Search Results

Standard

BARKHAUSEN NOISE INSPECTION FOR DETECTING GRINDING BURNS IN HIGH STRENGTH STEEL PARTS

2010-11-01

HISTORICAL

ARP4462

This recommended practice covers the procedures and method for establishing acceptance criteria when performing Barkhausen noise testing of surface-hardened steel components to detect grinding burns (metallurgical damage caused by over-heating) in bare or chromium-plated parts.

Standard

Barkhausen Noise Inspection for Detecting Grinding Burns in High Strength Steel Parts

2018-07-10

HISTORICAL

ARP4462A

This recommended practice establishes the requirements and procedures for Barkhausen Noise (BN) inspection of ferromagnetic steel components. Applications of the method are listed below in 1.2 through 1.5.

Standard

Barkhausen Noise Inspection for Detecting Grinding Burns in High Strength Steel Parts

2019-06-06

CURRENT

ARP4462B

This recommended practice establishes the requirements and procedures for Barkhausen Noise (BN) inspection of ferromagnetic steel components. Applications of the method are listed in 1.2 through 1.5.

Standard

CONTRAST DYE PENETRANT INSPECTION

1955-03-01

HISTORICAL

AMS2646

Standard

CONTRAST DYE PENETRANT INSPECTION

1964-01-01

HISTORICAL

AMS2646A

Standard

CONTRAST DYE PENETRANT INSPECTION

1969-05-01

HISTORICAL

AMS2646B

Standard

CONTRAST DYE PENETRANT INSPECTION

1991-10-15

HISTORICAL

AMS2646C

This specification establishes a procedure for detection of discontinuities open to the surface of parts by the use of a penetrating dye.

Standard

Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware

2019-10-14

CURRENT

AS4787A

This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, low conductivity (less than 5% IACS) aircraft engine hardware with fasteners removed. The inspection is intended to be performed at maintenance and overhaul facilities on engine run hardware.

Standard

Eddy Current Inspection of Circular Holes in Nonferrous Metallic Aircraft Engine Hardware

2013-06-11

HISTORICAL

AS4787

This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, aircraft engine hardware with fasteners removed. The inspection is intended to be performed at maintenance and overhaul facilities on engine run hardware.

Standard

Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure

2013-06-11

HISTORICAL

ARP4402

This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures.

Standard

Enhanced Ultrasonic Immersion Inspection for Titanium Alloy and other Metal Alloy Billets

2019-05-16

CURRENT

AMS2628B

This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy round billet 5 inches (127 mm) and over in nominal diameter (see 8.5). Metal alloy billets other than titanium may be tested to this specification with the use of suitable reference standards.

Standard

FLUORESCENT PENETRANT INSPECTION

1991-10-01

HISTORICAL

AMS2645H

This specification establishes a procedure for detection of defects by use of a fluorescent, penetrating liquid.

Standard

FLUORESCENT PENETRANT INSPECTION

1965-02-15

HISTORICAL

AMS2645F

Standard

FLUORESCENT PENETRANT INSPECTION

1969-05-01

HISTORICAL

AMS2645G

Standard

FLUORESCENT PENETRANT INSPECTION

1950-06-15

HISTORICAL

AMS2645A

Standard

FLUORESCENT PENETRANT INSPECTION

1964-01-31

HISTORICAL

AMS2645E

Standard

FLUORESCENT PENETRANT INSPECTION

1955-03-01

HISTORICAL

AMS2645C

Standard

FLUORESCENT PENETRANT INSPECTION

1961-01-15

HISTORICAL

AMS2645D

Standard

FLUORESCENT PENETRANT INSPECTION

1953-06-15

HISTORICAL

AMS2645B

Standard

FLUORESCENT PENETRANT INSPECTION Aircraft and Engine Component Maintenance

2011-08-10

HISTORICAL

AMS2647

This specification establishes requirements, instructions, and procedures to ensure that fluorescent penetrant inspections are capable of achieving an acceptable level of defect detection on aircraft and engine components during maintenance and overhaul operations.