FAA AC 23-24 : 2005
Current
The latest, up-to-date edition.
AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
Hardcopy , PDF
English
01-01-2005
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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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