FAA AC 33-2 : 2013
Current
The latest, up-to-date edition.
GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
Hardcopy , PDF
English
01-01-2013
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. Purpose
2. Applicability
3. Cancellation
4. Related Documents
5. Related Reading Material
6. General Type Certification Process
7. Surplus Military Aircraft Engines and Parts
8. Data Plates
9. Part 33 Guidance Material
Specifies general guidance concerning type certification projects for aircraft turbine engines.
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| 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 120-77 : 0 | MAINTENANCE AND ALTERATION DATA |
| FAA AC 43-207 : 2002 | CORRELATION, OPERATION, DESIGN, AND MODIFICATION OF TURBOFAN/JET ENGINE TEST CELLS |
| SAE AIR 4766 : 2012 | AIR QUALITY FOR COMMERCIAL AIRCRAFT CABINS |
| FAA AC 33.27-1 : 2011 | ENGINE AND TURBOSUPERCHARGER ROTOR OVERSPEED REQUIREMENTS OF 14 CFR SECTION 33.27 |
| FAA AC 20-147 : 2014 | TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| FAA AC 33-6 : 2017 | WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES |
| SAE AIR 1904 : 2012 | TIRE SPRAY SUPPRESSION - AIRPLANE DESIGN AND CONSIDERATION FOR |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 33.15-1 : 0 | MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
| SAE AIR 4766/2 : 2011 | AIRBORNE CHEMICALS IN AIRCRAFT CABINS |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
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