FAA AC 33-6 : 2017
Current
The latest, up-to-date edition.
WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES
Hardcopy , PDF
English
01-01-2017
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1. PURPOSE
2. RELATED PARTS AND SECTIONS OF 14 CFR
3. RELATED READING MATERIAL
4. BACKGROUND
5. DEFINITION
6. DISCUSSION
Gives guidance to demonstrate compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) part 33, Airworthiness Standards: Aircraft Engines.
| DocumentType |
Standard
|
| Pages |
12
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| SAE AMS2645K | FLUORESCENT PENETRANT INSPECTION |
| FAA AC 33-2 : 2013 | GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES |
| SAE AMS 2646 : 1999 | CONTRAST DYE PENETRANT INSPECTION |
| SAE AMS 2804 : 2001 | IDENTIFICATION - CASTINGS |
| SAE AMS 2630 : 2010 | INSPECTION, ULTRASONIC, PRODUCT OVER 0.5 INCH (12.7 MM) THICK |
| AWS A5.10 : 1992 | BARE ALUMINUM AND ALUMINUM ALLOY WELDING ELECTRODES AND RODS, SPECIFICATION FOR |
| SAE AMS2635D | RADIOGRAPHIC INSPECTION |
| SAE AMS 4190 : 2015 | ALUMINUM ALLOY, WELDING WIRE 5.2SI (4043) |
| SAE AMS 2694 : 2013 | IN-PROCESS WELDING OF CASTINGS |
| SAE AMS H 6088 : 2000 | HEAT TREATMENT OF ALUMINUM ALLOYS |
| FAA AC 43-9 : C | MAINTENANCE RECORDS |
| FAA AC 43.9-1 : 2007 | INSTRUCTIONS FOR COMPLETION OF FAA FORM 337 |
| AWS B2.1 : 2005 | SPECIFICATION FOR WELDING PROCEDURE AND PERFORMANCE QUALIFICATION |
| SAE AMS 4031 : 2011 | ALUMINUM ALLOY, SHEET AND PLATE, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-O) ANNEALED OR WHEN SPECIFIED, 'AS FABRICATED' (2219-F) |
| AWS D17.1 : 2001 | SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
| FAA AC 145-3 : 1981 | GUIDE FOR DEVELOPING AND EVALUATING REPAIR STATION INSPECTION PROCEDURES MANUALS |
| SAE AMS 2644 : 2013 | INSPECTION MATERIAL, PENETRANT |
| SAE AMS4143E | ALUMINUM ALLOY FORGINGS AND ROLLED OR FORGED RINGS, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4214 : 2013 | CASTINGS, ALUMINUM ALLOY SAND, 5.0SI - 1.2CU - 0.50MG (355.0-T71), SOLUTION HEAT TREATED AND OVERAGED |
| FAA AC 43.13-1 : 0 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR |
| SAE AMS4313E | ALUMINUM ALLOY, ROLLED OR FORGED RINGS, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-T351, 2219-T352) SOLUTION HEAT TREATED AND MECHANICALLY STRESS RELIEVED |
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