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 |