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AIA/NAS - NASM33602

BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR

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Organization: AIA/NAS
Publication Date: 28 October 2011
Status: inactive
Page Count: 2

Document History

NASM33602
January 31, 2023
BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR
A description is not available for this item.
NASM33602
October 28, 2011
BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR
A description is not available for this item.
NASM33602
October 28, 2011
BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR
A description is not available for this item.
NASM33602
September 1, 1999
Bolts, Self-Retaining, Aircraft, Reliability and Maintainability, Design and Usage Requirements for
A description is not available for this item.

References

This document references:
NASM21224 - NUT, SELF-LOCKING, CASTELLATED, HEXAGON, COUNTERBORED, ASSEMBLED WASHER, 250 °F, NON-METALLIC INSERT (FOR SELF-RETAINING BOLTS)
Published by AIA/NAS on November 29, 2019
A description is not available for this item.
This document references:
NASM310 - NUT, PLAIN, CASTELLATED, AIRFRAME
Published by AIA/NAS on October 30, 2021
A description is not available for this item.
This document references:
NASM21224 - NUT, SELF-LOCKING, CASTELLATED, HEXAGON, COUNTERBORED, ASSEMBLED WASHER, 250 °F, NON-METALLIC INSERT (FOR SELF-RETAINING BOLTS)
Published by AIA/NAS on November 29, 2019
A description is not available for this item.
This document references:
NASM83050 - BOLT, SELF-RETAINING, IMPEDANCE TYPE
Published by AIA/NAS on February 28, 2020
This specification establishes the requirements for an impedance-type self-retaining bolt that is intended for critical applications.
This document is referenced by:
NASM21244 - NUT, CASTELLATED, HEXAGON, COUNTERBORED ASSEMBLED WASHER, 450 °F, FOR SELF-RETAINING BOLTS
Published by AIA/NAS on September 19, 2014
A description is not available for this item.
This document is referenced by:
MIL-DTL-9490 - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
Published by NPFC on April 22, 2008
This specification establishes general performance, design, develop, and quality assurance requirements for the flight control systems of manned piloted aircraft. Flight Control Systems (FCS)...
This document is referenced by:
NASM21125 - BOLT, SELF-RETAINING, POSITIVE LOCKING, CRES, 90 KSI Fsu, 63 KSI Ftu, PAN HEAD, 450 °F & 650 °F
Published by AIA/NAS on May 31, 2022
A description is not available for this item.
This document is referenced by:
NASM21244 - NUT, CASTELLATED, HEXAGON, COUNTERBORED ASSEMBLED WASHER, 450 °F, FOR SELF-RETAINING BOLTS
Published by AIA/NAS on September 19, 2014
A description is not available for this item.
This document is referenced by:
NASM21130 - BOLT, SELF-RETAINING, POSITIVE LOCKING, CRES, 90 KSI Fsu, 63 KSI Ftu, 100° FLUSH HEAD, 450 °F & 650 °F
Published by AIA/NAS on July 31, 2012
A description is not available for this item.
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