• There are no items in your cart
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Dismiss alert

FAA AC 33-6 : 2017

Current
Current

The latest, up-to-date edition.

WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2017

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 AMS 2645 : 1995 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 AMS 2635 : 1999 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 AMS 4143 : 2012 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 AMS 4313 : 2016 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

View more information
£33.39
Excluding VAT

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.