklist specific to a project?
12 What are the applicable regulations and guidance for the
   installation of an autopilot system?
13 What are the applicable regulations and guidance for the
   installation of a reciprocating engine with increased
   horsepower?
14 What are the applicable regulations and guidance for the
   installation of a turbo-prop engine with increased
   horsepower?
15 What are the applicable regulations and guidance for the
   installation of turbine engines to replace reciprocating
   engines?
16 What are the applicable regulations and guidance for the
   installation of a different propeller (simple)?
17 What are the applicable regulations and guidance for the
   installation of a different propeller (complex)?
18 What are the applicable regulations and guidance for the
   installation of auxiliary fuel tanks?
19 What are the applicable regulations and guidance to
   increase the airplane gross weight?
APPENDIX 1 - Supplemental Type Certificate Compliance
             Checklist

Provides information to create compliance checklists for some common Title 14 of the Code of Federal Regulations (14 CFR) part 23 Supplemental Type Certificate (STC) projects.

DocumentType
Standard
Pages
69
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 23-14 : 0 TYPE CERTIFICATION BASIS FOR CONVERSION FROM RECIPROCATING ENGINE TO TURBINE ENGINE-POWERED PART 23 AIRPLANES
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 23.607-1 : 0 SELF-LOCKING NUTS ON BOLTS SUBJECT TO ROTATION
FAA AC 20-119 : 1983 FUEL DRAIN VALVES
FAA AC 36-4 : C NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION
FAA AC 36-3 : 0 ESTIMATED AIRPLANE NOISE LEVELS IN A-WEIGHTED DECIBELS
FAA AC 36-1 : 0 NOISE LEVELS FOR U.S. CERTIFICATED AND FOREIGN AIRCRAFT
FAA AC 23-13 : 2005 FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
FAA AC 33-2 : 2013 GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
FAA AC 20-88 : A GUIDELINES ON THE MARKING OF AIRCRAFT POWERPLANT INSTRUMENTS (DISPLAYS)
FAA AC 23-9 : 0 EVALUATION OF FLIGHT LOADS ON SMALL AIRPLANES WITH T, V, +, OR Y EMPENNAGE CONFIGURATIONS
FAA AC 23-15 : 2003 SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM
FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
FAA AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
FAA 8110.4 : 2011 TYPE CERTIFICATION
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
FAA AC 23-2 : 0 FLAMMABILITY TESTS
FAA AC 23-19 : A AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
FAA AC 20-124 : 0 WATER INGESTION TESTING FOR TURBINE POWERED AIRPLANES
FAA AC 21.101-1 : 2016 ESTABLISHING THE CERTIFICATION BASIS OF CHANGED AERONAUTICAL PRODUCTS
FAA AC 35.37-1 : 2011 PROPELLER FATIGUE LIMITS AND EVALUATION
FAA AC 23-10 : 0 AUXILIARY FUEL SYSTEMS FOR RECIPROCATING AND TURBINE POWERED PART 23 AIRPLANES
FAA AC 36-2 : 0 MEASURED OR ESTIMATED (UNCERTIFICATED) AIRPLANE NOISE LEVELS
FAA AC 23-8 : 2011 FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
FAA AC 20-66 : 2011 PROPELLER VIBRATION AND FATIGUE
FAA AC 23.143-1 : 0 ICE CONTAMINATED TAILPLANE STALL (ICTS)
FAA AC 23.1523 : 2005 MINIMUM FLIGHT CREW
FAA 8110.48 : 2017 HOW TO ESTABLISH THE CERTIFICATION BASIS FOR CHANGED AERONAUTICAL PRODUCTS
FAA AC 20-146 : 2003 METHODOLOGY FOR DYNAMIC SEAT CERTIFICATION BY ANALYSIS FOR USE IN PARTS 23, 25, 27, AND 29 AIRPLANES AND ROTORCRAFT
FAA AC 20-74 : 1971 AIRCRAFT POSITION AND ANTICOLLISION LIGHT MEASUREMENTS
FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
FAA AC 21-40 : 2007 GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE
FAA AC 23-21 : 2004 AIRWORTHINESS COMPLIANCE CHECKLISTS USED TO SUBSTANTIATE MAJOR ALTERATIONS FOR SMALL AIRPLANES
FAA AC 23-17 : 2011 SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
FAA AC 20-130 : 0 AIRWORTHINESS APPROVAL OF NAVIGATION OR FLIGHT MANAGEMENT SYSTEMS INTEGRATING MULTIPLE NAVIGATION SENSORS
FAA AC 23.629-1 : 2004 MEANS OF COMPLIANCE WITH TITLE 14 CFR, PART 23, SECTION 23.629, FLUTTER
FAA AC 183.29-1 : 0 DESIGNATED ENGINEERING REPRESENTATIVES CONSULTANT DIRECTORY
FAA AC 20-122 : A ANTI-MISFUELING DEVICES: THEIR AVAILABILITY AND USE
FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
FAA AC 23-23 : 2004 STANDARDIZATION GUIDE FOR INTEGRATED COCKPITS IN PART 23 AIRPLANES
FAA AC 20-147 : 2014 TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION
FAA AC 20-135 : 0 POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA
FAA AC 20-128 : 0 DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

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